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NAVAIR 51-60A-1_____________________ TO 35E2-2-7

Handbook

Installation, Maintenance, Repackagingand

Illustrated Parts Breakdown

AM -2 AIRFIELD LANDING MATAND ACCESSORIES

Basic & All Changes Have Been Merged To Make This A Complete Publication

This publication te required for official ue or for administrative or operational purposes only. Distribution is limited to U.S. Govern-ment agencies. Other requests for this document must be referred to Warnar Robins ALC/MMEDT. Robins AFB GA 31098-5609.

PUBLISHED UNDER AUTHORITY OF THE SECRETARY OF THE AIR FORCEAND BY DIRECTION OF THE CHIEF OF THE NAVAL AIR SYSTEMS COMMAND

--^ 1 APRIL 1974CHANGE 2-6 SEPTEMBER 1985

TO 35E2-2-7

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TOTAL MUMBKR OP PA6H IM THIS PUBLICATION IS 166 COHSISTIM& OF THt FOLLOW1WC:

Page * Change Page ChangeNo. No. No. No.

Title 2A 2i vii 0viii Blank. 01 4 0

1-1 1-4 02-1 2-10. 03-1 3-18. 04-1 4-2 0

5-1 5-8 06-1 6-2 0

7-1 7-15. U7-16 -7-18 17-19. 07-20- 08-1 8-8 08-9 8-10 Deleted. 08-11 8-18 09-1 "-2 010 ;.. 10-3 010- wiank. 011-1 211-2 o12-1. 012-2 Blank. 013-1 13-6 014-1 14-10- 0

14-11 14-12 Deleted 014-13 14-40 015-1 15-7 0

15-8 Blank. 0

Index I Index 3 0

Index 4 Blank 0

Flyleaf 1 0Flyleaf 2 Blank 0

* Zero in this column indicates an original page.

A Change 2

NAVA1R 51.60A.1 TabI* ot ConfnU

TABLE OF CONTENTS

Section pa^

INTRODUCTION 1

1 Purpose of Handbook\

2 Scope of Handbook3 Responsibility4 Arrangement of Contents? Related Literature6 Binding and Identifying Manuals 2

7 Changes and Revisions of Manuals8 Recommending Manual Change ->

\ FIELD CONFIGURATIONS AND SITE PREPARATION 1-1

1-1 Field Configuration I’l

1-3 Soil Condition I’l

1-4 Site Preparation 1-1

1-6 Grading 1-1

1-7 Survey 1-1

1-8 Hard Surface Runway 1-1

II GENERAL DESCRIPTION 2-1

2-1 AM-2 Matting and Related Components 2-1

2-3 AM-2 Matting 2-1

2-4 Mat Coverage 2-42-6 Starter Keylock 2-42-7 Typical Keylock 2-42-8 Female Keylock 2-52-9 90 Connector (H Type) 2-52-10 Adjustable 90 Connector 2-52-11 Mat End Ramp 2-62-12 Blast Deflector Adapter 2-72-13 Tiedowns 2-72-14 Guide Rail 2-72-15 Replacement Mats 2-72-16 Heavy Duty Mats 2-82-17 Adjustable Keylocks 2-92-18 Spacer Mats 2-92-19 Edge Clamps and Stakes 2-9

III PACKAGING 3-1

3-1 General 3.13-3 Mat Pallets, (Full Length), Fll, F15, and F27 3.13-4 Hall Mat Pallet, F12 and F32 3.33-5 Keylock Pallet, F13 3.5

i

Tabl of Contents NAVAIR 51-60A-1

Section Page

3-6 Adjustable 90 Connector Pallet, F31 3-63-7 90 Connector (H Type) Pallet, F14. 3-73-8 Blast Deflector Adapter Pallet, F18 3-83-9 Ticdown Container, Fl 3-93-10 Edge Clamps and Stakes Pallet, F28 3-103-11 Heavy Duty Mat Pallet, F26 3-113-12 Spacer Pallet, F25 . 3-123-13 Adjustable Keylock Pallet, F29 3-133-14 Mat End Ramp Pallets 3-143-15 Replacement Mat Pallet, SF1 3-153-16 Replacement Mat Pallet (AM-2, Mod 4), SF2 3-16

IV TOOLS AND EQUIPMENT . 4-1

4-1 General 4-14-3 Miscellaneous Tools 4-1

V PALLET DEPLOYMENT 5-1

5-1 Deployment 5-15-3 Method 5-15-5 Fork Lift Truck Deployment 5-15-6 On Field Deployment 5-15-7 VTOL Airfield Matting Deployment 5-15-9 VSTOL Airfield Matting Deployment 5-15-11 SATS Airfield Matting Deployment 5-45-13 Expeditionary Airfield 5-65-15 Miscellaneous Pallet Deployment 5-75-16 General 5-75-17 Mat End Ramp Pallet 5-75-18 Blast Deflector Adapter Pallets 5-75-19 Tiedown Containers 5-75-20 Edge Clamps and Stakes Pallet ’. 5-75-21 Heavy Duty Mat Pallet 5-85-22 Adjustable Keylocks and Spacer Mats Pallets . 5-85-23 Replacement Mat Pallets 5-8

VI PALLET DISASSEMBLY 6-1

6-1 General 6-16-3 Disassembly Instructions 6-16-4 Mat Pallet . 6-16-5 Keylock Pallet 6-16-6 90Connector Pallets 6-16-7 Blast Deflector Adapter Pallet 6-16-8 Tiedown Containers 6-16-9 Edge Clamp and Stakes Pallet 6-16-10 Heavy Duty Mat Pallet 6-16-11 Spacer Mat Pallet 6-26-12 Adjustable Keylock Pallet 6-26-13 Replacement Mat Pallet 6-2

ii

NAVAIR 51.60A-1 Table ofConfnf

Section Page

VII INSTALLATION INSTRUCTIONS 7-1

7-1 General 7-17-3 Installation Crew 7-17-5 SATS Field Installation Sequence 7-17-6 Without Guide Rail . 7-17-7 With Guide Rail 7-17-8 Mat Laying Procedure Without Guide Rail 7-17-10 Approach Aprons and Mat end Ramps 7-87-11 Mat Laying Procedure With Guide Rail 7-10

7-13 Field Laying Procedure 7-157-15 Runway Taxiway Connectors 7-157-16 Installation of Tiedowns 7-167-17 Parking and Storage Areas 7-167-18 Blast Deflector Installation 7-177-19 Installation of Edge Clamps and Stake Assemblies 7-17

VIII ORGANIZATIONAL LEVEL MAINTENANCE 8-1

8-1 General 8-1b-3 Deck Covering Repair 8-18-4 Surface Dent Repair 8-18-5 Skin Ruptures 8-28-6 Individual Mat Replacement 8-38-7 Section of Runway Replacement 8-68-8 Deleted 8-88-9 Deleted 8-118-10 Edge Repairs 8-118-11 General 8-118-12 Use of Typical Keylocks, Adjustable Keylocks, and Spacer Mats 8-138-13 Replacement Procedures 8-138-14 Maintenance of Adjustable Keylocks and 90 Connectors 8-17

IX REMOVAL PROCEDURE 9-1

9-1 General 9-19-3 Matting Removal Without Guide Rail 9-19-4 Matting Removal With Guide Rail 9-1

X REPACKAGING . lo-l

10-1 AM-2 Mar Pallet Assembly 10-110-2 Half Mat Pallet Assemblies 1Q-1

10-3 Keylock Pallet Assembly 10-110-4 Adjustable 90 Connector Pallet io-210-5 Blast Deflector Adapter 1Q-210-6 Tiedown Containers 10-210-7 Edge Clamps and Stakes Pallets (F28). io-210-8 Heavy Duty Mat Pallet Assembly (F26). io-210-9 Spacer Mat Pallet Assembly (F25) 10-310-10 Adjustable Keylock Pallet Assembly (F29) 10-310-11 90 Connector (H Type) Pallet (F 14) 10-3

ill

Table of Contents NAVAIR 51-60A-1

Sectionp^

XI INTERMEDIA? 1’: LKVEL MAINTENANCE H-l

11-1 General 11-111-3 Unpacking 11-111-5 Tie Rod Pallets n.i11-6 Strap and Seal Pallets 11-}

11-7 Special Containers n.111-8 Inspection and Classification n.i11-11 Repair 11-211-13 Repackaging n.2

XII DEPOT LEVEL MAINTENANCE 12-1

12-1 General 17.1

XIII ILLUSTRATED PARTS BREAKDOWN-INTRODUCTION 13.1

XIV GROUP ASSEMBLY PARTS LIST 14-1

XV NUMERICAL INDEX 15-1

ALPHABETICAL INDEX Index-1

iv

NAVAIR 51-60A-1 Listof llluraloB

LIST OF. ILLUSTRATIONS

Figure ?’<

1 Sample of NAVAIR Form 13800/2 for Recommending Changes to Handbook 41-1 Field Configurations Direct Installation 1-2

2-1 AM-2 Matting and Related Component Installation (Without Guide Rail) 2-22-2 AM-2 Matting and Related Component Installation (With Guide Rail) 2-32-3 AM-2 Mat Configuration 2-42-4 Starter Keylock 2-42-5 Typical Keylock 2-52-6 Female Keylock 2-52-7 90 Connector (H Type) 2-52-8 Adjustable 90 Connector 2-52-9 Mat End Ramp 2-62-10 Blast Deflector Adapters 2-72-11 Tiedown 2-7

2-12 Guide Rail (Catapult System) 2-7

2-13 Replacement Mat 2-8

2-14 Heavy Duty Mat 2-8

2-15 Adjustable Keylock Assembly 2-92-16 Spacer Mats 2-92-17 Edge Clamps and Stakes 2-10

3-1 AM-2 Mat Pallet (Full Length) (Fll) 3-13-2 AM-2 Mat Pallet (Full Length) (F15 and F27) 3-23-3 AM-2 Mat Pallet (Half Length) (Fl 2) 3-33-4 Half Mat Pallet (F32) 3-43-5 Keylock Pallet (F13) 3-5

3-6 Adjustable 90 Connector Pallet (F31) 3-63-7 90 Connector (H Type) Pallet (F14) 3-73-8 Blast Deflector Adapter Pallet (F18) 2-83-9 Tiedown Container (Fl) 3-93-10 Edge Clamps and Stakes Pallet (F28) 3-103-11 Heavy Duty Mat Pallet (F26) 3-113-12 Spacer Pallet (F25) 3-123-13 Adjustable Keylock Pallet (F29) 3-133-14 Mat End Ramp Pallets 3-143-15 Replacement Mat Pallet (SF1) 3-153-16 Replacement Mat Pallet (AM-2 Mod 4) (SF2) 3-16

5-1 Pallet Deployment on Runway in Parallel Rows (Without Guide Rail) 5-25-2 Pallet Deployment on Centerline of Runway (Without Guide Rail) 5-35-3 VTOL Airfield Arrangement 5-45-4 VSTOL Airfield Arrangement 5-45-5 SATS Airfield Arrangement 5-55-6 Pallet Deployment for Taxiways 5-55-7 Expeditionary Airfield Arrangement 5-65-8 Pallet Deployment for Expeditionary Airfield Parking Area 5.7

7-1 AM-2 Mat Installation Sequence (Without Guide Rail) 7.27-2 Placing of Starter Keylocks on Transverse Centerline of Runway 7.5

v

List of Illustrations NAVAIR 51-60A-1

Figure Page

7-3 Placing of First and Second Mats. 7-47-4 Engaging First Mat (Half Length) to Starter Keylock 7-47-5 Engaging of First and Second Mat 7-57-6 Locking First and Second Mat Using Locking Bar 7-67-7 Insertion of the Locking Bar 7-77-8 Placing of Third Mat (Full Length) 7-77-9 Correction of Mat Misalignment 7-97-10 Placing of Typical Keylocks in Matting Field 7-107-11 Laying of Runway Approach Apron 7-117-12 Placement of Mat End Ramps 7-127-13 AM-2 Mat Installation Sequence (With Guide Rail) 7-137-14 Laying of Guide Rails and Mats 7-147-15 Installation of Adjustable 90 Connectors, Procedure No. 1 7-157-16 Installatioo of 90 Connectors (H Type), Procedure No. 2 7-167-17 Drilling Jig for Installing Tiedowns 7-177-18 installing Tiedowns in AM-2 Matting 7-18

7-19 Installation of Blast Deflector Adapters and Mats 7-187-20 Anchoring Female Mat Edge Using Type I Edge Clamp 7-197-21 Anchoring Male Mat Edge Using Type II Edge Clamp 7-197-22 Anchoring Edge with Downturned Prongs Using Type III Edge Clamp 7-197-23 Anchoring Edge with Upturned Prongs Using Type IV Edge Clamp 7-20

7-24 Methods of Emplacing Stakes to Retain Edge Clamps 7-20

8-1 Surface Dent Repair 8-2

8-2 Skin Rupture Repair 8-2

8-3 Mat Cutting for Removing Mat 8-48-4 Replacement Mat Installation 8-58-5 Typical Keylock Removal Tool 8-68-6 Removal of Locking Bar. 8-78-7 Deleted 8-8

8-8 Deleted 8-98-9 Deleted 8-10

8-10 Straightening of Lower Female Edge 8-11

8-11 Straightening of Upper Female Edge 8-12

8-12 Straightening of Male Edge 8-12

8-13 Row Space to be Filled with Adjustable Keylocks and Spacer Mats 8-138-14 Installation of Row of Typical Keylocks 8-14

8-15 Installation of Right or Left Hand Row of Adjustable Keylocks 8-158-16 Installation of Row of Spacer Mats 8-168-17 Installation of Row of Various Combinations of Keylocks and Spacer Mats 8-18

10-1 Alignment of AM-2 Mat Ends in Pallet 10-1

10-2 A’ignment of Replacement Mat Ends in Pallet. 10-2

vl

NAVAIR 51.60A-1 List of Illustrations

GROUP ASSEMBLY PARTS LIST

LIST OF ILLUSTRATIONS

-"igure Page

14-1 VTOL Matting Installation, Forward Operating Site (2 Sheets) 14-214-2 VSTOL Matting Installation (Direct) Forward Operating Facility (2 Sheets) 14-414-3 VSTOL Matting Installation (Conversion) Forward Operating Facility (2 Sheets) 14-614-4 VSTOL Matting Installation (Not Expandable) (2 Sheets) 14-814-5 SATS Matting Installation (Direct) (2 Sheets) 14-1014-6 SATS Matting Installation (Conversion VSTOL to SATS (2 Sheets) 14-1214-7 Expeditionary Airfield Matting Installation (Direct) (2 Sheets) 14-1414-8 Expeditionary Airfield Matting Installation (Conversion from SATS Airfield) (2 Sheets) 14-1614-9 Tiedown Container (Fl) 14-1814-10 Full Mat Pallet (Fll) 14-19[4-11 Half Mat Pallet (F12) 14-20.4-12 H.ilf Mat Pallet (F32) 14-21^4-13 Keylock Pallet (F13) 14-224-14 90 Connector (H Type) Pallet (F 14) 14-244-15 Pallet and Mat Assembly (F15) (Full Mat) 14-264-16 Blast Deflector Adapter Pallet (F18) 14-274-17 Pallet and Spacer Assembly (F25) 14-284-18 Heavy Duty Pallet and Mat Assembly (F26) 14-294-19 Pallet and Mat Assembly (F27) 14-304-20 Mat End Ramp and Pallet Assembly 14-314-21 Adjustable Keylock Pallet Assembly (F29) 14.324-22 Edge Clamp and Stake Pallet (F28) 14-344-23 Replacement Mat Pallet (SF1) 14-364-24 Replacement Mat Pallet (SF2) 14-384-25 Adjustable 90 Connector Pallet (F31) 14-40

LIST OF TABLES

imber Page

Soil Characteristics 1-3List of AM-2 Matting and Related Component Packages 3-17List of Special Tools 4-1Dimensions and Package Data for Typical Keylocks, Adjustable Keylocks, and Spacer

Pallets 8-131 Combination of Items Versus Size of Row Space 8-14

vii,

NAVAIR 51.60A.1 Introduction

\

INTRODUCTION

1. PURPOSE OF HANDBOOK, brief treatment of the site preparation requirementsfor each.

Ti ins handbook is issued as a basic publicationic prpsenr the derailed installation, maintenance, and SECTION II. GENERAL DESCRIPTION. Thist"rr; -.?; in^Tr tion’, for the following applications of section describes the AM-2 matting and related con>-\\!-: airf si-id landing n;.. and accessories- ponents. It also contains typical configurations to

show their arrangement for runway, taxiway, and park-’i-iK-a’ take-off and landing site (VTOL) init areas.

Very short rak’--.if and landing site (VSTOL) SECTION III. PACKAGING. This section con-tains a description of the method of packaging AM-2

,’".’..f: air-it ;J fo; ,.ical .support (SATS) matting and related components. It includes a list ofpackages. Table 2, with identification numbers and

Ex;-c.iitionary airfield (EA) description of contents. Each individual package is

described.2. SCOPE OF HANDBOOK.

SECTION IV. TOOLS AND EQUIPMENT. ThishanJb’;L.ti <’!’s<rib<:;s general requirements forsection lists the tools and equipment that are required

.site ,’rcpaiation, pallet deployment, and outlines the i f i

for the miscellaneous preparations, installation, anddeta;S"ti installation and removal procedures for AM-2

-i j adjustments incident to the use of AM-2 matting andmat’i;if;’. and n-lated components. Detailed instructions

ar" a’so (,rovi,’cd for connecting and interlocking the "lated components.

indi.n’na! ,\\’,- f. n’a’s to construct the various air-field types sp- ifieJ in paragraph 2 above. SECTION V. PALLET DEPLOYMENT. This sec-

tion furnishes the optimum deployment of pallets and

3. RESPONSIBILITY, containers to minimize manual handling under combatconditions, consistent with available manpower and

Th<- officer in charge of this installation and/or equipment.

removal of thr: matting field, and the AM-2 mattings,.shall become thoroughly familiar with the contents SECTION VI. PALLET DISASSEMBLY. This

of this handbook and shall insure that all prescribed section instructs how to disassemble each pallet and

procedures are followed. Personnel assigned to install includes advice on storage of pallet items for future

the AM-2 matting and related components shall be use’

thoToughlv trained in the procedures outlined in thishandbook so the matting field can be constructed as SECTION VII. INSTALLATION INSTRUCTIONS.

quickly and efficiently as possible. This handbook This ^"o" prescribes the organization of the instal-

shall be used as the basic source of material for this lation crew and g"^ the general sequence to install

training, and as a standard reference for the con- matting and components for various types of runway

tinuing guidance of the crew in the performance of with their modifications. Illustrations depict detailstheir assigned duties. of a11 installation operations

4. ARRANGEMENT OF CONTENTS. SECTION VIII. ORGANIZATIONAL MAINTE-NANCE. This section describes the maintenance

SECTION I. FIELD CONFIGURATION AND SITE tasks which are allocated to the organizational main-PREPARATION. This section presents the VTOL, tenance level. The section describes how to repairVSTOL, SATS and EA field configurations and a damaged matting and related components. Included

1

Introduction (UVAiR S1 &’)A-1

in the section is a list of required tools, equipment c. NAVAIR 51-5A-3, Installation, Operation andSlit-id materials. Maintenance with Illustrated Parts Breakdown, Light

weight Earth Anchor and Tool Kit Manual.SECTION IX. REMOVAL PROCEDURE. This

section provides the sequence of operations to dis- d. NAVAIR 51-35-7, Technical Manual, Logisticsassemble and remove matting and components of a Data Initial Staging Area to Field Installation, Ex-completed airfield, peditionary Airfields.

SECTION X. REPACKAGING. This section gives <" Installation Sequence Data Cards (ISDC), SATS.the method and sequence to reassemble and repackagethe matting and components removed from a dismantled f- ^Pa""16’"1 of Army Technical Manual TM-5-530,airfield. Materials Testing.

I" addition, Matrine Service Changes, Service Bul-SECTION XI. INTERMEDIATE MAINTENANCE. l.,ins, and Repair Procedures are issued by the NavalIhis section presents the maintenance tasks which Air s;i7cin, ("- A TI. i*/l" systems (.-ommand. These documents supersedeare allocated to the intermediate maintenance level, iiifnrmari^ ,.1, <intorinatlon in the manual if they are not listed on the

flyleaf page as incorporated.SECTION XII. DEPOT MAINTENANCE. This

section provides a description of maintenance tasksassigned to depot level maintenance personnel.

A COInp ete set aperture cards is su(TIlcd bythe Naval Air Engineering Center. Subsequent changes

SECTION XIII. ILLUSTRATED PARTS BREAK-t() the’e aperture cards are automic’lly furnished by

DOWN, INTRODUCTION. This section containsinstructions for use of the Group Assembly Parts List.The section also provides a list of definitions for fi. BINDING AND IDENTIFYING MANUALSSMR codes appearing in the list (section XIV).

SECTION XIV. GROUP ASSEMBLY PARTS LISTThree-post binders are available from general

(GAPL). This section illustrates the four airfieldslotes under publication No- ^VAIR 00-25-509,

configurations covered by this technical manual andRachet Lock Looseleaf Binder’ and COIne i" two

the individual pallets required to construct them; Eachslzes: 2 lnch mlmmum to 3 inch maximum and 3 inch

illustration is accompanied by a list of parts thatmlnlmm to 5 inch maximum. When ordering, specify

comprise the illustrated assembly. Instructions forslze requlred and "ulnber of binders "^"^Y to

use of the GAPL are provided in section XIII.maintain an orderly arrangement of manuals. Thecommanding officer of the activity shall request

SECTION XV. NUMERICAL INDEX. This sectionalditlon^ manuals, as needed, on NAVAIR Form

provides a listing of parts comprising the AM-2 mat- 5605/3^ Mailing List Request for Aeronautic Techni-ca.l Publications.

ting and related components. The list is arranged innumerical order by part number.

To facilitate identification, the model of the Mat-5, RELATED LITERATURE, ""g and the specific contents (manuals, bulletins,

etc.) shall be marked in black ink and inserted in the

Additional information on matting may be obtained window of the binder.

from the following manuals:7. CHANGES AND REVISIONS OF MANUALS.

a. NAVAIR 51-15ACA-1, Handbook, Installationand Operation Instructions, Catapult Type CE, Mark Landing mat manuals are generally brought up-to-1 Mod 3. dace on a three-month basis, when past service bulle-

tins, service changes, repair procedures, and anyb. NAVAIR 51-5EAA-2-1, Handbook, Installation, other pertinent information are incorporated. Docu-

Operation, Maintenance Sc Overhaul with Illustrated ments which are incorporated in the manual are notedParts Bres-kdown, M-21 Expeditionary Aircraft Re- on the flyleaf page. Manuals are current to the revi-cowry System, sion or change date on the title page.

2

NAVAIR 51-60A-1 Introduction

A manual CHANGE is not a complete publication; 8. RECOMMENDING MANUAL CHANGE,only superseding or supplementary pages are issued.The title page of the change contains a change notice NAVAIR Form 13800/2, Changes Recommendedand all pages show a change date in the lower corner, to Aircraft Launch and Recovery Equipment TechnicalA complete list of changed pages with their change Manuals, has been devised for suggesting corrections,

dates is given on the A-page following the title page. changes, or innovations to the manuals. These forms

The portion of the text affected by the current change sha11 be ordered from the Forms and Publications

is indicated by a vertical line in the outer margins of Segment of the Navy Supply System in accordance

the page. (This line is omitted in the numerical index.) widl NAVSUP Publication 2002. ALL OPERATINGPERSONNEL ARE ENCOURAGED TO MAKL FULL

A manual REVISION is a complete new manual USE OF ^S SYSTEM. The completed form shall be

and will supersede the entire preceding issue and its sent to the Commanding Officer, Naval Air Engineer-

changes. The revision date appears only on the title ^g Center, Engineering Dept. (Sl), Philadelphia,

page. For subsequent changes, the revision date is Pa., 19112. See Figure 1 for sample of this form.

retained on the title page, with the change date notedunderneath. The following information shall be included in

the form by the sender:

Old pages of the manual should not be discardeduntil the service changes, repair procedures, etc., The exact NAVAIR number, revision date, sec-

which have been incorporated on them have also been tion, page, and paragraph affected.

incorporated on the equipment. The newly changedpages shall be inserted to maintain a current basic The correct manual title and mat model number.

manual, but the old pages shall be kept in the frontof the manual for reference until the applicable equip- A recommended correction or revision (only one

ment changes have been made. When old pages are change to a sheet). The recommended change may

kept, ink notations shall be made on the superseding concern anything that involves the technical content

pages in the basic manual as follows: "This change of the manuals, such as correcting a dimension, an

is not incorporated into the equipment see old illustration, a specific step, or an entire procedure.

pages". Old pages reflecting actual status of equip-ment shall be separated by cardboard from basicmanual pages.

3

NAVAIR 51-60A-1 SectionField Configuration and Sit* Preparation

SECTION

FIELD CONFIGURATIONS AND SITE PREPARATION

1-1. FIELD CONFIGURATIOHS. 1-6. GRADING. The terrain in the area to be utilizedshall be leveled and rolled to provide a compactmatting base. Grading shall provide adequate drainage

1-2. The general arrangement of the field is depen- ,-of surface and rain water away from the field area.

dent on governing military conditions, local topo- ^ ^ ^^ ^ disturbed a minimum amount ingraphy, the operational requirements of the aircraft obtaining the prescribed finish to provide a soil ofbeing used, the existence (or non-existence) of small maximum bearing capacity. Any areas under the mattinglocal airstrips, etc. This section describes the four ^quiring installation of service or drain pipes orconfigurations illustrated in Figure 1-1.6 6 other objects shall be backfllled and thoroughly

tamped. The final grading operation shall be suffi-

1-3. SOIL CONDITION. The soil and sub-base ciently level so that mats when laid shall not varymaterials of the field shall be suitable for use with more than 1/4-inch in height over a 12-foot distance.

the AM-2 landing mats. The sub-base material shall Hand raking may be requited to accomplish this

have a bearing capacity relative to a minimum CBR condition. Hand raking may also be necessary to

(California Bearing Ratio) rating of 4 or firmer. The remove small rocks and other debris which wouldCBR ratings of various soils can be determined by impair the interconnecting of mats.

identifying the characteristics in accordance with a

comparable type listed in Table 1-1. The term CBR is 1’^- SURVEY. The general field configuration musta measure of the relative bearing capacity of soils be staked out in its entirety. Accurate longitudinal and

and base materials and is expressed as a percentage transverse centerlines must be established to facili-

of the unit load required to force a three square inch tate the deployment of the pallets. When no guide

piston into the soil, divided by the unit load required rail is used both lateral ""^Y ^8" must ^ ’*""-to force the same size piston the same depth into a

ate^ """ked to insure smooth linear edges from which

standard sample of compacted crushed rock. Forto lay the mat fleld- rhe hne for both edges of therunway shall be determined by use of a transit, and

complete CBR in field test performance instructions ^^y ^^ ^ ^ ^alk line or stakes. Thissee Department of the Army Technical Manual survey will also be required for taxiways and parkingTM-5-530. areas when installed. When a guide rail is installed,

only the centerline of the guide rail is established

1.4. SITE PREPARATION, by transit.

1-8. HARD SURFACE RUNWAY. Site preparation1-5. The following operations are part of the site may not be required if there is an existing concrete orpreparation which must be accomplished before mats asphalt runway. Matting will be laid over the hardmay be installed, surface.

1.1

&>ctlon NAVAIR 51.60A.1Field Configuration and Site Preparation

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1.2

NAVAIR 51-60A-1 Section IField Configuration and Sif Preparation

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s S S w i^ S w? 2? 3 d 5 S riS < o < S3 S0 a; So 0 S 8u u u 3

1.3

Action NAVAIR 51-60A-1Field Configuration and Site Preparation

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’ f1.4

NAVAIR 51-60A.1 Section IIGeneral Description

SECTION II

GENERAL DESCRIPTION

2-1. AM-2 MATTING AND RELATED COMPONENTS, piece main panel extrusions which, when weldedlongitudinally, form the same size and shape as the

2-2. The AM-2 matting and related components, which one-piece extrusion.) AM-2 matting is painted Marine

consist of keylocks (starter, typical and female), 90 Corps Green No. 23 color and the top surface is coated

connectors, mat end ramps, blast deflector adapters, with a non-skid material of the same color. For run-

aircraft tiedowns, and guide rails (for catapults), pro- ways and taxiways, the mats are installed in a brick-vide for the runway, taxiway, and parking areas rework type pattern. This staggered joint arrangement

quired for VTOL, VSTOL, SATS and EA field configur- provides the required stability across the runway,ations. Refer to Figures 2-1 and 2-2 for the relation- and the necessary flexibility in the direction of air-

ship of the AM-2 matting and related components with- craft travel.out a guide rail and with a guide rail respectively. Allpart numbers used are NAEC part numbers, b- The sides of the mat panels are constructed to

interlock with a rotating motion. The end connectors

2-3. AM-2 MATTING. (See Figure 2-3.) AM-2 matting are arranged with the prongs up on one end and down

is described as follows: on the other. Thus, by properly placing the end con-

nector of one mat over the end connector of the pre-a. The AM-2 mat, NAEC Drawing No. 615526, is vious mat, a continuous layer of matting is formed

a fabricated aluminum panel, 1-1/2 inches thick, which (see detailed installation procedure). A flat lockingconsists of a hollow, extruded, one-piece main section bar is then inserted into the slot common to the two

with extruded end connectors welded to each end. mats to form a non-separable joint. The physical(AM-2 mats may also be fabricated in two-and three- characteristics of AM-2 matting are as follows:

DWG 615526

(1) Weight (full length mat) 144 Ibs

(2) Length (full mat) 12 ft

(3) Length (half mat) 6 ft

(4) Width 2 ft

(5) Wt/Sq Ft of Coverage 6 Ibs

(6) Locking Bars

Length 24 in.

Width 5/8 in.

Depth 3/16 in.

2-1

Section II NAVAIR 51-AOA.1General Description

uz3

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i8^ IP1-2

NAVAIR 51 -60A. 1 Section IIGeneral Description

U(o t=oc. v) /I

^ S ^ /Q:(^ Q: i- / <Z (- /^ / UJ< uj \ \ /’ r,/0{3= 2 \\ v /^ ^s ^ \\ ^\ /

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2-3

Section II NAVAIR 51-60A.1Generol Description

^ ,^.------ -"’%, ..-.--<-^ :^- ^^" v ’<^ .--""" "’-,

âil :-^ ^ ’" PART NO. 615526.1. .2^rj^ D

^- END CONNECTOROI-^T.^M

z END CONNECTOR"PRONGS"DOWN bLLTION A-A "PRONGS"UP

f"^ ^7’^7 ^/"’"^ ’~^~77^7 ’’’^^ ^7"^_’7 ?~7_7~7~ /’i-1 yf ’[ u M M \ ’{ V’-’-l/ a H n [ if\// ^. ; J, J. _J_ ; A ^V/ ^/^ i’.i-n-r-r-r-1’^-T-r r-r-r"-r-n-n-T’/-r-n I’^T-r-rTTr’/’/ ’/’I I’i ’<

^-FEMALE EDGE MALE EDGE-11-SECTION B-B

Figure 2-3. AM-2 Mot Configuration

2-4. MAT COVERAGE. 2-7, TYPICAL KEYLOCK. (See Figure 2-5.) A typicalkeylock is insertedêvery 100 feet in the pattern to

2-5. The quantity of mats found in the standard permit the easy removal of sections of the matting

pallet assembly (F27) will provide a width of 3 for ""^"Ple nat replacement. Thus a maximum of

ros (6 feet) on a runway or taxiway which is 72 50 feet of ^Y one section need only be removedf. c; .1, ^.\.\ -A to replace mats that could not economically be replacedfeet wide (432 sq. ".). aince the parking and storage .r.

as individual units by replacement mats. Typicalareas need not have a specific mat pattern^ as is keylocks are furnished in 3-foot, 9-foot and 12-footrequired on the runways and taxiways. the extra" \^^ to provide for staggering of joints of mattinghalf-length or full-length mats which result from the patterns. The typical keylock is coated with a non-runway construction may be used in these areas. s^t,j material. Typical keylocks may also be usedThe use of a guide rail and/or keylocks will not alone, or in combination with adjustable keylocksaffect the amount of coverage to any great extent, and/or spacer mats, to fill the last row of replacement

matting when the row space is less than 24 inches in2-6. STARTER KEYLOCK. (See Figure 2-4.) A starter width.keylock is a very narrow mat which is used to de-crease runway installation time by approximately one ,-</-’’’<?;S>^._^--’’-^-SOCKET HEAD SCREWShalf.’ Previous mat installation methods required ^"C*^^^ \assembling the runway at one extremity and working <^:>.’’i*C ^s \to the other end. The starter keylock is installed in ^^^S:|^;^’^ ^^^^^ rMALE CONNECTOR

the middle of the runway only, and enables two mat- ^t<^^^^^<^^^(R)^::^ \laying teams to start together and work simultan- î>>^s^^^^(R)^S^?s^sêously toward each end of a runway section. Starter ^’^S^^^^^S ^^^^s.keylocks are furnished in 3-foot, 9-foot and 12-foot ^^^^^^ ’^C"^^^)lengths to provide for staggering of joints in matting T^^SÎt’’?^patterns. The starter keylock is coated with a non. MALE CONNECTOR-/ ^^^^^skid material,

p^ ^ 4,3370.^ .3 . ^^^Not 508389-1, -3, -4 CONNECTOR BAR-/417034.1, .3. .4

The starter keylock is not used in the por-

tions of an installation having a guide rail. Figure 2-4. Starter Keylock

2.4

NAVAIR 5I.60A-1 Section 11General Description

/’-SOCKET HEAD SCREW ./’’^SJ^â!!.,.^^f^’’*"^.":’"’^^^^. /-MALE CONNECTOR /Wî ^!’’^|^(R)3;^^

FEMALE CONNECTOR-’ ^^%,^^S^ri<’’’^^^ y^3^:â’’’’/"^^^

PART NO. 508389-1, -3. -4 ^^^|^||pl’IffiillS^

^ r^S:s;y ^rp^^ ^^ 415040.1

Figure 2-5. Typical Keylock ^^ss:^

2-8. FEMALE KEYLOCK. (See Figure 2-6.) A femalekeylock is used to join two adjacent male mats. The Figure 2-7. 90 Connector (H Type)female keylock is coated widi a non-skid material.

2-10. ADJUSTABLE 90 CONNECTOR. (See Figure2-8.) The adjustable 90 connector is used to jointwo matting patterns that are adjacent to each otherat a 90 angle, such as the main runway and a taxi-

SOCKET HEAD SCREWS^ way. This connector is also used to join additional^^’’’^^M^^^ \ FFMAI c matting or mat end ramps to the ends of the runway^’^^^^^’v^^^ fciwMi_c ûnjNtCTOR

-’’’<^^ \ where a catapult guide rail is installed. Connectors(^îM^^ff^;^.^^^^’’’:^;^^^ are 12-foot long aluminum sections which can be

^^^K^K^^^^^ adjusted in width from 6-1/2 inches to 9-1/2 inches^’!/^^^^^tet^s~aK::’;Y!y to facilitate the joining of two adjacent matting

r’^^^^g^^^^^ "ctions.

-FEMALE CONNECTOR ^^^say ^-v.,^FEMALE KEYLOCK____-// y ^^~~^--_

^CONNECTOR BAR /~,^^^ <^^~-~.,_~~’^^y ~~^PART NO. 417034.1, .3, .4 /"’>^><^^^:::;^^^-^^

511875.1, .2 /-^ ’^^’- ^-^^’^^Figure 2-6. Female Keylock V^S> ^^."^’^^./ .^y

^" ^^^^--’ây’ ,^r /-PRONGS UP END2-9. 90 CONNECTOR (H TYPE). (See Figure 2-7.) ^’Î::^^^^^^ / KEYLOCK ASSEMBLY

The 90 connector is used to join two matting pat- ^’’^^W ^-.-^’"--^ ^>terns that are adjacent at a 90 angle such as the K^LOcS ASÊMILY .<’"^<^--^’ ^^^Lrunway and a taxiway. It is also used to join addi- l^--’^*’^"^. / / ^’.^"tional matting or mat end ramps to the ends of the ^^^^^’^(yyy^runway where a catapult guide rail is installed. Con- PART NO 513850.1 -2 ^’"’"^’’’SL ^^nectors are 12-foot long aluminum "H" sections 616095.1which allow relative movement and slight misalign-ment between the adjoining sections of matting. Figure 2-8. Adjustable 90* Connector

2.5

Section II NAVAiR 51-60A-1General Description

2-11. MAT END RAMP. (See Figure 2-9.) The mat rows of matting. Ramps are fabricated from aluminumend ramps are used at the ends of runways, laid on a extrusions either of the open extrusion type or thehard surface (concrete), to smooth the passage from closed extrusion type as shown in Figure 2-9. Rampsone surface to the other. The edge connection between arc drilled and tapped to allow die ramp sectionsramp and mat sections is die same as between two to be joined and anchored.

’^^^^^^^^^ PART NO. 615074.1

CLOSED EXTRUSION TYPE

^^^^/.^.^-.^s^^L^-^^ PART NO. 612717-1

OPEN EXTRUSION TYPE

Figure 2-9. Maf End Ramp

2-6

NAVAIR 51-60A-1 Section IIGeneral Description

2-12. BLAST DEFLECTOR ADAPTER. (See Figure2-10.) The blast deflectors are provided to protectthe area surrounding the airfield from the blast of ^^~~---’~~-~>^the engine exhaust. These deflectors consist of

RING ^ ^^^^nv ’^^"^\mat sections held at about a 60 angle to the hori- .^^---->- ^\zontal by blast deflector adapters, which are two /^^ .st^’^^’ ^^\ ]feet in length. Blast deflectors and adapters can be \^^ --y ^^^~--^^^ Ainstalled along the edges of the taxiways and park- ^^^’ ’’~~-~~^ ^~7^Xing areas but are not used along the runways. / ~~~~~~~~- 11 ^^~~1

Type I adapter joins to the male edge of the matting V^-. ^^/ ^\and to the female edge of the matting. Type II joins ^--^---^

v RING RETAINER

to the prongs-up end of the matting. Type III joinsto the prongs-down end of the matting.

2-13. TIEDOWNS. (See Figure 2-11.) Tiedowns are Figure 2-71. Tiedownprovided for aircraft anchorage and are bolted in

place on the site by drilling and tapping the neces-

sary holes in the AM-2 mats. according to aircraft 2.14 GUIDE RAIL. (See Figure 2-12.) When a cat-configuration, in the parking areas, apult is used, a guide rail may be required to provide

stability to the dolly and aircraft during the launch.

^^(fl^^^ The guide rail is supplied in 9 and 10-foot lengths-^’’’S^^^^^^^ an(^ âs connectors on both sides to mate with the

^.ff^^^^^^^^^ mat ^ connectors. A 1/8-inch rubber seal is in-^’e^sy ^^^^^^^^^^/^ stalled between each section to provide for thermal

^.(-g^^^^^g T^-^^1’**^ ^rexpansion and to prevent debris and soil from coming

^^g^^^^^^^^ ’^^ ^^^ up between the rail sections. Dowel pins are used be-,^^^^^^^^^’y^-^^^’^ tween two mating holes in each end of the guide

^/ .^’^^^^’^/^^^ PART NO. 416875-1 rails to maintain alignment of the sections. The guide^sgy fsf^ ,^^ rail is installed concurrently with the mat field, andY’91^ / ^^- standard mat locking bars are used to secure it to

the mats.

,^:’?^^^^^^ 2"15- REPLACEMENT MATS. (See Figure 2-13.)

^^^^^^^^^^^ Replacement mats allow for the replacement of dam-

^^^^^^^^^^^^/ aged mats with a replacement item that duplicates the

C9" ^^^^^^,,/-’ PARTÔ. 416876-1 r(STOWEO POSITION) -<^^^^^0

/^ 5^^^^^"^ PART NO. 416877.1 ’^ ’i^^^^DOWEL PIN

<^ îr ^’ ^$^ ADJUSTING SLOT

Figure 2-10. Blast Deflector Adapters Figure 2-12. Guide Rail (Catapult System)

2-7

Section II NAVAIR 51-60A-1General Description

_^---^^’"-^ ^\ SOCKET HEAD

^ -, ’-v^ CAP SCREW

SETSCREW----.S^,--^ "-..sa*’^^^^^^^^^^^’^ MIDOLE-YLOCKING BAR"’""’^ "^^^^^^^^^^^^^’^ADJUSTING HOLE /^^^^^^’^. N-MALE CONNECTOR

X \ PART NO. 508387-1LOCKING BAR SOCKET HEAD SCREW

Figure 2-13. Replacement Mat

original installation, re-establishing the beam con- also be disassembled and saved as prepared replace-cept and requires only the removal (by cutting) of merit mats for the next installation.the original damaged piece. These mats are completewith a non-skid coating. Replacement mats are pre- 2-16. HEAVY DUTY MATS. (See Figure 2-14.)pared from AM-2 mats by cutting off the "prongs-up" Heavy duty mats are provided under arresting cablesedge and the male connector edge, and welding on to eliminate excessive dents and other externaladapters. Additional adapters must be bolted on damage that occurs to regular matting during air-at the time of installation. In case of site disassem- craft arrestment procedures. These mats are alsobiy, replacement mats may be disassembled and used installed on each side of the guide rail and serveas standard mats without further alteration. They may to reinforce the guide rail and provide a firmer

^^^----^^’"^^’^ ^^^ PART NO. 513579-1

Figure 2-74. Heavy Duty Mat

2.8

NAVAIR 51-60A-1 Section IIGeneral Description

/-KEYLOCK ;-MALE/ C ^DCIA/ / ACCC’kJOi^/nc, ^wL Ivl DLT ^ ~^^--^.

^-^^^^^" ^^ ’"---^^-^^^^ </<^^’’^-,^^^^ PART NO. 511871.1 (MALE)â;:^^/ ^^-^^^^^ ^^^^^^^^^ 511875.1 (FEMALE)

Figure 2-75. Adjustable Keylock Assembly

surface for the launch dolly. These mats are 6 feet in width. These mats maybe used alone or in combinationlength and 18 inches wide after connectors are with typical keylocks and/or adjustable keylocks.attached. Heavy duty mats are painted Marine Corps Spacer mats are furnished in 6-foot and 12-foot lengthsGreen No. 23 color and the top surface is also coated and are 12 inches in width. The spacer mat is coatedwith a non-skid material of the same color. Locking with a non-skid material.bars used to secure heavy duty mats together are

approximately 6 feet in length. 2-19. EDGE CLAMPS AND STAKES. (See Figure2-17.) Edge clamps are provided to secure AM-2

2-17. ADJUSTABLE KEYLOCKS. (See Figure 2-15.) matting at aircraft taxiing and parking area turningAdjustable keylocks are provided to fill the last row points. Stakes anchor the edge clamps to the mats byof replacement matting when the row space is lessthan 24 inches in width. These keylocks may be Note

used alone or in combination with typical keylocksand/or spacer mats, depending on the width of the Quantity and location of edge clamps may

row space. Adjustable keylocks are furnished in 3- vary for a ^^"^ installation, depending

foot, 6-foot, and 12-foot lengths and can be adjustedon s011 and ^"’"""ntal conditions.

to expand from 6 to 9 inches in width. Right and left^^^âdjustable keylock assemblies are comprised of a ^-^’^^"^^ ^^S.

combination of 6-foot male and female keylock as- sS"’^^’^ ^^s.semblies. Expansion in width of these keylock as- ^---’"^^^"^V^ ra.semblies is controlled by a keylock screw in the male S^^ ^^^^"^ .ss^^HiTkeylock assembly which rides in a slot in the female ^^V ^\ y^-^^^^^^^^^^keylock assembly. Adjustable keylocks are coated with ^^ ’\ -rf’^^î^’^^^â non-skid material. ^^. \, ’’_-aSS^^^^^^^^^

2-18. SPACER MATS. (See Figure 2-16.) Spacer mats’"’i^S-- p^^ ^ 615286.1, -2

are also provided to fill the last row of replacementmatting when the row space is less than 24 inches in Figure 2-16. Spacer Mots

2-9

Section " NAVAIR 51.60A.1GenTol Description

EDGE CLAMPS

^.^PART NO. 512596.1 / /////

TYPE

PART NO. 512597.1 ///y//

TYPE 11 r "’-j

^ |f4pPART NO. 512598.1 / //.///

// &>’

TYPE III

PART NO. 512599-1 //U/ / t | PART NO. 512600.1

TYPE IVSTAKE

Figure 2-77. Erfge Clamps and Stakes

being driven into the ground. There are four types of Type III edge clamp anchors downturned prongs ofedge clamps which are as follows: mat (see Figure 7-22); and.

Type IV edge clamp anchors upturned prongs ofType I edge clamp anchors female edge of mat mat (see Figure 7-23).

(see Figure 7.20);Type II edge clamp anchors male edge of mat (see Short locking bars are used to secure Type III and

Figure 7-21); IV edge clamps to the matting.

2-10

MAVAIR 51-60A-1 Sct(n 1Packaging

SECTION III

PACKAGING

3-1. GENERAL, assembly consists of 11 full-length mats, 2 half-lengthmats, and 13 locking bars. The other standard pallet

3-2. Table 3-1 is a list of package identification num- assembly contains 16 full-length mats, 4 half-lengthbers, with drawing numbers, necessary tor installation mats, and 20 locking bars. The pallets are fabricatedof the field configurations covered by this technical end frames (spot welded or fillet welded) which aremanual, held together either by tie rods or strapping and seals.

The end frames retain the ends of the mats and serve3-3. MAT PALLETS (FULL LENGTH) Fll, F15, as a storage area for the locking bars. Figures 3-1 andand F27. AM-2 mats are packaged in two standard 3-2 show exploded views of mat pallets designated Fll,pallet loads for shipment and storage. One pallet F15 and F27.

LIFTING EYE-~Sl----."^agS^^C P^^^K^^^(R)^^.- /-FULL LENGTH MATS (IZ FEET)

Th^^s-Afcs^ / (II PER PALLET)

SEE DETAIL A"-/I ^^^^^B,-;.SBft^ ft^ ^\

SEE DETAIL "B"-/ ^^^^^^FS%(R)^%S’K

HALF LENGTH MATS (6 FEET) -’^^^^^^^y^l!!^’^?^!^

^^^^^^ft^ ^^^^^^^^^^’^^^’T" WOOD FILLERS4" X 4" BLOCKING -------.^^^^^^^ i.’^^^^1’ /

(NOT PART OF PALLET) ’"^^^^^^^^^//JAM NUT

LOCKING BAS---^^;^^^.^^|yGtN--^’(13 PERPALLET) ^r^^^.1’ --^--’^’ V801’1m\U <> --’’""^ (TORQUE TO

LOCKING PIN----i ^^, LB-FT)

yCsfFLAT HEAD PIN-’ I-END FRAME

^-ENOFRAME ^-ENDFRAME\.^ \. 1-LOCKING PIN

" i-i. r-TIE ROD r 1/------qt--

c^^^^^ F-^Y^’ ^^.^^pLL--V \-JAM NUT L^-

\ \ t--FLAT HEAD PIN’--BOLT

\__-Qge DETAIL 8

OETAIL-A" TIEROD CONNECYION

TIE ROD CONNECTION

F/gure 3-7. AM-2 Maf Pallet (Full Length) (F11)

3.1

teSil’j NAVAIR 51-60A1

^ E S2 .1<t < /-._J (D 0- / 0

10 =^ 0 0: / gI- n- 2 U y-----------\ /

^ I s ^ \ \ y ^^ ^ ^L2i /’A\ \ \ ^ SLjt: 5^ ^ S<^ (>\ \ \ V ^S ^ ^ ^-^; ^^ ^^d^_A--^ 5^

=! ^ ^^||!^|^ m ^_i /^?;?;h^::^;i::^;v ^ / Uuj o u^2 /y’ ^WSW^^ / C \ ^d ^^ .^A’^^ssy^/ ^ -^ \ \ \ \i 2 ^^^;:^^^^ ^ / ^ \ \ \ V ^a ^

g ^^^^/.-y 7 tn -J

^ ^ / s2< / .’ CDa / a:1- / QU<rt z Q_

u o0 cy

3.2

NAVAIR 51-60A-1 i*^’0" 1"Pockoginfl

3-4. HALF MAT PALLET, F12 and F32. Half mat F32 pallet (see Figure 3-4) contains 18 half mats and

pallets are of the same type and arrangement as full- 20 locking pins. The end frames are clearly marked to

length pallets (see Figures 3-1 and 3-2), except for indicate their use for 6-foot mats. The end frame for

being only half as long. The F12 pallet (see Figure the F32 pallet is fillet welded.

3-3) contains 12 half mats and 12 locking bars. The

r-END FRAMEr- END FRAME \ --LOCKING PIN

L3i [-TIE ROD Fr-Y-’1^^’^^^^^^L. ^, L TIE ROD

^ I1-JAM NUT ^---L--FI.AT HEAD PINBOLT DETAIL "B"

--30SS TIE ROD CONNECTION

DETAIL "A"TIE ROD CONNECTION

LIFTING EYE

/-’-^^^^^\ HALF MAT (6 FEET)

SEE DETAIL ’^--^^ ^^BSI^^ (12 PER PALLET)

4"X 4" BLOCKING<:^^^^^gg|||^(NOT PART OF ^^^^^^?1^---"/FILLERS

LOCKING BARS’^S^ llt/ ’P----’’-^^ ^’-^^--^(12 PER PALLET) W ^^-^"^ "^ (TORQUE

’" -’""--" ^ >^ TO 40-45

LOCKING PIN---i ^^-I-S-F1’^

/^^FLAT HEAD PIN ^END FRAME

Figure 3-3. AM-2 Mot Poef (Ho// Length) (F12)

3.3

section w NAVAIR 51-60A-1Packaging

’^^l-^^^^ ’^ /- HALF-LENGTH MAT (6FT)

^ ^"irni li i ^ |!K\ / C8 PER PALLET

^^^ ^ ’^^ %S ISBB8&^ ^- WOOD FILLERS

LOCKING BARS-7(20 PER PALLET) Y^ ^^

END FRAME-^ > ^--^ss!ss^(FILLET WELDED) ^ viss^"’

Figure 3.4. Half Mat Pallef (F32)

3-4

Section III NAVAIR 51.60A-1Pockoging

3-5. KEYLOCK PALLET, F13. (See Figure 3-5.) one 3-foot female keylocks. The 9-foot and 3-footStarter keylocks, typical keylocks and female keylocks sections of keylocks are standard 12-foot lengths cut

are packaged in the same pallet. The package is desig- into two sections. Additional 9-foot and 3-foot lengthsnated F13. Each pallet contains nine full-length starter therefore may be readily fabricated in the field if

keylock assemblies (keylocks and connecting bar), necessary. The keylock sections are contained in the

one 9-foot and one 3-footstarter keylock, 60 full-length pallet by utilizing standard AM-2 mats as top and Dot-typical keylock assemblies (keylock plus connecting torn covers. Two socket head screw wrenches are in-

screw), ten 9-foot typical keylocks, ten 3-foot typical eluded to connect keylock sections along with two

keylocks, nine full-length female keylock assem- special tools for removal of typical keylock sections.

blies (keylocks and connecting bar), one 9-foot and

y-SEE DETAIL"A" ^--- END FRAME

/ ^-LIFTING EYE \ /-- LOCKING PIN

^B^(R)^^^^(R)^^^ FLAT HEAD PIN

:^^^?S^::^^.^^^w;yS^ ^FULL MATS TOP DETAIL "8"/1^ ^N^^1;.;:’^:’N;K;^^^:^^^ / AND BOTTOM TIE ROD CONNECTION

^-SEE ^^^^^^1^^^%8CT t^ IS-^ (l) 9-FTDETAIL’R’’S:;^^^^^^^"S^;^ AND (I) 3-FT

’;^^^^^^|^?^\^Si? FEMALE KEYLOCKS/l^^^^^^^|f^H;^:.^.S^ (IO)9-FT AND (IO)3-FT /

4"X4" BLOCKING /^’^^^^^^S.IB;;!;^ TYPICAL KEYLOCKS? /

(D3-FT AND (I) 9-FT .^^^^^^IKSS^1^^^^^^’’^/^^STARTER KEYLOCKS-^^ ’S^^^^^p^^^g^ / / FILLERS

^-END FRAME ^^^^^1^B^^ ^JJ ^l’^10P i ,__TIE ROD (9)12-FT STARTER ..^^^^^^^V ^S^S tiM^l ^->\^~^ \ "E ROCI KEYLOCKS-^^^^^^g 1^ t;-:::-:^ ^liL3^^ ^^^^^^- (60) 12-FT TYPICAL /^^^ A’ W --^^^7^ ^N. V"’^’^01’ KEYLOCKS-^ A ^

<k ’^’^’^Y /\^-BOLT ^ -^--’’ ’S’^--’-. ^BOLT\ 1/4" SOCKET HEAD ^^^ ff{^ (TOROUF’-- BOSS SCREW WRENCH --^_^^ ’’SB^, ,^--^

H’ORQUE

DETAIL "A" LOCKING F>IN-’"^^. ^ -^^S^^ LB-FT)

TIE ROD CONNECTION FI.AT HEAD PIN ^^ C^^^^’ ^^ REMOVALTOOL

Figure 3.5. Keylock Pallet (FJ3)

3^

Section III NAVAIR 51-60A-1Packaging

3-6. ADJUSTABLE 90 CONNECTOR PALLET, F31. standard half mats as top, bottom, and side covers.

(See Figure 3-6.) The adjustable 90 connector pallet, Wood fillers divide the adjustable connectors into

which is designated F31, contains 42 adjustable con- 3 rows of 14 connectors each and serve to furnish

nectors and 4 half-length mats. The 6-foot adjustable additional protective rigidity.connectors are contained in the pallet by utilizing the

__CC" A

ff ^8ttl8MKM^^< ^HALF LENGTH MATS (6 FT)

/n4 PER PALLET

^ ^Y^000 FILLERS

STRAPPING-^ \, ^ I ^^^ifi^ /

ADJUSTABLE 90 CONNECTOR (6 FT)-/ /-"’ ^^^^^^S^’^^(42 PER PALLET) / x .^r ^’sis ----^’

WOOD FILLERS-lr \^ ^1

END FRAME-^^ [JLg? ^^ff^(FILLET WELDED) "^

Figure 3-6. Adjustable 90 Connector Pallet (F31)

3-4

NAVAIR 51-60A-1 Section 411Packaging

3-7. 90 CONNECTOR (H TYPE) PALLET, F14. support piece is used along the bottom longitudinal(See Figure 3-7.) The 90 connector package desig- edges of the pallet to supply additional protective

nated F14 contains 42 connectors. A special steel rigidity.

i^lB^fl^MNH /- 900 CONNECTORS (12 FEET)

\ ^1^ ^:^::- ^NAIL-. ^S -^-1^5 ^^^ ^-^ ^ -" \ "^’-^ /\^-"\-^ Y /

V. BOLT

LOCKING PIN--’ a\^. ’^^C^^^FLAT HEAD PIN -^ \-END FRAME

Fgure 3-7. 90 Connector (H Type) Pallet (F14)3.7


3-8. BLAST DEFLECTOR ADAPTER PALLET, F18. 120 type II adapters, 120 type III adapters and 240(See Figure 3-8.) The Blast Deflector Adapter pack- locking bars.age, designated F18, contains 200 type adapters,

A- LOCKING BAR

/ ^^^ ^^^--^ X / ADAPTER /. ^

^ ^!^^^^ ^n^..^^^^ ^LOCK WASHER -- j(R) ^==^^ ^^_ ^^"^^Sr ’Sy

Figure 3-8. Blast 0^cfor Adupfr Pallut (F18)

34

NAVAIR 51-60A-1 Section UPackaging

3-9. TIEDOWN CONTAINER, Fl. (See Figure 3-9.) downs and the necessary screws, drilling, and tappingTiedowns are packaged in FSN8140-038-9894, desig- equipment.nated package Fl. The package contains 120 tie-

/---^ ./--LID

^

Fl (120 TIEDOWNS)

Figure 3-9. Tie</own Container (Fl)

3.9

Section III NAVAIR 51.60A.1Packaging

3-10. EDGE CLAMPS AND STAKES PALLET, F28. Total amount of edge clamps is 130. There are also(Sec Figure 3-10.) The edge clamps and stakes pallet 80 locking bars which are secured in the top open endF^o consists of an open frame base assembly which of the stakes (approximately 20 bars in each of 4holds 120 stake assemblies. All edge clamps are stakes). Locking bars are taped together in accord-retained on the shafts of the stakes (Sec Figure 3-10). ance with good commercial practices. The stakes areThere are 25 each of edge clamps Type and Type 2, retained in the pallet by strapping and retaining barsand 40 each of edge clamps Type III and Type IV. (see Figure 3-10).

TYPE I-MALE END // ^^^^^^^3toJ’ [^T^rSSr ^ ^------LOCK WASHER

EDGE CLAMP SIDE ^^^a’^.g^’ ’-LOCKING BARSTYPE IT-FEMALE ENO L.BASE ASSEMBLY (80 PER ^LLET)(25 PER PALLET)

Figure 3-10. Edge,Clamps and Stakes Pallet (F28)

3-10

NAVAIR 51-60A-1 Section (II

Packaging

3-11. HEAVY DUTY MAT PALLET, F26. (See end frames and the locking bars are placed in theFigure 3-11.) Ihe heavy duty mat pallet, designated exposed connector bar slot of each heavy duty..mat.F26, contains 16 heavy duty mats and 16 locking These locking bars are also secured by strapping andbars. The heavy duty mats are placed vertically in (he seals of the F26 pallet (see Figure 3-11).

r-- END FRAME

/-LIFTING EYE _\ I-- LOCKING PIN

\ ^ 3-^^’’’^^^^^^^^^ L .-~i-- FLAT HEAD PIN

^^^^^^^^^^^^’"’^-STRAPPING TIE ROD CONNECTION

/^ ^ \ ^^^^^^^^^(R)^ ^^~HEAVY DUTY MAT C8 IN- x e^-)

//V 811W: S --*-^^?? ,>-WOOD FILLERS

TIE RODS^ \|JJB Jipl ^^ ^ / ^^ NUT

-<- END FRAME .--------’’’’^^^ 1

1,-^^^ ^-TIE ROD LOCKING PIN-^^ .^^^ ^^^^^ ^^^^^^ ^ /-T \ ^JAM NUT ^ ^^J ^BOLT

’--^ .^^ ^ -^’:^:::::^ ^O^S1--BOSS FLAT--"’""^ V^^l LB-FT)

,/ ZEND PLATE

TIE ROD CONNECTION ^END FRAME

Ff-gure 3-11. Heavy Duty Mat Pallet (F26)

3-11

Section III NAVAIR 51.60A-1Packaging

3-12. SPACER PALLET, F25. (See Figure 3-12.) full-lensth AM-2 mats, serving as the top, bottom, anThe spacer mat pallet, designated F25, consists of sides of the pallet protect and contain the space25 spacer mats (12 feet long) and 6 spacer mats (6 mats. The end frames of the spacer mat pallet ar<feet long) stacked in two rows of 14 each. Four ^l16^ welded.

^^-T-\ /-SEAL

S. ’^ÎSIIî^^ ^-FULL LENGTH MATS (12 FT)

^ ^L ^^^^î^^^J^^N / TOP, BOTTOM, AND SIDES

STRAPPING-’ \< ^^^ ^îNl^yil ^ 1^^\. ^^ ^NÛ iti lJl^’^.t ..T-WOOD FILLERS

SPACER ASSEMBLIES-7 ^ ^.-^^^^^^ /-"’s-^""^(6 PER PALLET 6 FT \ ^^^^^^^’^f^^(25 PER PALLET -12 FT) x^^;-^^^^^s^ _^-

LOCKING BARS-^ \ ÊND FRAME-" ^f^’*^^^(FILLET WELDED) ^^

Figure 3-12. Spacer Pallet, (F25)

3.12

NAVAIR 51-60A-1 Section IIIPackaging

3-13. ADJUSTABLE KEYLOCK PALLET, F29. full-length AM-2 mats also enclose the adjustable(SeeFigure 3-13.) The adjustable keylock pallet, desig- keylock assemblies (see Figure 3-13). Adjustablenated F29, consists of 20 each of right and left keylock pallet end frames are either spot welded or

adjustable 12-foot keylock assemblies, 2 each of 6-foot fillet welded. Spot-welded end frames have differentmale and female keylock assemblies, and 4 each of wood fillers than fillet-welded end frames.3-foot male and female keylock assemblies. Four

^y^^dj^a ii%t^\ ^FULL LENGTH MATS (12 FT)WOOD FILLERS ^^N:^(R)!^!!^ / ^OP, BOTTOM, AND SIDES

\ ^ <^^"1 MALE KEYLOCK ASSEMBLY-^" ’"^ ’^^ C^ --ax

\ (2 PER PALLET-6 FT) \ -ZJ Z-^ (C^ s^S^^ \^K (4 PER PALLET-3 FT) -\ ^’’S^S’^^^ ^ \

^ _J FEMALE KEYLOCK ASSEMBLY \ .^V^ \/ ^k ^^’ (2 PER PALLET-6 FT) \ ’-^-H ’\ ?^ \LWQOD ^k. ^^ .^--^’ (4 PER PALLET-3 FT) )’/^^Vf -’ \ ^^\

/r RIGHT ADJUSTABLE KEYLOCK ASSEMBLY^ V" ^^^^-^-sSs?^’^’^/ (20 PER PALLET-12 FT) /\. .-^-^fii. S?-’’"END FRAME-7 LEFT ADJUSTABLE KEYLOCK ASSEMBLY / ^\,->--^ Lf^ ---^’&. ^"^^(SPOT WELDED) (20 PER PALLET-12 FT) / j /-^

WOOD^^ ’->\<FILLERS ^^/’ ^---^"

END FRAME^ ^^^^(FILLET WELDED) W^^

Figure 3-13. Adjustable Keylock Pallet (F29)

3-13

Section III HAVAIR 51-6CA-1Packaging

3-14. MAT END RAMP PALLETS. (Sec Figure are held together by tie rods. The end frames retain

3-14.) The mat end ramp pallet contains 9 mat end the ends of the mats.

ramps. The pallets are fabricated end frames which

^-1\ ^- LIFTING EYE

LOCKING PIN--^3 ^N^1’,.^----’^^

T C-^^^Y- \-ENO FRAME

\ ^^-BOLTFLAT HEAD PIN -1

Figuf 3-14. Mor End Ramp Pallets

3-14

NAVAIR 51-60A-1 Section IIIPackaging

3-15. REPLACEMENT MAT PALLET, SF1. (See sizes of socket head screw wrenches are includedFigure 3-15.) Replacement mats are packaged in the with the pallet for mat disassembly and assemblysame manner as the" basic AM-2 mats. There are 12 purposes. Pallets containing full-length replacementmats to a pallet. Locking bars and the "prongs-up" mats are designated SF1.adapters are assembled to the mats. Two each of two

SEE DETAIL "A" V-END FRAME/ \ i--- LOCKING PIN

/ r^--- LIFTING EYE F \//---’3,/

f ^ Es|:;:^^ -J --TIE ROD

^- ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ S SEE DETAIL B ~T_ fLAT HEAD PIN

^^v, .^--’’’’"^ DE TA L B

.^T^^^^1 /; ’^’^^"’^^ ’K TIE R00 CONNECTION

’^^^^^^s|^^^ /-FULL LENGTH REPLACEMENT MAT\]^^^^^^^^^^ X X (12 PER PALLET -12 FT)

TIE Roos ~~^~~ "^^^^^^^ ^\4X4 WOOD ^^^^^^^ ^Y^----^-^’^^BLOCKING ^^^^^^!S. :/ /::’^^^^ FILLERS

(NOT PART OF PALLET) ----^ ^^^^^^ ’^^^^ ^ts. //

’’ LBOLT ^^ <^ -^LTRDcq^^ \ \ ITOROUE TOBOSS J 40-45LB-FT)

--BOSS ^ -^ \ \LOCKING PIN -^ ^ "^ \ \ ^/ ^’ \ \ END FRAME

DETAIL A FLAT HEAD PIN-^ \ \TIE ROD CONNECTION \ L SOCKET HEAD SCREW

\ WRENCH (5/32 SIZE)

^SOCKET HEAD SCREWWRENCH (5/16 SIZE)

Figure 3-J5. Replacement Mat Pallet (SFJ)

3-15


3-16. REPLACEMENT MAT PALLET (AM-2 MOD 4), i" a pallet, 4 of which serve as the top, bottom

SF2. (See Figure 3-16 Replacement mats (AM-2 and sides of the replacement mat pallet, designated

MOD 4) are packaged in the same manner as the AM-2 SF2. The end frames are fillet welded.

MOD 4 half mats (see Figure 3-4). There are 18 mats

s] \^\)^’ ^ w ^s; ^^V\ /-FULL LENGTH REPLACEMENT MATSS S*. ^. N^ H^ ^^ ^^I’YS, / CS PE" PALLET 12 FT

STRAPPING-^ \ ^^^ N^^ ’? .^(R)S 1^\\ ^^ ^^H ’.^^S Wi^\. yf-WOOD FILLERS

END FRAME-’^ ^ ^ ^^ ^^--’(FILLET WELDED) ^^^^ \^ ’-^"^

SOCKET HEAD SCREW--’" ^8’’88 /WREiMCH (5/32 SIZE) /

SOCKET HEAD SCREW-!WRENCH (5/16 SIZE)

Figure 3-16. Replacement Mat Pallet (AM.2 Mod 4) (SF2)

S.M

NAVAIR 51-60A-1 Section (IIPackaging

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3.17

teS;;^ NAVAIR 51.60A.1

60

D; ^^ 3 ^ ?- % % 3 S5 S> y. .B

^ "^ N1 rt’i u"<1/1

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3-18

NAVAIR 51-60A.1 Section IVTools and Equipnrnt

SECTION IV

TOOLS AND EQUIPMENT

4-1. GENERAL, and to position matting for repackaging), brooms (forcleaning out the interconnecting grooves), and small

4-2. The AM-2 mats (full length and half length) have hammers (for driving the locking bars). A pavementbeen designed so that no special tools are required breaker or sledge hammer is required for drivingfor their normal installation. However, tools listed in holddown stakes. Cutting and welding equipment willTable 4-1 are required for related components, prepara- be required for removal of individually damaged mats

tions and adjustments, in preparation for installation of replacement mats.

Tiedowns require drilling and tapping equipment plus4-3. MISCELLANEOUS TOOLS. The hand tools re- three sizes of hex keys that are packaged with thequired consist of rakes and shovels (for final grading), tiedowns.adjustable wrenches (for pallet breakdown), crowbars,sledge hammers and 4 by 4 (or larger) wood blocking(for shifting and aligning of mats already in position

TABLE 4-1. LIST OF SPECIAL TOOLS

Item Part No.Nomenclature Use IllustrationNo. No. Req’d

Key "T" Handle Wrench 415531-2 1 For installation of ^-sss^^^^W5/16 Hex. Packaged In keylocks ><^ C\~----Keylock Pallet F13 tfCa^^ VrJ

2 Drill Fixture. Packaged 509044-1 10 For drilling holes \in container Fl for tiedown screws --AK^^ ,1

^y ^^i "^3 Removal Tool Packaged 420235-1 2 For removal of ^^^-*>^ ---"’.^

in Keylock Pallet F13 typical keylocks ^^ ’v^^’"^’

4.1

Section IV NAVAIR 51 60A-1Tools and Equipment

TABLE 4-1. LIST OF SPECIAL TOOLS (Cont’d)

temNomenclature

part ’,, Use IllustracionNo. No. Req d

4 Socket Head Screw 616205-7 2 For installation of

^ ---S^^Wrench. Packaged in end adapters in JJIJ ^-’^^^^^s^^Replacement Mat Pallet replacement mats Nv^^^fSS^^^^

5 Socket Head Screw 616205-8 2 For installation of Iffi -^^^^^^Wrench. Packaged in locking bars in ll^S^^^^^’’^Replacement Mat replacement mats ^^’Pallet SF1

6 Stake Driving Tool 509595-1 2 For anchoring --=< 3 ^edge clamps -?s^^-’^..-^

4.2

NAVAIR 51-60A-1 Section YPallet Deployment

SECTION V

PALLET DEPLOYMENT

5-1. DEPLOYMENT, provides an efficient arrangement (see Figure 5-1’).Deployment of pallets along the runway centerline is

5-2. Deployment of pallets should be such as to keep an alternate deployment method with the averagemanual handling and carrying of mats and related corn- walking distance from pallet to mac placement beingponents to a minimum. Deployment should be con- nearly twice as long as the 8- x 24- foot arrangement

sistent with the available equipment, manpower, and (see Figure 5-2).

the conditions under which the installation is under-taken. b. Distribution of the starter keylocks, typical

keylocks and female keylocks can be accomplished5"3. METHOD, for any one section, such as a runway or parking area,

utilizing a forklift truck and dropping off the appro-5-1. Pallet deployment may be accomplished by priatc number of pieces at the required intervals in

either of the following general methods, the spaces between the mat pallets.

5-5. FORKLIFT TRUCK DEPLOYMENT. Deployment c. If a guide rail is to be laid as part of the run-

of pallets by rough terrain forklifc trucks is by far the way, it is assumed that due to the close tolerancemost desirable method. The forklift truck delivers the required, the position of the complete length of guidepallets directly to the mat laying crews. Pallets are rail would be established prior to mat laying and thatdisassembled while on the forklift truck and the truck guide rail alignment would then be checked and cor-

remdins until the pallet load has been installed. This recced as needed as the mats were attached. (Actualmethod of deployment assumes that a sufficient number laying of the guide rail will be in approximately 50-of forklift trucks will be available to continuously Coot increments.) The establishment of the guide rail,supply the laying crews, with consideration for the because of its off-center position, requires distinct

round trip time between the work area and the pallet "iat pallet deployment patterns.

storage point. Pallet disassembly is preferably doneat the work area rather than at the storage area since d. F’or a 96-foot wide runway, the guide rail divides

loose macs are more subject to spillage during the the runway into a 78-foot and 18-foot strips. To pre-

trip from the storage area to the work area. Deployment vent major displacement of the guide rail, the mat

of less frequently used items makes the forklift truck laying procedure should proceed at an equal pace on

a practical necessity. Items such as starter keylocks, either side of the rail.

which in some installations are used only a few times

at positions several thousand feet apart and typical 5-7. VTOL AIRFIELD MATTING DEPLOYMENT.keylocks, used every 100 feet or more, are examples.Tiedowns and 90 connectors are also in this category. 5-8. The VTOL airfield matting (see Figure 5-3)

covers an area 72 feet long by 72 feet wide. Deploy5-6. ON FIELD DEPLOYMENT. Deployment on the F27 pallets in two parallel rows which are 25 feet on

field may be performed by the following procedure: either side of the centerline. Each row should contain

8 pallets spaced on 4 foot centers.

a. Under conditions where delivery by forklift truckis not possible, pallets may be grouped on the field 5-9. VSTOL AIRFIELD MATTING DEPLOYMENT.after major leveling operations have been completed.This type of deployment will understandably result 5-10. A VSTOL airfield (see Figure 5-4) is comprisedin more manual handling and the consuming of more of three major areas of matting: runway, taxiway and

time. For a nominal 96-foot wide runway without a parking area. The procedure for deploying matting

guide rail, placement of pallets on 8- x 24- foot centers on the airfield area is as follows:

5.1

Setlon V NAVAIR 51-60A-1Pallet Deployment

,^’T ^ ^5^.- giS5-"i ^>^~?:^,L â-i-xwiir h-^tîo

----\---------------’<o --------------!-----,\ ol

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5-2

NAVAIR 51-60A-1 S.cti-1 VPallet Deploy-nt

==\ -?< OT OT

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--------------^ --------------------------^

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5.3

SMtlon v NAVAIR 51.60A.IPallet Deployment

Six 12-foot typical keylocksOne 6-foot typical keylock

-------72-----

î^lli^lllli^lllllllli^^llFflilliiIlliiliiilii; ^1 c. Deploy one F26 pallet every 96 feet along the

l^lllllllllllllljil^lllll yijllll llllljjpljilllilllj guide rail side of the runway.

llllll’lllll’^lllhlll i||p| 11111111111111:11 DWG NO. d- Deploy F27 pallets, 90 connectors and stanei

72 |^||;;||1|;^|||1| 11.1 |^ 516325 keylocks (see Figure 5-5).

ll^^llllliîlilillllllllllllllllllllllllllll 11111111111|| e. Deploy two F27 pallets every six feet in parIlillll^llll^llllllliyilllllll Illlllllll 111111111111111111111 III allel rows which are fifty feet on each side of th<

.!.i.......^.....^,;iii parking area centerline.

Figure 5.3. VTOL AirfieldArrangement

5.11. SATS AIRFIELD MATTING DEPLOYMENT

a. From the initial starting point, deploy two F27 5-12. A SATS airfield (see Figure 5-5) is comprisepallets every four feet along the runway centerline. of fê major areas: a runway, two taxiways and tw<

parking areas. The procedure for deploying mattinjb. Deploy a typical keylock set every 100 feet on the airfield area is as follows:

along the runway centerline. Each keylock set shouldconsist of the following;

a. At the initial starting point, deploy a sec o

starter keylocks consisting of:

-<----- 150 ----- Seven 12-foot starter keylocksn IMJ One 9-foot starter keylock

1111 11 III III 1111111 One 3-foot starter keylock":;"!;: Hill "iiraiK a-"!";

I IIJI B ||| II i|| .--PARKING AREA

^ lit |!!i| |j|l||ii ^ b. Deploy F27 mat pallets along the runway ceniei

111 jl 1 [I I’ IflMi l.ine on both sides of starter keylock line; two pallets|| I ||j p| || every four feet

IBIi 1111 DWG NO. 617260

I 11 iBi! 1 ^-STARTER KEYLOCK(ilil!!^^^^ ^r RUNWAY CENTERUNE-7|lW^ -^--"--INITIAL STARTING POINT / 10-H <- r- <S

h<--- 118--*\ 18.1/2GUIDERAIL EDGE

I------------------------------- 600 ----------------___________^.

F/gure S-4. VSTOL Airfield Arrangement

fr4

NAVAIR 51.60A.1 Section Y;Pallet Deployment’

<---360--- .-LARGE PARKING AREA

III 1|| (1 1 |ll SMALL PARKING AREA^^240-^. 7,2

illli |i II 240 v-ARRESTINGWIRE \_________*Ilia! !|hlljl|l ;|n| ^CENTERLINES NK!F^B

456 ii aliliill-JL ,,,T,AL \\ ., ilJfflb||l^-TAX.WAy^^^g^’NG \\ -148^___________________________|||| __-120!i|^.vi,îi^ TjW,| ijilii ilg ij iiilill ill feiii’iiiiii.jiill’iaMJ IE3i"1111 ’-96

\(fr litittttt^^^^,.;, tjjij;^ _^ JJHJiiiiJJJJ ;!""l"y"";’l’:’J"""""iiiJ"""""

L-^-----\^--...----------^-^^STARTER KEYLOCKS \-GUIDE RA IL CENTERLINE RUNWAY CENTE RLINE-’

DWG NO. 617261

Figure 5-5. SATS Airfield Arrangement

c. From the initial starting point, proceed to the d. From the starting point, proceed to the rightright and deploy typical keylocks at 100-foot intervals and deploy an additional F27 pallet at the 700-footas follows: mark and then every 100 feet thereafter through the

1700-foot mark.FEET FROM 12-FOOT 6-FOOT

STARTING POINT KEYLOCKS KEYLOCKSe. Deploy an F26 pallet every 48 feet adjacent

100, 200, 300, 1700 to the guide rail centerline.

1800, 1900 and 2000 6 1

400 and 1600 7 f. Deploy four F26 pallets along each of the two

500 and 1500 7 1 arresting wire centerlines.600 and 1400 8

700 and 1300 8 1

800, 900, 1000, 9 1 g. Deploy F27 pallets, 90 connectors and starter

1100 and 1200, keylocks at each taxiway (see Figure 5-6).

’Illi "iiiii"! !ss "I!!;’" i";! i|l iiiiliiiiiiil’ iiHI!! i! \iiipilNililil!|!i!!ill!^l !M;!i;lll!;U!!!ilii n 90 V-cnrc ncte "saA: î::: pi S: SP! -a!:ss!\ -cDBE Ur

!;; !;; I" !!’;! ;!;!i

3-FT ADJ 90 CONNECTOR \--- it! 1111111111 a III Ip III UN PARKING AREA

9.FT ADJ 90 CONNECTOR ==== IIHIMIffi 11| | |! 1| I l|li I___15 12.FT ADJ 90 CONNECTORS |---- 11 ||i | || | | |g ---A"

llilJIIIIIilll III3 11111 il1 U 1111 III 1111liiiiiliî’i.’i ilii \\\ ill I3 |iii ill ii;! 28S’iii!’:;’!’:!;!;iiiif’iilii iiii ili’ !|i|i i!| ^ ;i; IHi

l<!p|l !i’ ||;1 ^ ;!; 1ii;;!!i j;111| te!| ^ i|ij I iP ii ______l-

3 F27PALLETS------ll||l ! III II 1i;;;|;,s |i; ;!; ;;,;, I,, ;;;;! !, ;;

!!! "I"!’ 1!! ’<lK I’l ili IS’i i;!1;’ ii1

ilillll ill III! ill ill III !11 II ili ^(R)

i’iiiiHijiii!’ î iii ill; "i ili T3.FT STARTER KEYLOCK ==_ 11 || I |1 N I I ---L9.FT STARTER KEYLOCK === !11|1| lli|il pi ll lljN| N1

5 12.FT STARTER KEYLOCKS =^= illil 1 1111|;| lljl l| IN! Illi III /-EDGE OFlil II III il 1111 II! / RUNWAYiii iiiiii h,tll|| "i i|i iiiiiii iii "I /

SOS |li: li; ’I t----------

Figure 5-6. Pallet Deployment for Taxiways

5.5

SMIOI V NAVAIR 51-60A.1Pallet Deployment

h. In the larger parking area, deploy F27 pallets d. From the initial starting point, proceed to thein parallel rows which are fifty feet on either side right and deploy typical keylocks at 100-foot intervalsof the parking area centerline. Pallets should be as follows:deployed two pallets every six feet in each row. FEET FROM 12-FOOT 6-FOOT

STARTING POINT KEYLOCKS KEYLOCKS

i. In the smaller parking area, deploy F27 pallets 100, 200, 300, 1700, 6 1

along the parking area centerline; one pallet every 1800, 1900 and 2000 6 1

fou, feet 400 and ^O0 7500 and 1500 7 1600 and 1400 8

i. In the large parking area, deploy a keylock set 700 and 1300 8 1at a point 276 feet from the edge of the area. 800, 900, 1000, 9 1

1100 and 12005-13. EXPEDITIONARY AIRFIELD i- u ^ v. ,e. From the starting point, proceed to the ngh

and deploy an additional F27 pallet at the 700-foo5-14. An expeditionary airfield (see Figure 5-7) is

mark and every 100 feet thereafter through the 1700comprised of a main runway (with extensions), two foot mark.taxiways and a large parking area. The procedurefor on field deployment of matting for an expeditionary f. Deploy one F26 mat pallet every 48 feet alon<airfield is as follows: the guide rail centerline.

a. At the initial starting point, deploy a set of K- Deploy four F26 mat pallets at each of the tw

starter keylocks consisting of: arresting wire centerlines.

h. Deploy F27 pallets, 90 connectors and startcaeven 12-foot starter keylocks

keylocks at each taxiway (see Figure 5-5).One 9-foot starter keylockOne 3-foot starter keylock i. Deploy F27 pallets in parallel rows 90-fect or

either side of the parking area centerline (sec Figur’b. Deploy F27 mat pallets along the runway center- ^-8).

line on both sides of the starter keylock; one palletevery four feet. J- Continue the pallet deployment pattern showr

for the entire 2258-foot length of the parking area.

c. From the starting point, proceed to the left andk. Ueploy a typical keylock set every 276 fcci

at 200-foot intervals, deploy a typical keylock set(sxcept at the parking area transverse centerline).

consisting of:Each set should consist of the following:

Seven 12-foot typical keylocks Twenty-eight 12-foot typical keylocksOne 9-foot typical keylock One 9-foot typical keylockOne 3-foot .typical keylock One 3-foot typical keylock

*-------------^-------------- 2258 -------------------------.’*------------1130 - ^-STARTER KEYLOCK

^^J STARTING POINTV^-GU4^ R^^^^"T,HO WIRE CENTEPUNESneri.u<-nB RUNWAY CENTERLINE-^ CENTERLINE

DWG. NO. 617262

Figure 5-7. Expeditionary Airfield Arrangement

5-6

,.rAlR 51-60A.1 Section,VPallet Deployment

16 10 10 10 10 10 10 /-K 12-FT TYPICAL

[-* fc-lAl^LL.Llx’rlAlJ.I TYPICAL / KEYLOCKS--^-. *i-i ^. <i^ <i <^. KEYLOCK /_____ ’ /,,__i!i|l||i!|pir"i!|||! spi ilp-ip Hfpl illl IIilpjiBi?! ililiiiiliiliinilliSIISIHrillllip rilri? llii!i^|!lii!l!ll!gSBi!i!pl’j!l"i 9

END OF MATTING W3S ^ "ll l|i !1:" ^ illlli !ii";>; 9"SSS Illl"!! l!""!!!!"^! iiil^^ili! iliil ii’i >lli iUi^i K I’"!’’’ ^’IIIJP ’"III ?">’

11 1 1 ii ill llill |IJ ijii iili! !B H 1 11 lil 1 I jlli I

|siJ!lliili|ll|iJlllliilll^ 27< _______. \-Ii!||"|| illllllillillllllllli!;!!;!;’;"!::;!;:;!!;-!^";) ’--14 I2.FT TYPICAL KEYLOCKSpWliililiillilll^ ___pocc OF 9FT TYPICAL KEYLOCKllffiMllllllffii-^ltlilllM^^^^^^^ TAXIWAY 3FT TYPICAL KEYLOCK

Figure 5-8. Pallet Deployment for Expeditionary Airfield Parking Ara

1. Deploy a starter keylock set at the parking area 5-18. BLAST DEFLECTOR ADAPTER PALLETS.transverse centerline. The siancr keylock should The use of blast deflector adapters is restricted to theconsist of the following: sides of taxiways and parking areas. The pallets may

be distributed as required at which time mat palletsTwenty-eight 12-foot starter keylocks will also be required to complete the deflector in-One 9-foot starter keylock stallation.One 3-foot starter keylock

5-19. TIEDOWN CONTAINERS. Tiedowns will not5-15. MISCELLANEOUS PALLET DEPLOYMENT, be needed until the parking areas have been laid.

However, the location of these areas will be known at5-16. GENERAL. The pallets discussed below are least approximately from the beginning of site prepara-.items used to complete or repair an installation, tion. Therefore, tiedown containers should be tempo-

rarily stored in the vicinity of these areas.5-17. MAT END RAMP PALLET. When matting is

installed on a hard surface runway, mat end ramp 5-20. EDGE CLAMPS AND STAKES PALLET. Edgepallets may be deployed in equal numbers at each clamps and stakes will also not be needed untilend of the runway or at other designated approaches, taxiing and parking areas have been laid. HoweverFor future use in runway repairs, mat end ramp pallets the location of these areas will be known at leaatshall be conveniently stored, approximately from the beginning of site prepara’

5.7

action V NAVAIR 51-60A.1Pallet Deployment

’ion. Therefore, edge clamps and stakes pallets should 5 22. ADJUSTABLE KEYLOCKS AND SPACER MATSbe- temporarily stored in the vicinity of these areas. PALLETS. The use of adjustable keylocks and space

mats is restricted to replacement of an AM-2 matting

runway section when the last row spacer is less than

24 inches. Therefore, these pallets should be grouped5-21. HEAVY DUTY MAT PALLET. Heavy duty mats in a. convenient storage area.arc required during initial installation. Since thesemats are used to replace regular matting under the 5-23. REPLACEMENT MAT PALLETS. Replacement

arresting cables, and along the guide rail, the heavy mats will not normally be required during initial in-

dury mat pallets should be grouped and stored con- siallation and therefore are best grouped in a con-

veniently near these areas, vcnient storage area.

5.8;

NAVAIR 5L60A.1 Section VIPallet Disassembly

SECTION VI

PALLET DISASSEMBLY

6-1. GENERAL, tools used to remove typical keylock sections whenrepairs to the matting are necessary. It is unlikely

6-2. This section of the handbook presents instruc- that these tools will be needed at the time of installa-tions for the removal of AM-2 matting and related tion; therefore, these tools should be stored with the

components from the shipping pallets. It also includes replacement mats. Prepare tie rods, end frame:, andinformation on the disposition of the pallets following filler wood assemblies for storage in the same mannertheir disassembly, as for mat pallets.

6.3. DISASSEMBLY INSTRUCTIONS. 6-6. 90 CONNECTOR PALLETS. (See Figures 3-6and 3-7.) Pallet disassembly is accomplished in

6-4. MAT PALLET. (See Figures 3-1 thru 3-4.) If (he same manner as mat pallets. Two support piecesmats are to be used directly from fork lift trucks, along the bottom longitudinal edges of the pallet willpallet disassembly may be readily accomplished while fall free when the end frames are removed. Secureon the lift. If deployment of pallets is on the ground, pallet parts, as described above, for future use.pallets should be blocked high enough near the center

to prevent the foot rails of the end frames from resting 6-7. BLAST DEFLECTOR ADAPTER PALLET. (Seeon the ground. Figure 3-8.)

r^IjTJION 6-8. TIEDOWN CONTAINERS. (See Figure 3-9.) Tie-down containers (or boxes) require only loosening of

Do not remove components from pallets rest- latches on lids to expose contents. Drill fixtures,ing directly on the ground, since removal of drills, taps, and screws are packed in the containersend frames may result in damage. Pallets with tiedowns.shall be stored for repackaging when instal-lation is removed. 6-9. EDGE CLAMP AND STAKES PALLET. (See

To remove end frames, release jam nut at upper end of Figure 3-10.) Remove the retaining bars on the top of

each de rod. Back off bolt until rod is free. In the the P""" and cut the ^"P8- The stakes "ay. now be

case of Pallet F15, cut strapping. Remove end frame ^moved without disassembling the rest of the pallet.

and filler wood. Remove locking bars from filler wood. The ed^ clamps are stored on four stakes on the

Disassemble lower ends of tie rods and place drilled floof of the P311^- cut the wire <" remove the pin)

pins back into end frames. Secure with locking pin. and slide them off- The locking bars are stored

Place jam nut on tie rod bolt and thread bolt securely between the prongs of the stakes that hold the edge

into tie rod. Tie rods, end frames, and filler wood clamps. Cut the wire and remove these. After all the

assemblies shall be stored for future use. These dis- stakes have been removed replace the retainer bars.

assembly procedures also apply to half mat pallets

^ ^^ ^.y ^ p^LET. (See Figureand mat end ramp pallets.3-11.) Use the same procedure that is used in dis-

6-5. KEYLOCK PALLET. (See Figure 3-5.) Removal assembling the mat pallets, with the exception ofof end frames of keylock pallets is accomplished in strap removal. Remove- the pallet framework, butthe same manner as for mat pallets. Within the filler because the heavy duty mats are stored vertically,wood area of one end frame are stored two socket head the mats must be flipped to a horizontal positionscrew wrenches to be used to fasten starter and female before removing the straps. Store the frame parts forkeylock sections together. There are also two removal future use.

6-1

Section Yl NAVAIR 51.60A.1Pollt Diso(smbly

6-11. SPACER MAT PALLET. (See Figure 3-12.) Figure 3-13.) Use the same disassembly procedure as

Follow the same procedure as described for the mats. ^s used for the spacer mat pallets. Remove the two

The end frame can be removed by cutting the cross- center wood fillers after the removal of the two end

strapping on the sides. Remove the top and side mats rows of adjustable keylock mats.

and store these with the other mats. The locking barsare taped together (18 at each end) and are located ^- REPLACEMENT MAT PALLET- (see Flgure

beneath the end piece of wood filler. After removing3-1’1 and w) The P31161 ls Assembled in the

the spacer mats remove the mat on the bottom and sanie manner as mat ^nets- Lockln bars are stored

store it with the other mats. Store all the parts of the within the mats- Four ^ock^ head screw wrenches,

framework for future use.which are "sed for mat lnstauatlon’ are ^P^ on an

end frame. Retain all pallet items for future use.

6-12. ADJUSTABLE KEYLOCK PALLET. (See

6-2

NAVAIR 51-60A-1 Section VIIInstallation Instruction*

SECTION VII

INSTALLATION INSTRUCTIONS

7-1. GENERAL, that reversing the procedure is difficult and inefficient.The coated side is always "up" and the interlocking

7-2. This section provides the procedures for install- prongs on the short (2-foot) edge are always to theing AM-2 matting at an airfield site. In addition, it right and up. Survey lines are present to guide at

presents information on manpower requirements and least one edge of the section being laid to maintainorganizational structure of the installation crew. proper longitudinal alignment. Other sections of the

site may be laid in the same manner, and at the same7-3. INSTALLATION CREW. time, if survey lines have been established, pallet

deployment has been accomplished, and sufficient7-4. Field experience indicates that a 16-man crew personnel are available. A typical keylock section isprovides maximum efficiency and feasibility when laid every 100 feet starting with the 100-foot mark on

laying a runway 96-feet in width. Thus two crews may either side of the starter keylock.be utilized in laying a runway and additional crewsused for laying other areas simultaneously. The break- 7-7. WITH GUIDE RAIL. The genei sequence ofdown of a typical 16-man crew and the duties of each laying matting for the runway, with the guide rail in-man are as follows: stalled, is to start at one end (at the approach apron)

and work toward the opposite end. The guide rail1-NCOIC: Supervisor divides the runway into two sections, 18 feet and 781-Alignment Man: Insures that the linear align- feet (or 18 feet and 30 feet for a 48 foot runway).

ment of the field is main- Individual mats are laid in a brickwork-type pattern,tained by adjusting the first from the guide rail to the outer edge, in each sectionmat in each transverse row when facing the working area. The starter keylock isto be flush with the pre- not used when laying a runway with a guide rail.surveyed lateral boundary Instead, typical keylocks are laid at 100-foot inter-prior to the rest of the mats yals on the runway, and for other sections of the SATSin that row being laid. field are laid in accordance with Paragraph 7-6.

2-Prybar Man: Adjusts individualmats usinga prybar to provide maximum Not*allowance for thermal expan-sion and inserts mat locking Visually inspect upturned sides and endbars. connectors of AM-2 matting for foreign matter

12-(Six 2-man Teams) working with a partner, ob- before placing them in position. The pre-Mat Installation Man; tains a mat from the pallet; sence of dirt, chips, stones, etc. will prevent

carries mat to emplacement proper interlocking of mats. Brooms orpoint; and, installs mat in brushes may be used to clean foreign matter^le^’ from the connectors.

7.5. SATS FIELD INSTALLATION SEQUENCE. 7.3. MAT LAYING PROCEDURE WITHOUTGUIDE RAIL.

7-6. WITHOUT GUIDE RAIL. The general sequenceof laying matting for any lengthy section of an instal- 7.9. jhe sequence for installing AM-2 macs and re-lation is to start at the transverse centerline and prog- lated components is shown in Figure 7-1. The se-ress toward each end simultaneously. The starter quence can be modified so that work proceeds on onlykeylock section is laid and then individual mats are one row of mats at any given time; however, SPEEDlaid in a brickwork-type pattern from left to right when QF INSTALLATION IS IMPORTANT: The sequence,facing the working area. The left-to-right sequence is as shown in Figure 7-1, allows for the use of at leastdictated by the mat interlock design which is such (WQ crews, with six 2-man teaas on each crew carrying

7.1

SMtlen VII NAVAIR 51-60A-1InBtollotion Instruction*

KE^YLOCK-s. ^9-FOC)TSECTIC)N FILL-LENGTH MAT--^^^---,---.7 / ^-TRANSVERSE

V, (7) 12-FOOT SECTIONS-7 3-FOOT SECTION -/ CENTERL1NEv-HALF-LENGTH MAT OF RUNWAY

STARTER ""- l-l-NG^ MAI1-5-^

KEYLOCK-^ r~~Z--I"""’! -;

i 1 ’___STARTER ’---’---’ f--4--\~~3~"iKEYLOCK-^ ___________________________________| 4 1-2 ":

[-1-L.- 2 4u-3__I=3=3

1-^-1STARTER 5 T 4--’ TKEYLOCK-^ r--g--r~-k--f--2 "I""1

2 4 5

r--?--^--4---1 ^ 1. RUNWAY

STARTER I---6--T"56

ÊDGE OF

KEYLOCK ______j g^n 5 4 3. RUNWAY

r-5-1 6 -p-^--5.--E=+/-LT^

r--1.______,-_.l t 1-6

___r 7 6 5

STARTER 7 1"-6--T S -1"^ L~3l!KEYLOCK-^ |--7-~’]~6---’--^--T---^--T--^---I--J---J

LJJ--2--L--4_J__ 5__L__? 7 JL 3 -r 4 r 5 ^ 6 ^7^1L.--r---^---.--i.--.---i-----i---~-i^L--+/-S=3

-O^L-? 7 _~L~_6_;

"^ T ^L... ’.0 0 0

KEYLOCK^ 8 1-7---^--i -^--5---^-- ^--^-3-KEYLOCK^

^ ^ ^-- g-- ^-, ^-------i-Lj’-. z-t-^--i-s-.i-s i,,! a Jr ? 7 4 r 5 ^ 6 7 8

L: 5q_-^-4----j 8=]

b+/-=p[-a=r^’"^ _îE=E^

,------|---,L-?--J-- 8-!--7--!-^-, rTRANSVERSESTARTER j. 9 I 8 7 6 5 GENTERLINEKEYLOCK. ^^__^.._p5^__ ^F^--^-^--^-4--.^--^--;-3^ OF RUNWAY

^l^--2-- ^-4---^--5---,---6---}--?----L.- 9 f 1L_ 3-_L_-^--L-_ 5__i.__s-L-{__-L__._J-a-iÂ^..6_^-.7..^_^__F^=:J^-TT--8--f & 100 FEET

r~TT~~ r (’) 12-FOOT SECTIONS

JJS’Â.^ r 9-FOOT SECTION 3-FOOT SECTION -\KEYLOtiK-’-^^^^^^^^^^^^^_^^^^^^^_^^^^^^^-^_^^_^_^^^^^^^_^^^^^^^^^^^^^^ ’^^

F/ffyr* 7-L AM-2 Mat Installation Sequence (Wifhout Gui’c/e Ra/^

7.2

NAVAIR 51.60A.1 Soctteh YllInstallation Instruction*

and placing mats and keylocks. The laying of AM-2 Notemats and keylocks is shown in Figures 7-2 through7-11 and consists of the following steps: Lay several transverse rows of AM-2 matting

in one direction only from starter keylock rowa. Lay starter keylocks on transverse centerline initially. If matting is started on both sides

of the runway. (See Figure 7-2.) A 9-foot starter key- of starter keylock, a seesaw force could re-lock is laid at outer edge of runway. Remove socket suit, disturbing alignment of entire field.head screws from keylock to allow for extending lock-ing bar into next keylock section. d> With non-skid side of mat turned up and the up"

turned prongs on the right, align first mat (half mat) on

b. Place a 12-foot starter keylock next to and left side with starter keylock (see Figure 7-3). Alignaligned with 9-foot section. Move 12-foot section downturned prongs with runway edge. Hook femaleagainst 9-foot section, and adjust locking bar so that edge of mat into groove on starter keylock (see Figuresocket head screws will secure locking bar in each 7-4) while holding mat in an angular position. Rotatesection. Thus 9-foot starter keylock and 12-foot starter mat downward to form joint. (See Figure 7-4.)keylock are secured together, as shown in Detail"A" of Figure 7-2. e. Lay second and all successive mats the same

way as the first mat (see Figure 7-3), in relation to

c. Repeat laying six more 12-foot sections and starter keylock. The downturned prongs of the secondone 3-foot section of starter keylocks to complete mat shall mate with upturned prongs of first mat,

96-foot width of the runway, as shown in Figure 7-5. When the mats are properly

RUNWAYTRANSVERSECENTERLINE -^

12-FOOT \STARTER LOCKING BAR ^s. ^ J^-^

rEDGE OF RUNWAY KEYLOCK -^^ (EXTENDED) .^^T^"’/ OR MATTING FIELD ---^ ^-sa-^^?^/ r SEE DETAIL "A" "^^ ^.sg^^^^ N^/ 9-FOOT -s^^^^^/ STARTER --ss^^^

/ KEYLOCK -i /" ’\,-as^^^^^^

3-FOOT STARTER KEYLOCK [A. L.-’^sffS-S^^^^’^^(TEMPORARILY LAID ASIDE)

^^^ pE^^^^^-^8^

<i"" STARTER KEYLOCKS LOCKEDTOGETHER

Figure 7-2. Placing of Starter Keylocks on Transverse Centerline of Runway

7.3

Section VII NAVAIR 51.60A.1Installation Instructions

STARTER KEYLOCK-i -^ss’11’’’’’3’’’^--^^\ A^^^ -sss-^13"^^ SECOND MAT

SEE FIG. 7-4 --7 \ /^^!:i^;::s ^’j---;’’’"’^

^^i^:;:::=s::::^::=^ \-SEE FIG. 7-5

FIRST MAT-/ \. /^

(HALF LENGTH) \ SX

EDGE OF RUNWAY ,/-\ /OR MATTING FIELD- \ /- HALF MAT //

\/ (TEMPORARILY LAID ASIDE ---\ (^/

FIgurs 7-3. Placing of First and Second Mats

.^^iiii^^ /--FIRST MAT UNIT

,j^^|d|| iLl^^^ ^-- MAT ROTATED

MAT POSITION PRIOR-^ ^^^^^r IVfTO ROTATION ^^^^/

TYPICAL LOCKED POSITIONFOR MATTING AND KEYLOCKS

Figure 7-4. Engaging First Mat (Half Lmigth) to Starter Keylock

7-<

NAVAIR 51-60A.1 Scten VtlInstallation Instruction*

liillillllll^^ 1;N ^Sl/lliN^^^

% (R) liSlJB16"H’iB 81?;^^HfevK \ v

^ffSIlM III tl Ilii 1^ ilH: 1^ ti^ liJ-^N w ^- END CONNECTORs

V^B3ff3Bflsff’^ v- MALE EDGE CONNECTOR

^^^^^^BtfBs’t^ N-SLOT FOR^^tp^0"^ LOCKING BAR

MATS ENGAGED

Figure 7-5. Engaging of First and Second Mat

7.5

action VII NAVAIR 51-60A.1Installation Instructions

engaged, a rectangular slot is formed by the engage- Notement of the end connectors.

The first row of mats and each alternate row

f. Lock first and second mats together, as shown thereafter is laid utilizing half mats at thein Figure 7-6, by inserting the locking bar (see Figure outer edges of the runway and full mats in7-7). between (see Figure 7-1). The second row

of mats and each alternate row thereafter isNote laid utilizing full mats only. This method

provides a staggered joint for greater mattingThe first two mats and all mats in the first strength.row should be aligned accurately before in-serting the locking bar. Misalignment of mats li. Complete first row, installing six more fullwill prevent proper installation of second length mats and finally a half mat, using the samerow. Locking bars may stick because of the procedure describing installation of second mat (seenatural waviness in the manufacture of mat Step e).end connectors and locking bars. A fewlight taps of a hammer should drive bar into Noteproper position.

The first row of mats on the opposite side

^ tne starter keylock row are all full matsg. Place third mat at start of second row as shown7 i\

in Figure 7-8. Ensure the third mat is aligned on lefts e ^"^

side with mat in preceding row. Refer to Figure 7-4 CAUTIONand Step d. for engagement procedure, which is the *.">^->,..-.- .1

same for engaging of third mat with first and second Align first row accurately with stakes ormats. guide lines delineating extent of matting.

LOCKING BAR ---7 Q-^’^^’’’^^(SEEFIG.7-7) / -^c??^^^?^^ \

CT&BTFO KCV1 f\fU ^^’rff^^^’^iW^V^/’y^. WSf:St:::i^^ \STARTtR KEYLOCK^ ^^--------?:;:?;^^ v- SECOND MAT

EDGE OF RUNWAY / \ (J\\ ^^ \OR MATTING FIELD H U .^r^-’7^^

HAL MAT(TEMPORAILY LAID ASIDE)

Figure 7.6. Locking First and Second Mat Using Locking Bar7.(

NAVAIR 51-60A-1 ,^,^ ,^:^"

^^(^1/ÊW c6NNECTl6N’l^î^î^

MALE EDGE CONNECTION-1 V ^’-s, Â JiF^-- V__---.

Figure 7-7. Insertion of ihe Locking Bar

STARTER KEYLOCK-.

SECOND MAT-\ -^.s.s----^’^’3’’^^ -^-^>.FIRST MAT^^^^-C- ^-----’-’^ /\ ^-:-:-:333;^ Q--^^KJ TRANSVERSE /^^^. ^---^"ê-’-"^2^^ CENTERLINE^

Vtfs333’331’’’3’3 ^^ -^^^^’’’’’^^ ^ SEE FIGURE 7-4 FORV ^:[^\L^-sss’’^:^ MAT ENGAGEMENT

CIDCT MAT / ^-^ âJ’13’^^ THIRD MATrinbl MMl / Vss^ ^s-^:?’^ Iciii c-M/’TLnor\\u-/ !y^scsS?y -) (FULL LENGTH)^x t’*-~7

SECOND ^^y \ y-EDGE OF RUNWAY OR\ / MATTING FIELD

’-HALF MAT ^^--’"’"’(TEMPORARILY LAID ASIDE)

Figure 7-8. Placing of Third Mat (Full Length)

7.7

^" Y" NAVAIR 51.6CA.1iHBtollatlon InBtructlon*

As work progresses, periodically check 9-foot section after first engaging female edge ofalignment of macs already installed. Any keylock with male edge of first two mats in precedingmisalignment will cause a displacement of row. Raise socket head screw in male end of 9-footrunway from planned position at far end of keylock until threaded hole in female end of 12-footf^ld. keylock is aligned. Then secure socket head screw

in 9-foot keylock using socket head screw wrench.i. Install second and succeeding rows in accord- Se.e Detail "A" of Figure 7-10, which shows typical

ance with procedure for the third mat (first mat in keylocks secured together. Repeat laying of six morethe second row) with one notable exception. The 12-foot sections and one 3-foot section of typicalsecond mat in each row must first be hooked to the keylocks to complete 96-foot width of runway.preceding row while being held at an angle (seeFigure 7-4). It must then be aligned so that when die Notemat is rotated downward, the end connectors will mate

properly, as shown in Figure 7-5. After the laying of a row of typical keylocksevery 100 feet, continue laying AM-2 mat-

"ott ting, in accordance with Steps d. through i.,to ends of runway.

The mats are designed with an apparent"loose fit". This is to allow for expansion, 7.10. APPROACH APRONS AND MAT END RAMPS.and also to allow for the natural waviness Install approach aprons and mat end ramps accordinginherent in the extruded mat sections. Be- to ihe following procedure.cause of this, it is possible to have a row

of mats "installed" but so misaligned as to a. Approach Aprons (earth runways). Runwayprevent the proper engagement of one or more approach aprons are required at each end of the mainof the mats in the following row. (Such a runway. These aprons are ramps made of mats, placedcondition in exaggerated form, and the method to prevent the tail hook of a low incoming aircraftof correction, is shown in Figure 7-9.) To from engaging or hooking on to the edge of the runway.prevent this, locking bars may be used as Refer to Figure 7-11.temporary spacers between the rows. Placea locking bar on edge where the ends of two (D ^ aprons are constructed in a brickwork-mats join and at the row ends. After three or type pattern (but may be entirely of half-length matfour rows have been laid using locking bar ^^^^^^^ ê full width of the runwayspacers, proceed with remainder of the run- ^, f^ ^ ^ ^ ^^ ^^ ^ ^ distance ofway or taxiway by removing the spacers from ^ lg ^ ^ yês below the normal ground levelthe furthest row and using them in the row Th,. g^nd surface beneath each mat should be shaped’just laid. to provide full contact across the bottom of the mat.

,’^’^yg..^ ^’’t installation of the ramp, the excavation shall be^.^H-’.JL0-.} back filled (ramp is covered to the normal ground

level). The backfill shall be tamped and compactedIf it becomes necessary to adjust matting

with a siedge. always place a wooden block

^ Installation of the ramp at the starting endagainst d,e mat edge before sinking as ^,,, ^y ^ accomplished althoughillustrated in Figure 7-9. ^ installation procedure is slightly different. Place

side connector under the overhanging lip of first rowj. Every 100 feet, install a row of typical keylocks ., -" row

of "a18 ^d "ft until contact is made. The mat is thenin matting field (see Figure 7-1). Place a 9-foot typical âted downward while keeping the two mats S conkeylock at outer edge of runway, with female end of tact. Locking bars are installed as described pre-keylock aligned with first mat of preceding row (see viously.Figure 7-10). Engage female edge of typical keylockwith male edge of mat in preceding row (similar to b. Mat End Ramps (hard surface runways). ManineFigure 7-4 and step d). installed on hard surface runways requires end ramps

Refer to Figure 2-9. Start first ramp at righthandk. Place a 12-foot typical keylock next to installed corner, looking toward opposite end of runway. Place

9-fbot typical keylock. Move 12-foot section against the next ramp adjacent to it, ensuring that holes in

7-8

NAVAIR 51.60A-1 Section YlInstallation Instruction*

^^ ^^ -ssff:ss:s^sss=aN\ // ----USE WOODEN BLOCK TO PREVENT\. .ss---’’^3^^ \< // DEFORMATION OF EDGES BY

^^^’’^^^ ’\ // SLEDGE HAMMER

^--^:::::::^ rq // /’ ’-"t^ F^T _^--<?’’’^^^

Figure 7-9. Correction of Mat Misalignment

7.9

Swetion VII NAVAIR 51-60A.1Instollotion Instructions

,-12-FOOT MATS ^---""’ ^s.f^’^

r’Row^^-^^ ../^^ K <^^^y^ ’’. ,--EDGE OF

";-9-FOOT ^ RUNWAY DETAIL ATYPICAL ’-- TYPICAL KEYLOCK CONNECTIONKEYLOCK

Figure 7-10. Placing of Typical Keylocks in Matfing Field

overlapping plate on ramp line up with threaded in- located parallel to and 32 feet, 4 3 -1 inches from (In-

serts on matting ramp. Insert five flat head screws in runway centerline. When a catapult is used, additional

each ramp, using Alien wrench provided in tool box. types of matting are required (sec I’ipure ~-131. "ol-

Apply anti-seize compound to screw threads, ing mats are substituted for standard mats ;it ilie ends

of the catapults. Tlie mats are water cooled to carry

Note off heat from jet engine exhausts. Heavy duty mats

arc used on both sides of (he guide rail and under theScrews and matting holes are color coded, arresting cables. These mats have a high resistanceEnsure correct screws are used.

^ damage from surface impacts. The water cooled

mats are the same size as a standard full mat. The(1) Use locking bar, on edge, between ramps heavy duty mats are not the same size as a standard

and edges of mats to assure straightness. half mat. Heavy duty mat is 1-1/2 ft. x 6 ft. Lay mat-

ting as follows.(2) As the ramps are placed and screwed to- a. Establish guide rail centerline using a tiansit.

eether, drill holes in concrete for lag screw shields,b. Install near end deck sheave as specified in

using the holes m each ramp as a template. Drill NAVAIR 51-15ACA-1, and Installation Sequence Dataholes to 5/8 inch diameter and 3 inches deep, with Cards (15DC).drill bit from tool box. Insert expansion shield in each c. Install first guide rail, with dowel pins facing

hole drilled in concrete. Insert lag bolt and washer aft (opposite to the direction of laying guide rails).

in each counterbored hole. Tighten lag bolts with The first guide rail should be nine feet in length,offset, square box end wrench provided in tool kit. NAEC Part No. 612535-4, to prevent guide rail joint

lining up with matting joint.(3) Complete end ramp installation is depicted

d. Install the next four guide rails (10-foot rails)in Figure 7~a-

utilizing spacer seats NAEC Part No. 414233-1, and

gap gages, NAEC Part No. 414219-1, between the

7.11. MAT LAYING PROCEDURE WITH GUIDE guide rail joints, before driving dowel pins. Drive

RAIL. dowel pins and check proper position of pins in guiderails, using pin gage, NAEC Part No. 414212-1.

7-12. The sequence for installing AM-2 mats and

related components (including certain catapult com-

ponents) is outlined in the following steps. The As the guide rails and "its are being laid,

catapult is used only with SATS and Expeditionary any visible depressions in the grade should

airfields and the installation sequence is the same be filled in and ri^ed with applicable hand

for both arrangements. The guide rail centerline is tools.

7.10

HAVAIR 51.60A-1 Section Vjl

Installation Instruction*

^-END MAT ^^;sa:?5::::^3^^ h/^ffifc^^OF RUNWAY ^’’’’^^:3^:S-.^^

’---------HAL:F-^ENGIH^rs .^-^^/^^

(-----]------ NORMAL GROUND LEVEL /

Figure 7-11. Laying of Runway Approach Apron

/ \\

Section VU NAVA1R 51.60A.1Installation Instructions

^-t^^^.^ ^ ^^^DETAIL A

INTERLOCKING OF END RAMPSEE DETAIL A

.-<| [__ __J ij\^^/-^ ^_____t J >_______ i____ ____-^__ ____^._

p-- p.-^ -^ ^- ^

Figwv 7-12. Placement of Hat End Ramps

e. Insert transit target, NAEC Part No. 414691-1, h. Lay matting along the heavy duty mats besidein the center slot of the guide rail and make prelimi- the guide rail on the narrow Side (18-foot) of the run-

nary alignment of each rail. way from the starter keylock toward the far end of thelunway. Refer to paragraph 7-4 for detailed mat laying

f. After the guide rail is aligned and pinned, instructions.

install heavy ’duty mats along both sides of the guiderail for its entire length, i. Insert the transit target, NAEC Part No.

414691-1, in the center slot of the guide rail andg. From the starter keylock (near end of runway) make final alignment by shifting the five guide rails

lay matting aft of the deck sheave. This area uses and attached mats. The guide rails and mats may bestandard mats and cooling mats as shown in figure shifted by pounding the edge of the guide rail or mat

7-13. with a wooden block and a mallet.

7-12

NAVAIR 51-60A-1 Section VJIInstallation lntruction

^n^F=3^’^.3-^ FULL MAT-^ r-OEW SHEAVE

.....^^W^.... 1\ \ /l\\\\\\\\\^^^ \ \ /_______C\\\\<\\\\N ^^’^ i. ..V -r- -\

^^^^^^ ÂTER ^^^^^y^n .^ s^’0 =2:Ê^==SECTION A-A

K\\\\\\\\\\\

i\\\\\mm^\\\^,,,^^^^,^ /1 \ -INTFRI OrKk\\\\\\\\\\\K\\\\\\\\\\1 / \ IN tKLUl-K-." ,,-_,k\^^ .-FAR END / CONNECTOR^^^^^^^---H / DECK SHEAVE /_._./ k\\\\\\\\\\\N\\^^ ^ / /-^^^g^^^ DECK SHEAVE-. / ^FULL MAT_____\\\\\\\\\\\’| y \ /--[^^^^ \ / /-----i-,^^TA\\\\\vA\’^ -.,\ ^.. ^---p/--_- ^-^^\\^\\\<^\\\\^ ^^s^?’^^^T ^^Y^S^^Sf, ^ xtB^/’TMv ’’L k\\\\\\^Wf^^ ___\iw///)w^J=^-^^^S^^^ rs-^N^.<^/?^Ks:

"^^g^^Ê^^ SECTION B-B=:==:^-.- -1 }----T-J ^-HEAVY==-^-^-E^p---I="-^7^^"DUTY-EE^’^-EE?^^ MAT

.-TYPICAL-r ^’^ J KEYLOCK=--, -~yZ~^~,T .^-10-FOOT FULL MAT-\ / /^FULL MAT

--T-- ~~~7 ,^ GUIDE \ / /

::’S’"T’’ r~^~ ’:^=F\,---^^’^ RAIL ps-s-a

^^C SECTION C-Cr-^ |V .^-"NEAR END

^\ ^~ DECK SHEAVE-----l--\ -I----’ ^"\\ I-STARTER~73"^^^^ ~A KEYLOCK:_ -J’Q -^^^^^ / (PEMALE)

: m /^ ?3 :=I- FULL MAT-\ / /-FULL MAT^______OS (R)^ -(*}- /

^//^g^-L^ ^l^ss^^^^^^^^^ ^-MATTING INSTALLATION ^^^^4^///^^^ BEGINS HERE p-iJ-^^ ^ ^ ^^ ^ ^^^^/mV%mn-^-^ SECTION D-D

^^^^^^^^ <TA.TCP\///!/m//W/^^ IL <~5>^-WATFH /-STARTERy//////////fy""" -r-S WATbR KFYLOCK^^////y/^t^^ COOLED / ^^’’-’-’’-Û////7/////A MATS / (MALE)

^^;^--^ FULL MAT^ / ^FULL MATY//^/W//^^^^^^ \ /v/////////A M^/y/^>77^^^^^ L^^l.^v^rF^zdw//’/^^^^ r ’"u w^---^^^^///////y/yr^^ -i. U JC____3’ M T......^///^^....- 3 -rJ^S^^^^^^v-l^^g/,/^/%/////l _J) -^T^-T-a^X^-^^y-l

^^^-W SECTION E-E

^^^^SFigure 7-73. AM-2 Mat Installation Sequence (’Wfth Gui’rfe Rai’/)

7-13

Section VII NAVAIR 51-60A-1(retaliation Instructions

^^’^^ /

WIDEFigure 7-14. Laying of Guide Rails arid Mats

)s|ote ed, substitute 9-foot guide rail for a

10-foot ^.iiick- rail.

The guide rail center line shall nor vary by

more than 1/4 inch in 50 feet in the horizon- ’ Continue installing matting until 100 tect of

tal direction, nor more than 1/8 inch in the runway has been laid.

vertical direction, as determined by a 12-foot

straight edge. When checking vertical align- Note

ment, the straight edge shall be moved in ^ minimum of 10 gap gages should remain

6-foot increments, installed aft of the guide rail dowel pins

being installed.

j. Begin laying matting along the heavy duty mats

beside the guide rail on the wide side (78-foot) of the ni. Every 100 feet, install typical keylocks across

runway from the starter keylock toward the far end of runway. Typical keylocks cannot be secured to thethe runway. Installation of the matting on the wide guide rail. Cut keylocks in six foot sections, as

side may lag behind the guide rail and mat laying on necessary, to facilitate installation on each side ofthe narrow side, but should never be installed beside the guide rail. Refer to paragraph 7-9, step j. and h.gride rails which have not yet been aligned in accord- for typical installation of keylocks in matting field.ance with step i.

n. Install heavy duty mats under the arrestingk. Install next five guide rails. Guide rail joints cable centerlines as shown in Figure 7-14.

shall never be closer than three inches in reference

to the transverse heavy duty mat joints, o. Continue laying runway until far end of guiderail is reached.

Nofp. Install deck sheave assembly as shown in

When the 3-inch minimum is being approach- Figure 7-13 at far end of runway.

7.14

NAVAIR 51-60A-1 Section VHInstallation Instruction*

q. Install standard mats and cooling mats at far 7-15. RUNWAY-TAXIWAY CONNECTORS. Install 90end of runway as shown in Figure 7-13. connectors on edge of runway at the point where

the lateral taxiways will connect with the runway(see Figures 2-1 and 2-2). 90 connectors may be

7-13. FIELD LAYING PROCEDURE, used at either points where two mat laying patternsat 90 to each other, are to be joined. Where the ad-

7-14. Several procedures may be followed in laying joining pattern has not been laid, install adjustablethe entire field as follows: 90 connectors in accordance with Procedure Number

1. Where the adjoining mat pattern has been laid, in-

a. The main runway is laid first. Then the lateral stall 90 connectors (H Type) in accordance with

taxiways are installed. Next the taxiway, parallel to Procedure Number 2.

the runway, the parking stands and storage areas

are installed, in that order. Note

b. The above procedure may be modified in the Adjustable 90 connectors provide a positiveinterest of speeding up the overall installation, lock between the adjoining sections of mat-

Thus, the main runway and the parallel taxiway may ting, whereas, H Type 90 connectors allowbe laid at the same time. The lateral taxiways and movement and slight misalignment between

parking areas may then be installed, the adjoining sections of matting.

CAUTION a. Procedure Number 1. Where the adjoining patternhas not been laid, install a sufficient number of

If the latter method or procedure is to be adjustable 90 connectors along the 2-foot edge of

used, the distance between the runway and matting (such as edge of runway) to equal the width

its parallel taxiway must be carefully con- of the taxiway or other section to be joined. Lay a

trolled. Since the mat width is 2 feet, a gap half-length mat into the first adjustable 90 connector

of almost one foot could occur at each end of so that the end of the mat matches the end of the

the interconnecting lateral taxiway. The gap connector. Engage prongs of a full-length mat into

between the lateral taxiway and the long prongs of half-length mat previously laid and pushtaxiway and runway should not exceed two into engagement with the adjustable 90 connector.

inches. Continue to lay mats in above manner until the first

RUNWAY

^ DIRECTION

^lll^-^l"^ \’ ^’W^/ .:J;;:;a^’: V V^: :-:’:.^:^’’. .’.;---. ^;/.^y.:,:’.:.,-;;.; Z-ADJUSTABLE 90’

/ CONNECTORSZ6FT MAT

TAX, WAY

* CONSTRUCTION DIRECTION

Figure 7-]5. Installation or Adjustable 90 Connectors, Procedure No. 1

7-15

Section VII NAVAIR 51.60A.1Installation Instruction*

row is completed to the length of the adjustable 90 retainer, using tools from tiedown containers. Referconnectors. Additional mats may then be laid in the t6Figure7.17.The procedure for drilling is as follows:usual manner. (Sec Figure 7-15.)

(1) Secure sleeve, Part No. 412131-1, co 5/16-b. Procedure Number 2. Where the adjoining drill with setscrew using drill fixture, Part No.

mat pattern has already been laid, adjust the last 509044-1 as shown in Operation 1, of Figure ".17.few rows of matting (of die taxiway) so that the Orient sleeve to ensure seating of setscrew on bodyspace between the runway and the taxiway is be- diameter of drill.twecn one and two inches. Place a 90 connector

(H Type) in position as shown in Figure 7-16 and, (2) Position drill fixture as shown in Operationusing a sledge hammer and a wooden block, drive 2, of Figure 7-17, and drill one hole as shown. Properinto position. The most efficient method is to drive depth is obtained when sleeve contacts bushing.the 90 connectors from cither edge toward thecenter of the taxiway. Place a mark at or near the (3) Insert pilot, Part No. 412130-1, through drillmidpoint of the taxiway but which is also at the bushing into drilled hole. Drill second hole as shownmidpoint of die 12-foot length of mat. Drive first in Operation 3, of Figure 7-17.:onnector to this mark. The positions of the remain-ing 90 connectors are dien automatically estab- (4) Tap 2 holes 3/8-16 UN(::-3B. Finish withlished. Care must be maintained, while driving the 90 bottoming tap (o obtain 9/16 minimum full-threadconnectors, not to allow debris to be scooped up by depth.the forward edges of the connectors.

(5) Stow sleeve anil pi lor in hole’s provided, and7-16. INSTALLATION OF TIEDOWNS. Install tie- secure with sctscrews.

I downs as shown in Figure 7-18 in accordance with

I the following procedure: b. Secure ring retainer with two socket head screws.

a. Drill and tap AM-2 matting on prongs-downconnector. Drill two holes for each tiedown ring 7-17. PARKING AND STORAtil-: AREAS. These areas

RUNWAYDIRECTION

j’ - ’"’- ^, ’^^^ ^’’’Nfel^ "j l5wm^^---_""~")

\ ^-’’^si^^^i--"~--- 90" CONNECTORS--7 ATAVUIAV \9 TAXIWAY ’--MIDPOINT

| CONSTRUCTION MARKDIRECTION

Figur* 7-16. Installation of 90 Connectors (H Typf), Proefdurs No. 2

7.H Change

NAVAIR 51.60A-1 Section VI)Installation Instruction*

I--------^----------I----------^----------------I I

^ .^--41FIXTURE -"^ ’-J

----------^------------------------^-----------------

^? T^i^-(R)-j^- FIXTURE ?/--"’" BIT PILOT -^ VY/ SLEEVE

^^ \\ ^ \ fiL lU|-----L----| Yj ^ffl ^^----^ \ ^

y:-.-V.|____j-^i- T ^, ^^ ---^ ^^^^H^.BIT < ^MK\^ < T "Ik- 1.875 l^^<^ ^^:^77^.....J -\

OPERATION OPERATION 2 OPERATION 3

Figure 7-17. Drilling Jig for Installing Tiedowns

should be installed last. Mats and locking bars are adapters to boundaries of matting, which will beinstalled in the same manner as for the runway and female or male edges, prongs-down ends, or prongs-taxiways except that the staggered joint pattern is up ends. Three types of adapters are supplied to fitnot mandatory. This means the areas can be built up any one of the four joints. Erect AM-2 mats to thein any random pattern and that all leftover half-length exposed upturned edge of the adapters to provideor full-length mats can be utilized. The adjustable the blast shield. Use two adapters to support each90 connectors shall be installed between these AM-2 mat. (See Figure 7-19.)parking and storage areas and taxiways in accordancewith the same procedure as outlined in paragraph 7-14. 7.19 INSTALLATION OF EDGE CLAMPS ANDInstall tiedowns on the matting in these areas as STAKE ASSEMBLIES. To secure matting at aircraftshown in Figure 7-18. taxiing and parking area turning points, edge clamps

and stake Assemblies may be installed as required.7-18. BLAST DEFLECTOR INSTALLATION. To -.1 1,There arc (vp<?s of edae clamps required because ofshield the around area around taxiways and parkingareas from the blast effects of aircraft, install blast 4 differcnt nac e^cs The ^ ^"’P "1""^ for

deflectors as required. Assemble blast deflector each mat edge is as follows:

Change 7.17

Section Yll NAVAIR 51.60A.1Inxtallation lntructions-

\^\S;^\ N\^^^^^^ ^ RING RETAINER

^. \^^^\\’\’’-^\\ ^t^^^^^^^’ / ,^ SOCKET HEAD

^^ >:^^^^-^ RINS~\^3<^. CAP SCREW

\ ’-.. \-^\,s^\ \,\ \ \,^ ’^^ 12FT-0(TVP) ^l1:^\\^\\’\X \ \S’’^^^ r ^ ^ [^-"PRONGS" DOWN ENI

X^^\\v\ \\ \\\\^ ^’ \ OF AM-2 MAT

\X\\\ Y\ \\\\^\^\ \\\6FT^ ^x N-^ ^ \’- \ ’v V^^^^ FT-^ MIN

\. lor \J

\^--- ITYP)

Figure 7-18. Installing Tiedowns in AM-2 Malting

/^^^\\ ’o^^,1 1^ y NOTE: BLAST DEFLECTORS ARE\ ^^^-^y^l"^. / STANDARD 6 FT OR 12 FT

TYPE III ^^------^TYPE IV TYPE 11

Piguf 7.19. Instellotlw 9} Blast D//ctor Adapters and Hats

7.18 Chang* 1

NAVAIR 51.60A.1 Section VIIInstallation Instruction*

Type Part No. Application -8’

I 512596-1 Anchoring female edge 7-20 ÎI 512597-1 Anchoring male edge 7-21 ^TT’ ^ STAKE DRIVING TOOLIII 512598-1 Anchonngdown- 7.22 ^ W^^f-

turned prongs TYPE II Û SLEDGE HAMMERIV 512599.1 Anchoring up- 7.23 CLAiSp (-\ (SEE FIG- 7-24)

turned prongs _I

Detailed instructions for installing each type of edge -i,-L, /~clamp and the stake assemblies are as follows: l^SI-Zj H C_SL

Lr-T-^L- -J _)Note MALE EDGE 0 0

OF MAT-1When emplacing stakes, NAEC Part No.512600-1, insert stake through hole in edgeclamp. Drive stake into the ground using Figure 7.21. Anchoring Male Mot Edg Usingstake driving tool, NAEC Part No. 509595-1, Type Edge C/ompand either a pavement breaker or sledgehammer. (See Figure 7-24). install Type II edge clamps, NAEC Part No. 512597-1,

in the same manner as described for Type 1 edgea. When female may edges are required to be clamps (see substeps (1), (2), and (3) of step a., and

anchored, install Type 1 edge clamps, NAEC Part refer to Figure 7-21).No. 512596-1, as follows: (See Figure 7-20.)

c. When the edge of the mats to be anchored has(1) Engage Type 1 edge clamp with female edge downturned prongs, install Type III edge clamps,

of mat. NAEC Part No. 512597-1, as follows: (See Figure7-22.)

(2) Anchor edge clamp with stake, NAEC PartNo. 512600-1, as shown in Figure 7-20. (1) Engage Type III edge clamp with edge of mat.

(3) Drive stake into ground using either a pave- (2) Slide locking bar, NAEC Part No. 320660-5,ment breaker or sledge hammer, as shown in Figure into key slot.7-24.

(3) Anchor edge clamp with stake, NAEC Partb. When male mat edges are required to be anchored, No. 512600-1, and shown in Figure 7-22.

o m] TÔR^’wlTH ’PAVE- ^/-E DRIVING TOOL

/ UQC Wl n rmVC iiec/ MFMT RRFAKPI* OB TYPE III / rOR USE WITH RftVE-mere onCAI\Cn Un UCUTL 1 <SlFnap MAUIUFB EDGE MENT BREAKER ORU.1 6L.C.UUE. MAMMtR CLAMP-> L ih el Fnre UAUUE’D/ \ (SEE FIG. 7-24) CLAMP- rt/rt SLEDGE HAMMER

FYpE {-- \ i.__} (SEE FIG- 7~24)

CL^lE^-, ---1 DOWNTURNED \ ,---->CLAMP-i PRONGS-\ \___^ ^STAKE N. ^ r- STAKE

^TRTO C&^-TfeaFEMALE EDGE / 0 0 \ Q 0

OF MAT-/ LOCKING \ ^ ^>DMn

Flgur 7.20. Anchoring F,mo/e Mot Edg Using Figw 7-22. Anchoring Edg with OownfurnorfTyp / Edg Clamp Prongs Using Type /// Edao C/omp

7-l

Section VII NAYAIR 51.60A.1Inctallotion Instructions

(4) Drive stake into ground using either a

pavement breaker or sledge hammer, as shown in[SD Figure 7-24.

Sr T r srAKE DRIVING TOOL/ FOR USE WITH PAVE- When the edge of the mats to be anchored has

TYPE IV U I i^iI-.^^S^^ upturned prongs, install Type IV edge clamps, NAECFrtnF SLEDGE HAMMER’--; (SEE FIG. 7-24) ’art -’" 51A599-1, in the same manner as described

\ r--1 for Type III edge clamps (see substeps (1) through

^PRONG^ \ \ --I (4) of stePc" and refer to Fiure 723)

^^~\, /~ e. Tools and Materials. A stake driving tool, NAEC)& Li _f 1 pwt No 509595-1, and either a pavement breaker or

LOCKING ,/ ^ sledge hammer are required for driving the stakes, asBAR shown in Figure 7-24.

.1

Figur 7-23. Anchoring Edge with UpturnedProngs Using Type IV Edge Clamp

"^

Figure 7.24. Methods of Emplacing Stakes to Retain Edge Clamps7-20

NAVAIR 51-60A-1 Section VttIOrganisational Lvl Maintenance

SECTION VIII

ORGANIZATIONAL LEVEL MAINTENANCE

8-1. GENERAL, b. Conditions for Application. The application ofthe deck covering coating shall not be started or

8-2. During use in the field, matting may become completed if; (1) the air temperature is under 50F,damaged and require repair. This section outlines (2) the area to be coated is wet, or (3) rain or snowthe instructions and procedures for accomplishing ts expected to fall within 12 hours after the start offield repair of the following matting conditions and repair.

instructions for specific replacement procedures.Not*

a. Deck Covering Repair A dry period of 12 hours is necessary beforethe recoated mat can be used. Any rain or

b. Surface Dent Repair snow during this 12 hour period will necessirtale the removal of the repair coating, using

c. Skin Rupture Repair methyl ^Y1 ketoae’ Specification TT-M-261B. The repair procedure must then berepeated.

d. Individual Mat Replacementc. Application of Coating. Apply "Emergency

e. Section of Runway Replacement Repair Deck Covering Coatings" qualified in ac-cordance with NAEC MPR 1214 to a thickness of

f. Heavy Duty Mat Replacement Under Arresting approximately 1/16 of an inch. The deck coveringCable compound may be brushed, sprayed, trowelled, or

rolled. The deck covering coating shall be allowedg. Heavy Duty Mats Installed Next to Guide Rail to air dry for at least 12 hours before the repaired

area is subjected to traffic of any nature.

8-3. DECK COVERING REPAIR. Application of deckcovering coating on AM.2 matting is necessitated in d- Tools’. Equipment, and Materials. The followinginstances wherein the coating is removed, loose, or tools’ """"Is. and equipment are required to repair

charred, regardless of cause. Deck covering coating the deck covering:

procedure shall be as follows

^ Stiff bristle brush

a. Preparation of Surface. Prior to application ofthe deck covering coating, all evidence of loose coat- [) ""S8

ing shall be removed by brushing thoroughly with astiff bristle brush. All loose matter shall be removed (3) Broomfrom the brushed area by wiping thoroughly with aclean, lint-free rag or sweeping with a clean broom. (4) Denatured alcohol

Any evidence of grease or oil shall be removed by theuse of denatured alcohol, Specification MIL-A-6091B, (5) Methyl ethyl ketone

applied with a clean, lint-free rag.(6) Deck covering compound

9 (7) Brush, trowelling equipment or sprayingequipment

The alcohol shall be confined to the metalsurfaces to be cleaned and must not contact 8-4. SURFACE DENT REPAIR. Surface dents thatthe firm deck covcrii." coating, do not exceed 10 square inches in area or 1/4 inch la

8.1

i-ctlon VIII HAVAIR 51-60A-1Organizational Levl Maintenance

depth may be repaired by buildup of weld metal. Dents prescribed welding process. Minimum heat,crossing the ribbing are indication of crushed ribbing consistent with weld penetration, should beand shall be cause for replacement of mat. Depth used to prevent "Burn Through",determination may be made by laying a straight-edgeacross the point of maximum depth and measuring a. Repair Procedure Without Filler. Skin ruptureswith a small rule. (See Figure 8-1.) which can be closed by welding without the addition

of filler material can be repaired in the followingGRIND OFF EXCESS WELD.

mallner- (see Figure ^j____________\ ^) Remove paint and coating for 1/2-inch on,-"’’^’’^^S^Ty^//’^^ either side and ends of rupture.

1/4-MAX. DEPTrJ ]j ^ (2) Weld skin rupture shut.

(3) Weld at least 3/8-inch beyond each end of

Figure 8.1. Surface Denf Repairrupture. Ensure all welded areas are level with originalmat surface.

a. Repair Procedure. Repair surface dents in the --1/2" tÊARfollowing manner: AROUND RUPTURE

(1) Remove paint and coating throughout dent ^^<"’"""’^::V^^:^;A:^ ^^^^.wR^; ^:;Sii.?i;>>’?s.

(2) Using prescribed welding process, fill dent \-^;^j^’;^ ;; a*’’^*^^.’’^^’^with weld metal, starting at lowest point and fill to ^ Xfei:^^ 1T’’<’’’’’^^^

(3) Remove any weld metal protruding above ^^^S t^^^^^^^^^8858’8^(4) Inspect to insure watertightness. NON-SKID COATING^

(5) Clean entire mat. Repaint and recoat asWELD 3/8" ^^-V^^

necessary according to paragraph 8-3. "UFTURE /f’’^^^^:^’’^b. Tools, Equipment, and Materials. The following /’’S.îi^’.i’^^tools are required to repair mat surface dents: >^^^Sy^^^^SS^

(1) Welding equipment ’^^ îlllllii-^^-^^(2)’ Welding material ^^LI^^^^^^^^^^(3) Grinding tool ^^-v^

8-5. SKIN RUPTURES. There are two basic types ofskin ruptures which can be repaired by welding. Skin /-GRIND OFFruptures which can be closed by welding without the / EXCESS WELDaddition of filler material; and skin ruptures which /^can be closed by welding a small plate over the hole. Lwy ^^<^t.^ S% ^Not. ^ 5^ ^Skin ruptures are to be welded according to

Figure 8.2. Skin Rupture Repair8-2

NAVAIR 51-60A-1 Section VIIIOrganizational Level Maintenance

Note <-ul;ir saw, set for 2-ui(-’h depth of cut. [he cut shouldbe made along male edge and prong s-up connector.

Presence of skin areas thinner than normal f^c Figure 8-;).will he cause for replacement.

(2) Ensure that all recesses in mats surround-(-0 Remove any weld material above mac sur- my, repair ;)re.i arc clean. Use a broom or brush to

face. remove any debris.

(^J Inspect to ensure watcrcightne.ss. (3) Remove in^Jc connector and adapters fromthe replacement mat. using socket liead screw wrenches

to) Clean repaired area of mat and repaint am! taped to the pallet. 1k careful to retain dowel pin inrecoat as necessary according to paragraph 8-3. lower adapter. (See View "A" of Figure 8-4.)

b. Repair Procedure With Filler. Skin ruptures (4) Pl.ice the lower adapter prong under thewhich can be repaired by welding a small plate over lower prong of tlie "prongs" -down end of adjacentthe hole can be repaired in the following manner: mat "A", keeping the dowel pin up. (See View "A"

of Figure 8-1.)(1) Remove deck covering from matting surface

requiring minor repair to provide base metal for weld- (5) place middle and upper adapters on themg- lower adapter, using dowel pin as a locating device.

Ensure chat the "locking bar con^uc" on middle(2) Weld patch to damaged area utilizing alumi- adapter is in the locking bar slut of mat "A" and

num plate 1/8-inch thick, upper adapter prong maces with upper prong of the"prongs" -down end of adjacent mat "A". (See View

(3) Clean repaired area of mat. "B" of Figure 8-1.’

(4) Apply deck covering coating to patched (6) place male connector inro female connectorarea in accordance with paragraph 8-3. of adjacent mats "B" and "C". iSee View "C" of

Figure 8-4.)c. Tools, Equipment, and Materials. The following

tools, equipment, and materials are required to repair (7) place female connector edge: of replacementmat skin ruptures: ma( pyg^ grooves of male connector edges of adjacent

mats "E" and "F" (see Figure 8-4). in the same(1) Aluminum repair plate manner that AM-2 macs are connected. Gently lower

replacement mat into place being careful to fit the(2) Welding equipment jo^l p^ -^y j^p , connector adapter and male

connector adapter into the groove in male connector.(3) Welding material (^g y^g ,^,, ^ ,,^,, ^ pigu^ 8-4.)

(4) Grinding cool (g) ^,^ ^^ between the upper, middle, andlower adapters and connector adapter. The dowel

8-6. INDIVIDUAL MAT REPLACEMENT. Where anpin wilt provide at least approximate alignment, how-

individual mat is damaged and cannot be satisfactorilyrepaired, damaged AM-2 mats may be cut out of the

ever some "linor shifti"^ of ^Pl.icement mat with a

installation and replaced with a replacement mat P^" "^ bc "Pessary. Insert and tighten the four

assembly, socket head cap screws with 5 ’16-inch wrench pro-vided. (See View "B" of Figure 8-4.)

a. Replacement Procedure. Replace damaged mat

in the following manner: (9) Place clamp over male connector. Alignmentof holes can be accomplished by .sliding clamp in

(1) Cut out damaged mat so complete removal adapter grooves. Insert and tighten ten socket headcan be effected without damage to surrounding mats. screws with 5/16-inch wrench. (See View "C" ofThis can best be accomplished using a portable cir- Figure 8-4.)

8-3

Section VIII NAVAIR 51.60A-1Organizatlonol Lev.l Mainfnane*

K- SAW CUT

END CONNECTOR-/ END CONNECTOR"PRONGS" DOWN SECTION A-A "PRONGS" UP

-j - SAW CUT

roro:E03:ro r;zz=2=ww =’%a^FEMALE EOOE^U---LJ--L- fl II I HJjd^ ^^ EDGE

Figuf 8.3. Mot Cuffing hf Removing Mat8-4

NAVAIR 51.60A.1 Section VIIIOrganizational Lev! Maintenance

a. ^S a: iii4 0:

Q oc m us 2 ?K ^ o ^1*3 S "^ Q:: HJ 0-

z Sa: bJi- iiJ a: S OT

^ ^ ^^ ^ 1 ^ ^ .^^ 8 I s s 3 ^ ^^^ Q

liipy J / c^iy / ii (^ i

a: ft.^j!^^^ /i W^ ’@1^ /JN’sp^i^^^^^^^ / ^ uora: (g

8 tu ^ ^^f/IS^ i a: ^ ^ / / z^ ^^_i <n _j ^^/fjS^. ’^ff i ^ ^^ / ^^ L V^

SF <t s "7 ^^~~^\\^\SK ^ fFt oc LJ a:

^ s ’ ^^^ ^^ ^--> OL 0- Q 6| =^

8.5

Section VIII NAVAIR 51-60A-1Organizational L*vl Maintenance

(10) Using 5/32-inch socket head screw wrench, a. General. The procedure for replacing a sectionloosen two setscrews retaining locking bar. Insert a of runway is essentially the same with or without ascrewdriver or similar instrument in holes next to g^e rail installation; however, with a guide railsetscrews, and force locking bar toward mat "D", 11 ^ tinstalled, removal of typical keylock sections willas tar as possible. This will lock the replacement

proceed from the outer edge of the runway regardlessmat and clear setscrew holes. Bottom setscrews so ^t""""--

that locking bar remains in place. (See View "D" ofof whlch side of thc guitie rail thc ^P^ is to take

Figure 8-4.) place. Without a guide rail and when starter keylocksare used, typical keylocks shall be removed from the

b. Tools, Equipment, and Materials. The following righthand edge of the runway (or taxiway), whentools, equipment, and materials are required to install facing the end of the runway from the transverse cen-replacement mat: tcrline. This edge of the runway exposes the female

end of the keylock into which the special removal(1) Portable circular saw (minimum 2-inch depth tool must be inserted.

of cut)

b. Replacement Procedure. The replacement of a(2) 5/32-inch socket head screw wrench -section or the runway is accomplished in the follow-

/,, ini; manner:(3) 5/16-inch box wrench

(4) Broom ^ Remove first typical keylock section bylof’sening the socket head screw at first inboard

(5) Prybar connection. This screw need only be loosened untilit is free of male end of adjoining keylock (about

(6) Replacement mac assembly 7/16 of an inch). The screw shall not be- removedfurther since it is designed to be self-retaining and

8-7. SECTION OF RUNWAY REPLACEMENT. Sec- reassembly can be effected from this position.tion of runway replacement may be required whengroups of mats are damaged beyond repair or excessive (2) Insert prong of removal tool under turnedmat deflection and roughness, due to cavities under down lip of female connector and slide keylock fromthe mats, must be corrected, its position, as shown in Figure 8-5.

"s<, ^s;;:^-^ F<RST MAT ^^ ^^^SECOND MAT "S^ ’’^^^’^ /-TYPICAL KEYLOCK

FEMALE END-^’ ^’’’^s^^r^-^- \-REMOVAL TOOL-/ ^^SeS-

Figurv 8-5. Typical Ksylock Removal Tool8.6

NAVAIR 51-60A-1 Section VIIIOrganizational Lvl Maintenance

Note (5) With the row of mats raised, insert a bentrod or wire in the locking bar hole and remove each

The initial 3-foot or 6-foot keylock sections locking bar including the bars securing the cut piecewill have to be pried out since the exposed ^ ^e rail. The first row of matting may then beend is merely an unfinished cross sectional disassembled and removed. (See Figure 8-6.)cut and will not accept the removal tool.

/i\ (6) With the clearance now provided, removal(3) Loosen the next and subsequent connectors

as described above and remove the remaining keylock of the ^aindei of the matting and additional guide

sections. If mat distortion is at a minimum, it may be rai1’ as necessary to effect the repair, may be readily

possible to remove more than one keylock section at accomplished. Remove the cut piece of guide rail

a time. aft of the repair area by removing the locking barsand disconnecting guide rail pins, using pin remover,

(4) Using blocking and prybars, the first row NAEC Part No. 414223-1. Slide the guide rail out ofof mats must be lifted high enough to allow the lock- (he mats.ing bars to clear. One pryb&r on each mat and allbeing operated at the same time for the full width of

^ ^^ ^ ^^ surface, as necessary,runway (or taxiway), to prevent warping of the mats. is

^^ reinstalling the guide rail and new or refur-reconunended. The mats will readily hinee at the first

blished matting.longitudinal mat joi.it.

(dote (8) The installation procedure shall be the same

as that for original installation. Replace the locking

If a guide rail has been installed, the adja- bars.

cent mat may be cut parallel to the guiderail. This cut must be made so that it severs (9) Reinstall matting over the repair area,the locking bar so that the locking bar and until the last row of matting is in place. At this point,the end connector may be removed from the this row of matting must be raised in unison, withguide rail. prybars, to permit the installation of locking bars.

MALE EDGE CONNECTION-1 / iViL /^ ^ \__LOCKING BAR-’ V^^^^B^l // ^"^~^

Figure 8-6. Removal of Locking Bar

8.7

Section VIII NAVAIR 51-60A-1Organ! zotional Level Maintenance

Note or damaged AM-2 mats. To save material and man-

It will not be possible to insert locking bars power, the mats in the bottom layer need not be joined

between the guide rail and adjacent mats for together. It is advisable to have the reinforcing mats

touching, but it is not imperative that the mats in thethis row. Therefore, a -replacement mat

^^ ^y^ ^ interlocked. The mats in the bottomshould be installed next to die guide rail. layer shall be placed with the long dimension of theA locking bar is built into the replacement mats at right angles to the mats in the top layer. Amat. double layer of matting should be considered in all

cases where sandy areas can cause excessive mat(10) Insert the typical keylocks in the reverse roughness due to sand movement.

order in which they were taken out. Always use woodblocking between the hammer and connector, if it is

^ Replace top layer of matting.necessary to drive the sections into place.

Note d. Tools, Equipment, and Material. The followingtools, equipment, and material arc required to replace

When the space for the last row of matting is a section of runway:less than 24 inches, refer to paragraph 8-12for instructions to install typical keylocks, (1) Socket head screw wrench

adjustable keylocks, and spacer mats in the

^ Removal toollast matting row. If the row space is lessthan 3 inches, however, a prybar may be (3) Pin remover NAI-.C Part No. 414223-1used to move the mats together until engage-

\4} Broomment can take place.

(5) Prybarsc. Excessive Mat Deflection and Roughness Re-

pair. Excessive mat deflection and roughness which (6) Old or damaged mats

can be attributed to cavities under the mats can berepaired in the following manner: ’/7) New or "-furbished mats

(1) Remove all mats which show excessive 8-8. Deleted.wear and deformation in accordance with paragraph8-7b.

(2) Fill all cavities under the mats and covercavity areas with old matting. Areas should be rein-forced with any available mailing; M9M1, M9M2, AM-1,

Figure 8-7 Deleted.

Figures 8-8 and 8-9 and Pages 8-9 and 8-10 Deleted.

8-8

AyAIR 51-60A.1 Section VIIIOrganizational Level Maintenance

illustrates the use of the Edge Tool for the maleedge of the mat.

b. Detailed instructions are as follows:

8-9. Deleted. (1) Mats that need edges straightened shall beplaced on blocks in order to raise the mat off theground and provide sufficient clearance to use edgetool.

(2) Orient the mat properly; that is, place thetop of the mat face up as shown in Figure 8-12 andplace the bottom of the mat face up, as shown inFigures 8-10 and 8-11, as required to allow the edgetool to be used in an upright position.

8-10. EDGE REPAIRS.(3) Engage the tool with the mat edge as shown

8-11. GENERAL. The following instructions are in Figures 8-10, 8-11, or 8-12, at the beginning of theprovided for use of the mat connector repair edge bent area.

tool, NAEC Part No. 510827-1, in straightening themale and female integrally-extruded edges of AM-2 <4) To straighten the edge, apply a lateral force

mats, including keylocks and spacer mats. Edges " thc t001 handlc to bend the ed^ lip toward a

which are slightly damaged during shipping and han- Lightened position. Be certain that the tool fully

dling can be straightened with the Edge Tool to allow etw)p" th(’ nlal, ^ ^ ^ ^P^K a constantfort-c on the loo) handle toward the mat.

the edges to be interlocked at installation.

(5) Move the tool into the bent area in smalla. Application. These instructions apply to all increments and straighten gradually until the entire

AM-2 matting. Figure 8-10 illustrates the use of length of the bent section has been straightened. Dothe Edge Tool for the lower female edges of the mat. not attempt to straighten the bent section in one pass;Figure 8-11 illustrates the use of the Edge Tool make several passes with minimum bending per passfor the upper female edge of the mat. Figure 8-12 until the area has been straightened.

/r-BOTTOM OF MAT \ ~\

\. / BOTTOM OF MATV,,,^l8?A^t^^

Figure 8-]0. Straightening or Lower Femo/e Edge

8-11

Section VIII NAVAIR 51-6CA.1Organizational Lev! Maintenance

/ r-BOTTOM OF MAT \ ^Q^ ^<

Figure 8-77. Straightening of Upper Female Edge

/ r-TOP OF MAT \^

Figure 8-12. Straightening of (Aale Edge

8-12

NAVAIR 51-60A-1 Section YHIOrganizational Level Maintenance

fCAUnON indicated in Table 8-1. The row space can be filled^J~V~^~V~U’U^--’

using the combination of items that corresponds to

Care should be taken during bending to pre- thc space, as indicated in Table 5. However, if the

vent crackine. row ^s^ ls less than 3 inches, a prybar should be

used to move the mats together until engagement can

c. Materials or Tools Required. Edge Tool, take place.’’10827-1, is required to straighten mat edge lips.

8-13. REPLACEMENT PROCEDURES. The various

8-12. USE OF TYPICAL KEYLOCKS, ADJUSTABLE replacement procedures for installing the combination

KEYLOCKS, AND SPACER MATS. During replacement of typical keylocks, adjustable keylocks, and/orof an AM-2 matting runway section, when the last spacer mats fsee Table 8-?) are as follows:

row for matting is less than 24 inches (see FigureH-H), typical keylocks, adjustable keylocks, and/or a. When row space is 3 inches and typical key-

spacer mats may be utilized as th’e last matting locks are required, install as follows: (See Figure

row. Dimensions and package data for each item are 8-14.

~. _LL-LAST ROW

---------------I------------_-----------I------------,-- SPACE LESSTHAN 24INCHES

Figure 8-13. Row Space 1o be Filled with Adjustable Keylocks and Spacer Mors

TABLE 8-1. DIMENSIONS AND PACKAGE DATA FOR TYPICAL KEYLOCKS,ADJUSTABLE KEYLOCKS, AND SPACER PALLETS

Nominal Available Insti Pallet

Width Length Figure No.

Typical 3 inches 3 ft 8-14 F13Keylock 9 ft

12 ft

Adjustable 6-9 inches 3 ft 8-15 F29

Keylock 6 ft12 ft

Spacer 12 inches 6 ft 8-16 F25

Mat 12 ft

8.13

Section VIII NAVAIR 51-60A.1Organisational L.V.I Mainfnanc*

TABLE 8.2. COMBINATION OF ITEMS VERSUS SIZE OF ROW SPACE

Row Space (Row(s)/Item Fig. No.

3 inches (1) Typical Keylocks 8-14

6-9 inches (1) Adjustable Keylocks 8-15

12 inches (1) Spacer Mats 8"l6

(n Typical Keylocks9-12 inches 8-17(A)

(1) Adjustable Keylocks

(2) Typical Keylocks12-15 inches .’. 8-17(B)


fl) Sp;if(.-r Mats15 inches 8-17(C)

(1.) lypi<-’al Keylocks

12-1H inches (2) Adjustable Keylocks 8-17(D)

(1 Sp.ic<T Mats18-21 inches 8-17(E)

(1> Ad)ii.stablc Krylocks

Spiu’cr Mats21-24 inclic.s (1) Typical Key locks 8-17(F)


y-SFT TYPICAL KEYLOCK ,-12 FT TYPICAL KEYLOCK .-MATTING 9 FT TYPICAL KEYLOCK-,J:__ /:...._,...-./f-.^ yz-^.^-^-/- ^-z-___

______\\_ _^A_ _[______________RUNWAY^ ^-^TYPICAL KEYLOCK-^ M--J INCHES-- RUNWAY

rm^^^iri^^M=^^SECTION A-A

MALE END-i ^-KEYLOCK SCREW

FEMALE END--’ SECTION B-B

Figure 8-14. Insiollafiw of Row el Typical Keylocks

8-14

NAVAIR 51-60A-1 Section VIIIOrganizational Level Maintenance

(1) Engage typical keylocks with matting, as Noteshown in Section A-A of Figure 8-14.

All connections between the adjustable(2) Slide typical keylocks into the space between keylocks shall be made by removing the

the mats. keylock screw from the male keylock, align-

ing the slot in the female keylock with the(3) Connect typical keylocks together by raising threaded hole in the male keylock, placing

socket head screw in male end until threaded hole in ^g keylock screw through the slot, andfemale end can be aligned. Tighten socket head screw

tightening screw into the male keylock, asinto female end, as shown in Section B-B of Figure

^^ ^ g^^ ^ ^ p^^ g,^

c. When row space is 6-9 inches, adjustable key-locks can be installed by either a right or left-hand (1) Connect 3 foot and/or 6-foot keylocks

row, as follows: (See Figure 8-15.) together, as required, to start filler row.

-------------------------96 FT.

r-ADJUSTABLE KEYLOCK ASSY, RIGHT 8 FT FEMALE KEYLOCK ASSY\(5 REO’O, PART NO. 614554-I) (I REO’D, PART NO. 511875-1) -,

\ "_I~ r^_ "_7~" LJ /ED^ F^-^ LA~\ ^ ^-^r

RUNWAY-, r-----J-----------L -_-^-------i_--__- j y-EOGE.\ ADJUSTABLE KEYLOCK ASSY, LEFT\ 3 FT MALE KEYLOCK ASSY / / OF

(5 REO’D. PART NO. 614554-2)-^ (2 REO’O.PART NO. 511871-2}-’ RUNWAY

RIGHT HAND ROW

96 FT. --------------------r-3 FT FEMALE KEYLOCK ASSY. LEFT ADJUSTABLE KEYLOCK ASSY, RIGHT(2REQD.PART N0.511875-2) /_(5_REO’D, PART N0.614554-1)

EDGE 1^, ^ 1^ ^--’ L--. ^ ---L-^ r ^GEOF /. ,.______j__.’--A__________ __________L_^ / / RUNWAY

RUNWAY^ ^.ADJUSTABLE KEYLOCK ASSY, LEFT 6 FT MALE KEYLOCK ASSY / /

(5 REO’D, PART NO. 614554-2) (I REO D, PART NO. 511871-1)-/

LEFT HAND ROW

^-------------- 6 TO 9 INCHES--------------

KEYLOCK SCREW-t r-SLOT IN FEMALE KEYLOCK

r’’^^^B^^^^ lYr1^^L-/ ^^^^SI$$ !:y^^S:S5S^;S:S:^^^^^ V ^^’__l

FEMALE KEYLOCK-/ ^MALE KEYLOCK

SECTION A-A

Figure 8-15. Installation of Right or Left-Hand Row of AJjustaL Keylocks

8-15

S.ciK)n VIII NAVAIR 51-60A-1Orgonliationol Lev.l Maintenance

(2) Adjust keylocks to permit engagement (5) Continue the process of staggering the two

between the adjustable keylocks and edges of mats, ^P" of adjustable keylocks and connecting them as

_i,- c noied above, until the last required adjustable key-as shown in Section A-A of Figure 8-15.6 lock is installed.

(3) Slide adjustable keylocks into space between (6) Connect 3 foot and/or 6-foot keylocks, as

the matting, required, to end filler row, and slide into the space.

(4) Connect next mating adjustable keylocks, c. When row space is 12 inches and spacer mats areand slide into the space, required, install as follows: (See Figure 8-16.)

-96 FT-----.-----.. .,j

f-6 FT SPACER MAT (2 REQ’Dl .-12 FT SPACER MAT (7 REQ’3)

|-/ ’"-"--.----B -----r-/--"-B----T-\ \-------U c ^ " ^ ^ ^=I---._--..--_-----L__...--------i_.._________i_) L--_____

^-ED6E OF RUN^EDOE OF W^-^^

|2 INCHES- --^

^’^^f--^ ==’’--^y^

SECTION A-A

12 FT MAT (PART NO. 615286-1)6 FT MAT (PART N0.615286-2)

i- LOCKING BAR (12 IN. LG)

rTWT""") T~-W1T~\/ ^ ( ^ )\.- ^ ^^,_^ L_.^ W. \

SECTION E3-B

Figure 8-16. Installation of Row of Spacer Mors8-16

NAVAIR 51-60A- 1 Section VIIIOrganizational Level Maintenance

Note other but shall be separated by standardmats to maintain rigidity in the matting

Connect spacer mats using locking bar, system.NAEC Part No. 320660-5, as shown inSection B-B of Figure 8-16. e. Tools and Materials. The following tools and

materials are required to install keylocks and spacer(1) Engage spacer mat with matting, as shown mats in accordance with the instructions as outlined

in Section A-A of Figure 8-16, and slide into space in steps a. through d. These tools and materials are

between the mats. normally available at the matting site.

(1) Broom.(2) Connect next spacer mat, as noted and

slide into space. (2) Crowbars (prybars), 4x 4 wood blocks, andsledge hammers.

(3) Continue the procedure until entire space(3) Key "T" handle wrench 5/16 hex (see item

is filled.1, Table 3).

d. To fill a row space of 9-12 inches to 21-24 (4) Shovel and rake.

inches, refer to Figure 8-17 and TableS-2. Followinstructions of steps a., b., and/or c. to install thevarious combinations of typical keylocks, adjustable g-14. MAINTENANCE OF ADJUSTABLE KEYLOCKSkeylocks, and/or spacer mats. AND 90 CONNECTORS. Adjustable keylocks and

connectors should be periodically inspected for dam-

Note aged edges and missing hardware. Damaged edgesshould be repaired in the same manner as mac edges

If the soil is weak, keylocks and spacer (refer to paragraph 8-11), Missing hardware shouldmats shall not be installed adjacent to each be replaced.

8.17

Section VIII NAVAIR 51-60A-1Organizational Level Maintenance

L---__-__.------- 9. 12 INCHES

^TYPICAL KEYLOCK /-ADJUSTABLE KEYLOCK

;_=-^ ^^^^_^_^^^ |F^||ii;j1 n v7in ~r-~],-p ^y-^_i nlj lÂ

..._-----------.-.---._)2 15 INCHES ---------------------I/-TYPICAL KEYLOCK -ADJUSTABLE KEYLOCK

i" -’-^"’ .’ C--_> ’/ !~~J~: AWiSi L //- r\ r^. ^::::^:$:::$:::^ -----^-s^

B_

^.- -_-_--_-_|5 INCHES

/-TYPICAL KEYLOCK /-SPACER MAT

^ ^r-^/-’nn;-^^^^L_^L_JLiUL^^Li_c_

~-------------12 16 INCHES ------------------------i

/-ADJUSTABLE KEYLOCK ADJUSTABLE KEYLOCK

r-’-e^^,7 ^^^^:^|/ --^TK^-]^ ||r^-r-----t^^ ^11^-p^^âZZJ^ ^/T^-^Â^.^..:-,-.^^... ^.^w^.v^.^...U^;’.-.. <-gy

_Dr ---,---------18 21 INCHES -)

i-ADJUSTABLE KEYLOCK ^-SPACER MAT

-^^^rTinr^^b-’-gs^ll-^^ ^W( Ji j_j_t î^LJ^-

___----2, 24 INCHES/-TYPICAL KEYLOCK .-ADJUSTABLE KEYLOCK .--SPACER MAT

r^fr^’1^^^^^30--^^^"^^L^L^^^^^^^^-^LîiVL^_F_

Figure S-17. Installation of Row of Various Combinations of Keylocks and Spacer Mats8-18

NAVAIR 51.60A.1 Section IXRemoval Procedure

SECTION IX

REMOVAL PROCEDURE

GENERAL, d. The adjustable 90 connectors are independentlyremovable by sliding individual connectors lengthwise.

9-2. Disassembled pallets should be distributed in However the mat disassembly procedure should bethe same pattern that was used for installation of planned so as to remove matting engaged on the 12-footfield to facilitate repackaging as the various corn- edge first. This occurs, for example, where the lateralponenis are removed. With the use of typical keylock taxiway matting (12-foot edge) meets the runway (seesections, disassembly can be done at several points Figure 7-15); adjustable 90 connectors can be removedsimultaneously consistent with the available per- more easily than by sliding connectors lengthwise.sonnel and handling equipment. Speed of removal ofmatting will be considerably greater if disassembly e. Tiedowns and edge clamps must be removedtakes place in the opposite direction of assembly, prior to parking area disassembly.that is, the female connector is removed from themale connector, f. Disassembly of a mat row may proceed from

the end with the overlapping mat. Remove the lock-9-3. MATTING REMOVAL WITHOUT GUIDE RAIL. ing bar from the adjacent mat by inserting a bent rodMatting removal at points other than exposed ends or wire into the hole in the locking bar and giving aof matting requires removal of typical keylock sec- sharp tug straight out. (See Figure 8-6.)tions as the initial step. Then disassembly of a mat

row can be accomplished by working from one end to g. The most efficient disassembly procedure re-the other, quires disassembly in reverse order of assembly;

therefore, starter keylocks will be the last componenta. Remove typical keylocks by loosening the removed from the runway. Remove starter keylocks by

socket head screw at the first joint until it is free of removing the socket head screws from each adjoiningthe lower threads (about 7/16-inch). Do not remove starter keylock. Insert the connector bar in the starter

further as this screw is self-retaining and disassembly keylock just removed to the second hole (the bar willand future assembly are accomplished from this post- protrude one inch) and tighten the screw. Replacetion. If the exposed end of the typical keylock is a and tighten the screw in the adjacent keylock.cut end, that particular section must be pried out or

pulled out. If the female end is exposed the sections 9-4. MATTING REMOVAL WITH GUIDE RAIL. Por-may be removed using the special removal tool. (See tions of the installation other than the runway mayFigure 8-5.) be disassembled in the same manner as described

above. Runway aprons, which do not include guideb. Following removal of typical keylock row, use rail sections, are an exception. These aprons may be

blocking and prybars to lift first row of mats high removed at any convenient time after the backfill hasenough to allow locking bars to clear. The mats will been removed. Removal of runway matting and guidereadily hinge at the first longitudinal mat joint. With rail may be started at the same end at which therow of mats raised, insert a bent rod or wire in locking runway was completed or after removal of a typicalbar hole and remove each locking bar, as shown in keylock section, as follows:Figure 8-6. The first row of matting may then be

disassembled and removed, a. Remove typical Tceylock section in accordancewith steps (1), (2), and (3) of paragraph 8-7b., of

c. The backfill must be removed from the runway Section Vni. After removal of row of typical keylocks,approach aprons which may be accomplished as the cut the mat, in the first row adjacent to the guidecenter portions of the runway are being disassembled, rail, parallel to the guide rail. Make certain that cut

9-1

Section IX NAYAIR 51.60A.1Removal Procedure

severs the locking bar so that locking bar and end wire in the locking bar hole and remove each locking

connector may be removed from the guide rail. bars, including the bars securing the cut piece of

guide rail. (See Figure 8-6.) The first row of mattingb. Use blocking and prybars to lift first row of

n^y then be disassembled and removed. With clearancemats high enough to allow locking bars to clear. The _,,;i.?,. ,.’, now provided, the remainder of the matting and guidemats will readily hinge at the first longitudinal mat

joint. With the row of mats raised, insert a bent rod or rail mw/ be removed.

9.2

NAVAIR 51.60A.1 Section XRwpockoging

SECTION X

REPACKAGING

10-1. AM-2 MAT PALLET ASSEMBLY. (See Figures b. Install wood fillers and locking bars (13 pieces),3-1 and 3-2.) Place the first full mat on a pair of and place the end frames in position. Secure lower end

blocks 4 x 4 or larger, leaving enough room at each "f each tie rod to the end frame with a flat head pin,

end to prevent interference with the placement of the and secure with locking pin (see Detail "B" of

pallet end frames when the pallet is to be assembled. Figure 3-1). Remove bolt and jam nut from the tie

rod. Insert bolt through boss on end frame, as shown

a. Center all succeeding mats, aligning the end in Detail "A" of Figure 3-1, and install jam nut on

connectors vertically as shown in Figure 10-1 to bolt. Screw bolts into tie rods and torque graduallyensure minimum clearance between end of mat and and in sequence to 40-45 Ib-ft. Tighten jam nut against

filler. From the bottom and counting upward, there tie rods.

should be nine full mats, two half mats, and finallytwo more full mats for a total of 13 pieces of matting, c. For mat pallet assemblies (F15) and (F27), the

12 rows high. The number of full and half mats per pallet assembly can be either spot welded or fillet

pallet may be varied, if necessary, according to the welded ’see Figure 3-2.. Install wood fillers and 10

quantities available for packaging. See Figure 3-2 for locking bars on each end of pallet. Tape lockingmaximum repackaging (this pallet normally contains bars together before placing end frames in position.

16 full mats and 4 half mats). Install new strapping and seals to secure mats in

pallet, as shown in Figure 3-2.

-I--(--(--- 10-2. HALF MAT PALLET ASSEMBLIES. (See

^ ^-^-^’ ^n Figures 3-3 and 3-4.) Half mat pallet assembly is

^^/’,^^-^^^^!-^ accomplished in the same manner as described above.

P^S^ V^\ ^’^>-FILLER The completed assembly contains 12 half mats and 12

Wyw Vn locking bars, as shown in Figure 3-3.

^^^ ^\\U;,^-END PLATE 10-3. KEYLOCK PALLET ASSEMBLY. (See Figure

I12" ^ 3-5.) Place an AM-2 full length mat on blocks 4 x 4

\ I---KICTTI- or l^got ln the same manner as previously described.

J ~~~\ "jj -/--LOCK ING BARS p^. ^ 12-foot starter keylock on the left edge ofMAT ASSEMBLY-^ __LL-_JL-J^J- the mat and interlock six, 12-foot typical keylocks.

/ -1-^--""Rw Interlock a 3-foot and 9-foot typical keylock section,Evwyl^ with the cut ends butted together and finish the layerv^y t*\^v

^JOo |K?^\ with one 12-foot female keylock. Repeat the above

------S?>6M K’)l ^~’^~ ENFRAME procedure for the next eight rows. On the tenth row,)f<j~ (\V^j butt the cut ends of a 9-foot and 3-foot starter keylock

_____g^T" HK^ section to start and interlock six 12-foot typical key-’r, lock sections, one 9-foot and one 3-foot typical kev-;__(ALIGN ALL MATS AGAINST ’,

FILLER IF POSSIBLE lock section, and finish the layer with a 9-foot andJ|:::}-t^AlfifEANDCFoEROsSoR^T 3’foot female keylock section. Place an AM-2 mat

’Q^zzz^’ [MKTS on top of the stack. The pallet load ready for assem-bly consists of two AM-2 mats, nine 12-foot starter

keylocks, one 9-foot starter keylock, one 3-foot starter

Figure 10-1. Alignment or AM-2 keylock, sixty 12-foot typical keylocks, ten 9-footMot Ends in Pallet typical keylocks, ten 3-foot typical keylocks, nine

10.1

Sct<n X NAVAIR 51-60A.1Repackaging

f-END FRAME END FRAME-7

.!>. ’TT’’’^

S^ //I t--- FILLER FILLER-^,’/[/);^^’ / S r SETSCREW / -.s’\ L ’_, i\

\^ ’]| ^--^--LOCKIN6 BAR ADAPTERS ^^-H yt, (; ^^NV^X\\^X^^^^ ^i ^--vfffAv-^i^^^< ^y^^@ r j r"PRONGS"DOWN ENDSTOWED POSITION "PRONGS"UP END

STOWED POSITION

Figure 10-2. Alignmsnt of Rsplaceaunt Mat Ends in Pallvt

12-foot female keylocks, one 9-foot female keylock packed in the container leaving a space at the topand one. 3-foot female keylock. Tape the two special sufficient to pack the bags of drills and fixtures. Placeremoval tools and the two 1/4-inch socket head screw lid in position and secure.wrenches to the end plate of one end frame. Placewood fillers in position and place end frames in 10-7. EDGE CLAMPS AND STAKES PALLETS (F 28).approximate position. Pin the lower ends of the tie (See Figure 3-10.) Remove the retainer bars and lay 2rods. Iawrt bolt through boss on end frame as shown straps across the floor of the pallet. The stakes shallwpefly "A" of Figure 3-5. Install the jam nut and be packed on the base of the pallet in a manner whichscrew -the bolts into the tie rod. Tighten bolts allows adjacent stakes to be pointing in oppositegradually in sequence until fully torqued (40-45 Ib-ft). directions. The edge clamps shall be put on the first,Tighten jam nuts against tie rods. second, third, and fourth stakes (counting from either

side) of the bottom row. In every case the clamps shall10-4. ADJUSTABLE 90 CONNECTOR PALLET be slipped onto the stake as close to the head as(F31). (See Figure 3-6.) Place an AM-2 half length possible. The first stake shall hold the Type clamps,mat on blocks 4 x 4 or larger. Stack three columns of the second stake shall hold the Type II clamps, the14 adjustable 90 connectors on the half length pallets third stake shall hold the Type IV clamps, and thewith wood fillers between the stacks of connectors, fourth stake shall bold the Type HI clamps. SecurePlace wood fillers at each end of the rows of adjustable each bundle of clamps to the stake head with a wire or90 connectors and on the sides. Add three more half pin. Insert the locking bars between the prongs of thelength mats to retain the sides and top of the three stake and secure these with wire. Each pallet willrows of adjustable 90 connectors. Place end frames contain 120 stakes, 130 edge clamps, and 80 lockingin position on each end of the adjustable connector bars. Strap the stakes as shown in Figure 3-10 and in-stack. Finally, install new scrapping and seals to stall the retainer bars.secure mats and connectors in the pallet, as shownin Figure 3-6. 10-8. HEAVY DUTY MAT PALLET ASSEMBLY (F26).

(See Figure 3-11.) Place the full mat on a pair of10-5. BLAST DEFLECTOR ADAPTER (Package blocks, 4 x 4 or larger, leaving enough room at eachAssembly F18). (Sec Figure 3-8.) The container will fnd to prevent interference with the placement of thehold 200 type I, 120 type II; and 120 type III adapters pallet end frames when the pallet is assembled.along with 240 locking bars. Install the wood fillers and lockingbars (16pieces) and

place the end frames in position. Secure the lower end10-6. TIEDOWN CONTAINERS. (See Figure 3-9.) This of each tie rod to the end frame with the flat head pincontainer holds 120 ticdowns (rings and retainers), and secure with the locking pin. Remove the bolt andTiedowns are to be tied in small groups of 5 to 10, and Jam nut from the tie rod. Insert bolt through boss on

10.2

NAVAIR 51-60A-1 Sclen XRftpockoginig

end frame, as shown in Detail "A" of Figure 3-1, shall be 3 adjacent right keylocks separated byand install jam nut on bolt. Screw bolts into tie rods wood fillers. The second row shall be 3 adjacent leftand torque gradually and in sequence to 40-45 Ib-ft. keylocks, separated by wood fillers. Alternate rows

Tighten jam nut against tie rods. New strapping is of tight and left keylocks through the twelfth row.

ipplied in the method of Figure 3-11. For the thirteenth row place 1 right keylock on each

^ side. In the middle of the thirteenth row interlock

10-9. SPACER MAT PALLET ASSEMBLY (F25). 1 six-foot female keylocks with 2 three-foot male

(See Figure 3-12.) Place a mat assembly on a pair of keylocks and adjust the width to that of the adjust-blocks 4 x 4 or larger with its bottom down. On top of able keylock beneath it. For the other half of this row

this place die 14 rows of spacer mats, 2 full length interlock 1 six-foot male keylock with 2 three-footmats to a row, except the fourth, eighth, and twelfth female keylocks and adjust the width. Repeat this

rows. For these rows place 2 half mats end to end process for the middle section of the fourteenth row.

and adjacent to 1 full mat. In all cases the adjacent Place 1 left adjustable keylock on each side of the

mats shall be interlocked in place. On top of the fourteenth row. Place a mat assembly, bottom side

fourteenth row of spacer mats place a mat assembly up, on top of the fourteenth row, and place 1 mat

with its bottom up. With the bottoms outward place assembly, bottom side out, on each side of the pallet.2 assembly mats, one on each side of the pallet. Then Strap the circumference of the pallet, install the woodstrap the pallet with new straps around the circum- fillers and place the end frames in position. Then in-

ference. Stack half the locking bars in each end and stall cross-strapping and seals as shown in Figure 3-13.tape them with suitable tape. These stacks will beplaced in line with the wood fillers as shown in 10-11. 90 CONNECTOR (H TYPE) PALLET (F14).Figure 3-12. Install the wood fillers and place the (See Figure 3-7.) Place the two support pieces 25-3/8end frames in position. Install cross-strapping and inches apart (outside to outside) on two pieces ofseals on each side of the pallet as shown in Figure blocking 4 x 4 or larger. (The end frames may be used3-12. to gauge the placement of the support.) Be sure the

U-shaped cutouts are uppermost. Place one 90 con-

10-10. ADJUSTABLE KEYLOCK PALLET ASSEMBLY nector next to support and interlock the next five(F29). (See Figure 3-13.) The adjustable keylock connectors in the first row. Continue to interlockpallet will contain 20 right adjustable keylock mats, connectors for seven rows until forty-two connectors

20 left adjustable keylock mats, 4 three-foot female have been stacked. Fasten the wood fillers togetherkeylocks, 2 six-foot female keylocks, 4 three-foot to make a unit and place in position on each end ofmale keylocks, 2 six-foot male keylocks, and 4 mat the connector stack. Place the end frames into post-assemblies. Place the first mat, bottom down, on cion being careful to slide the bottom angle of the enda pair of blocks, 4 x 4 or larger, allowing room at frame into the slots of the supports. Assemble, tighteneach end for placing the end frames. The first row and secure the tie rods as previously described.

10.3

TO 35E2-2-7

SECTION XI

INTERMEDIATE LEVEL MAINTENANCE

11-1. GENERAL. 11-6. STRAP AND SEAL PALLETS. Pallets pack.aged by this method are listed below and should be

11-2. Intermediate maintenance on AM-2 matting is unpacked as shown in the applicable figure referenced.generally performed after an airfield has been dis- Straps and seals should be disposed of. All othermantled, palletized, and removed from the airfield materials used for this method are reuseable.site. Intermediate maintenance includes the followingtasks:

a. UnpackingPALLET DESCRIPTION

FIG’

B t\c-r.Inspection and classification

Fll 16 full mats, 4 half mats 3-2c. t\epair

F25 Spacer mats 3-12F27* 16 full mats, 4 half mats 3-2d. Repackage

^ Adjustable keylocks 3-13

11 1 IIMPArKIMr ^-^ Adjustable 90 connectors 3-6F32 18 half mats 3-4

WARNING ^^ Replacement mats 3-16

Steel banding, cut under tension, can snap free, These pallets may also be packaged using tiecausing injury. Leather gloves and face shield rods.are required.

11-4. AM-2 matting components are packaged by oneof the following methods: 11.7. SPECIAL CONTAINERS. Tiedowns are pack-

a. Tie rods a8ed wkh tbe cools "’I"1"’’1 for installation in a con-tainer designated Fl (see figure 3-9). To unpack the

b. Straps and seals container, release the four lid clamps and removethe lid. All packaging materials used for the FI con-

c. Special containers tainer are reuseable. Edge clamps and stakes arepackaged in a special container designated F28

11-5. TIE ROD PALLETS. Pallets packaged by (see figure 3-10). To unpack the container, removethis method are listed, below and should be unpacked (he hardware securing the two retaining bars andas shown in the applicable figure referenced. All remove the retaining bars. Blast deflector adapterspackaging materials used for this method are reuse- are packaged in a special container designated F18able- (^e figure 3-8). To unpack the container, remove

PAT FT np<;r-RiPTinMFIG- the hardware around the Perimeter of the cover andPALLET DESCRIPTION^ remove the cover. The interior of the container is

divided into three compartments for the three typesFll 11 full mats, 2 half mats 3-1 ,,j.iv^-

of adapters as shown in figure 3-8.F12 12 half mats 3-3

F;3 ^’^no 3’5 H-8. INSPECTION AND CLASSIFICATION.F14 H-type 90 connectors 3-7F15* 16 full mats, 4 half mats 3-2F26 Heavy duty mats 3-1

9’ eac p m container is ""P^ked. the

F27* 16 full mats. 4 half mats 3-2contents shoul<l be ""P6"^ ^ ’he following:

F29* Adjustable keylocks 3-13a- flatness

SF1 Replacement mats 3-15Mat end ramps 3-14

b. Condition of interconnecting edgesThese pallets may also be packaged usingstraps and seals. c- Cracks in welds

Change 2 }}.}

faction XI NAVAIR 51-60A.1Intwdiat* Lvt Malnfnanc*

d. Holes in matting c. SCRAP beyond economical repair.

e. Extra coatings ,,^ REPAIR.

f. Missing components

1:1-12. Repair procedures applicable to intermediate11-10. As each component is inspected, each should level maintenance arc the same as those assigned to

be tagged and classified into one of the categories oisanizational maintenance (refer to section VIII).

defined below:

ri-13. REPACKAGING.a. AS IS requiring cleaning and touch-up painting

only.11-14. Repackaging of AM-2 matting should be per-

b. REWORK requiring straightening and/or formed in accordance with the instructions provided

welding and cleaning and refinishing. I" section X of this technical manual.

11.2

NAVAIR 51-60A.1 Section XIIDepot Level Maintenance

SECTION XII

DEPOT LEVEL MAINTENANCE

12-1. GENERAL.

12-2. Maintenance tasks assigned to depot levelmaintenance personnel are the same as those assignedCo intermediate maintenance (refer to section XI).

12.1

NAVAIR 51-60A-1 Section XIIIIllustrated Parts Breakdown

SECTION XIII

ILLUSTRATED PARTS BREAKDOWN

13-1. INTRODUCTION, needed to assemble each type of airfield. The partsare listed in order of disassembly and are intended to

13-2. The illustrated parts breakdown (IPB) consists show relationship to higher assemblies. The illustra-of a group assembly parts list. Section XIV, and a tion for each breakdown normally precedes the listing.numerical index, Section XV. The numerical indexis explained in Section XV.

13-3. GROUP ASSEMBLY PARTS LIST. 13-5. FIGURE AND INDEX NUMBER COLUMN.

13-4. The group assembly parts list contains a break- 13-6. The first column of each breakdown containsdown of the various types of airfield matting instal- the section and figure number of the reference illus-lations and of the packages of components required (ration and the index numbers of the parts whichto construct the airfields. Also, a breakdown of the correspond to the numbers shown on the illustrationmatting packages and their contents is included. The (see figure 13-1). The figure number is followed by afirst eight figures show deployment of packages for dash and the index number is preceded by a dash.setting up the various types of installations, from the On matting installation breakdowns, the package num-smallest (the VTOL pad) to the largest (the expedi- ber ("F" number) is used as the index number on the

tionary airfield). The succeeding figures show the figure. The index number is omitted for an installationbreakdown of every package and pallet assembly or assembly when its components are listed.

FIGURE UNITS UNITS USABLEAND PART DESCRIPTION PER PER ON

INDEX NO. NUMBER2 3 4 5 6 7 ASSY INSTL CODE

-Fl ^ta -B-----^B^-- Index number of matting package

p^^ ----y^^g LMTb L’SABLEAND PART DESCRIPTION PER PER ON

INDEX NO. NUMBER , ., , ASSY INSTL CODE2 3 4 5 6 7 ._______________________

Figure 13-1. Figure and /noex Number Column

13.1

action XIII NAVAIR 51.60A-1Illustrated Part* Breakdown


INDEX NO. NUMBER7 2 3 4 5 6 7 ASSY INSTL CODE

14-1 516325-1 ^^W -Part number of one complete airfield

-Fl 511152-1 ^^^-F27 615527-1 ^B^ Patt munbets of matting packages-F28 613600-1 -4^^


INDEX NO. NUMBER g g 4 5 6 7 ASSY INSTL CODE

14-9 511152-1 ^^w "Part number of one package (Fl i’rom figure 14-1)

-1 416557-1 ^^^"2 A.^^9 ^Part numbers of package components

509044-1 ^^yMS16995-78 ,<-^ ^-^*~~~~’-^ ^-^

Figure 73.2. Porr Number Column

13-7. PART NUMBER COLUMN. "2", and components of assemblies listed undercolumn "3" are listed under column "4". The addi-

13-8. All installations, assemblies, subassemblies, tional columns are used as required to complete theand component parts are identified by part numbers, equipment breakdown. A dot is used when a part isThe second column of each breakdown contains the indented to facilitate reading of columns. Referencespart numbers assigned, in accordance with the NAEC to other figures for next higher assembly or for sepa-drawings (see figure 13-2). All part numbers listed lately illustrated detail breakdown are included inare NAEC numbers unless otherwise indicated, the description column.

13.9. DESCRIPTION COLUMN. 13-11- UNITS PER ASSEMBLY COLUMN-

13-12. The fourth column of each breakdown (see13-10. The pact names are shown in the third column figure 13-4) lists the quantity of parts required for oneof each breakdown (see figure 13-3). There are six assembly or installation. For example: the mattingsubcolumns which are used to show the breakdown of installation (VTOL) includes one package of aircrafta assembly into component parts. The general ar- tiedowns (upper half of illustration) and the tiedownrangement la listed under column "I", all components package includes 120 tiedowns and two drill fixturesof the general arrangement are listed under column (lower half of illustration).

13-2

NAVAIR 51-60A-1 Section XIIIIllustrated Part* Breakdown

FIGURE UNITS UNITS USABLEAND PART DESCRIPTION Numerical PER PER N

JNDEXNO^ NUMBER , , 3 , , , ^f^^subdivision ASSY INSTL CODE

I4-1 516325-1 MATTING INSTALLATION, VTOL Forward landingsite

-Fl 511152-1 PACKAGE ASSEMBLY AIRCRAFT TIEDOWN ^L(See figure 14-9) ^^^-F27 615527-1 PALLET AND MAT ASSEMBLY, AM-2, Mod 4(See^ft^Name of

figure 14-19) ^y\ P"1"^68-F28 613600-1 PALLET ASSEMBLY, Edge clamps and scakea^^

^^^(See figure 14-22) L--~-~^ /-^


INDEX NO. NUMBER1 2 3 4 5 6 7

ASSY INSTL CODE

14-9 511152-1 PACKAGE ASSEMBLY, Aircraft tiedowns ^---- -Name o one pack age(Fl froi figure I. -1)

-1 416557-1 TIEDOWNS ^-^B^^-2 MISCELLANEOUS COMPONENTS ^--B^^I fcNames of packag components

509044-1 FIXTURE, Drill ^^Figure 13-3. Description Column


INDEX NO. NUMBER1 2 3 4 5 6 7 ASSY WSTL CODE

14-1 516325-1 MATTING INSTALLATION, VTOL Forward landing site Ref

-Fl 511152-1 PACKAGE ASSEMBLY AIRCRAFT TIEDOVN (Seefigure 14-9) 1

-F27 615527-1 PALLET AND MAT ASSEMBLY, AM-2, Mod 4 (See Jffigure 14-19) ^r 13

-F28 613600-1 PALLET ASSEMBLY, Edge clamps and stakea^^H(See figure 14-22) ^^’ ^fc. I

Quanities of packages for one airfield ^^^ ..^^*-


INDEX NO. NUMBER 1 2 3 4 5 6 7 ASSY INSTL CODE

14-9 511152-1 PACKAGE ASSEMBLY, Aircraft tiedowna

-I 416557-1 TIEDOWNS 120-2 MISCELLANEOUS COMPONENTS .^^

509044-1 FIXTURE, Drill .^^^^^ 2

Quantities of components in one package^*^^^^

Figure T3’4. Units Per Assembly Column

13.3

XT^’.!" ^’L NAVAIR 51.60A-1lllutratd Part* Breakdown

MATTING COMPONENTS

PKG PACKAGE _________________PACKAGE CONTENTS__________________ QTY/w- PART NO. DESCRIPTION ITEM PART NO. QTY/PKG INSTL

PI 511152-1 TIEPOWNS, AIRCRAFT 416557-1 120 120

F27 615527-1 MAT ASSY, 2FT x 12FT 2 615526-1 [6 ""ZOSMAT ASSY, 2FT x 6FT 3 615526-2 4 52

F-28 615600-1 EDGE CLAMP, TYPE 4 512596-1 ?5 25EDGE CLAMP, TYPE II 5 512597-1 25 25EDGE CLAMP, TYPE III 6 512598-1 40 40

EDGE CLAMP, TYPE IV 7 512599-1 40 40

Figure J3-5. Package Contents Chart

13-13. PACKAGE CONTENTS CHARTS. In addition number ("F" number), package part number, des-to figures illustrating the packages required for each cription of contents, itena numbers of contents, andtype of installation and the breakdown figure for each part number, quantity per package and quantity perpackage, a chart showing the contents of each package installation for each component included in the con-is included (see figure 13-5). This chart gives package tents.

13.4

NAVAIR 51-60A-1 Section XIIIIllustrated Parts Breakdown

^Won )(y f^^"""Tied) Ili^^^^^-t

^--’""-""’"^K>11’’ ^-^^~^~^~~ \ V^w" P*"^ r~~----^ / ^7_^^---’tto"*-"1- -----^7^ \---^ ÔDE ^sT^-T---/’^^---’^"^^ __----"""^ l’’’ p-- \ ^~i ~~t /-^""’E’i Â’5~~~---,--__

r^^^-^’^:^^^5 u :us r^~]J^^

\^^-’s^’^^^ /l i f ;

^ /\ ^^--^r^^^^’"01---^^ \ \ / /- i: r^l\ f^V^^-^^^ V\\ \ \\ r F ^ j Q /\ W"^^^ ^^.-^ ’’ \ \ \ \ \ / /’: :’4 ’^ /\ r^ p^ \. ^^{. : -\ \\ \ \\ ^ :: ^ ;^ /\ I/’2 pS V ^^’ A 19. \ \ \\ F ^ ^ ^^V .. \^ V. ^,^ \ ^ \ \ \ v ^ ^ ^ /A< ^ \^ \. :’- ^::::’- :. } \\ \ -^\ ^ ^ ;% /D^ \ ^ \^ V ^ ^^ - ^---^ \ ^ ’^B \\ -^Figure t3-6. Jyplcal Example of How to Use th Illustrated Parts

Breakdown (When Part Number Is Known)

13-14. IDENTIFYING PARTS.^ ^ ^ ^ ^^ ^^^, ^ ^^ ê

13-15. PART NUMBER AVAILABLE. When the partind" nurober referenced in the Numerical Index.

number is known (see figure 13-6) proceed as follows:c. If a pictorial representation of the part, or its

a. Locate part number in Section XV, numerical location is desired, refer to the same index number on

Index, and note the figure and index number, the accompanying illustration.

13.5

action XIII NAVAIR51-60A.1Illirtrated Parts Breakdown

____---- GRoup.,

\[^^ ^ r [^ -. ""w^"’ /\ ^{^. N-Y / / 1^ VSTO^,M"’’’*lrt^l’L’’F->,^o-|

^^ff/ ^ ^?^\ ’’ " "" - ^ /L^ ’TI^N1^^^/|S^y^^^i,/4/U [-"^T^’T s^/ 21’ f0"1-’-’... ^V^FS / ’’ ’’^’ /U ASn NUMBER lollUJ^-y !. ,’""’^c2"’s"e’ \ /I INDE)tOT_L-------\--- <- ^""Sp./^"^.^,;, \ /

---~-----T p*ll-ETAW>-y ’""^.^r’>’s "’ ^Po..., \ /1 u- i"""-’ ^^"a ’ ^"- "**">’..; ""V-’ / ’" /n ow’-l MAT^"! ^’"’fonrf;, "’^’"lic.; \. /\\ \ ltl"" PU-ET*9f ""’.r..s; """\dh., /. ’. ’ 1-i\\ ""4-’ f"-l-E7 ’"^^s.. -\’"""’r/^- .. j.,7

\\ \ /1 ’""*"’ "^Y V’ / ustu" <-’ // "f ltl6M-5 SE*’/ \ / "-. .)j

1/ -t tl62<"< ’"Y \/ ’-’< /

Figure ?3-7. Typi’co/ Example of How to Use rhe Illustrated PartsBreakdown (When Part Number Is Not Known)

13-16. PART NUMBER NOT AVAILABLE. If a part (ration page number.

number is not known (see figure 13-7) proceed as fol- b. Turn to the page indicated and locate the de-lows: sired part on the illustration.

a. Determine the function and application of the c. From the illustration, obtain the index numberpart required. Turn to the GAPL List of Illustrations assigned to the part desired. Refer to accompanyingand select the most appropriate title. Note the illus- description for specific information regarding the part.

13-6

NAYAIR 51.60A.1 Section XIVGroup Assembly Ports List

SECTION XIV

GROUP ASSEMBLY PARTS LIST

14-1. GENERAL part of every package is identified by an index numberon the appropriate illustration. An "F" type of index

14-2. The group assembly parts list begins with number indicates that the item is a package of mattinginstallation figures that illustrate the various types components.

of airfield layouts. These figures also show the de-14.3. ARRANGEMENT.ployment of the matting packages. Later figures show

partially exploded views of these packages, or pallets, 14-4. Packages and larger assemblies are listedwhich are used for shipment. Each package is iden- first, followed by listings of the various components.tified by an "F" number, which serves as an index Packages with contents related to each other are

number, and each package and part of a package usually grouped. The accompanying listing giveshas its own part number. The part numbers of matting index number, part number, description, and units

components in the packages are listed, in breakdown per assembly for each part. Index numbers are not

order, along with the package part numbers. Every given to parts included but not shown.

14-1

Sictlon XIV NAVAIR 51.60A.1Group Assembly Parts List

MAT DATA NOTE:

(ACTUAL QTY’S USED FOR INSTALLATION) Location of item. 4. 5_A & 7 for

typical Irmollotion. Quantity and

location may vary for specificVTOL inttallation depending soil

AREA QTY-6FT QTY-12FT 50. FTand <’"viro"’"’"tal conditions-

Q 36 198 5,184

i-P28 ^-^-C^^X’"""""’--F28

(2&3) ’OSN^ ^sf^^’’^^^ (6)

rzB(4)

Figure 14-1. VTOL Matting Installation. Forward Operating Site (Sheet 1 of 2)

FIGURE UNITS USABLE

AND PART DESCRIPTION PER ON

INDEX NO. NUMBER 2 3 4 5 6 7_____________________________ ASS’Y. _CODE

14.1 516325-1 MATTING INSTALLATION, VTOL Forward landing site Re(

-Fl 511152-1 PACKAGE ASSY AIRCRAFT TIEDOWN (see figure 14-9)

-F27 615527-1 PALLET AND MAT ASSEMBLY, AM-2, Mod 4 (see figure

14-19) 13

-F28 613600-1 PALLET ASSEMBLY, Edge clamps and stakes (see

figure 14-22) 1

14.2

NAVAIR 51-60A-1 Section XIVGroup Assembly Ports List

MATTING COMPONENTS

PKG PACKAGE ___________________PACKAGE CONTENTS______________ QTY/NO. PART NO. DESCRIPTION ITEM PART NO. QTY/PKG BMSTL

Fl 511152-1 TIEDOWNS, AIRCRAFT 416557-1 120 120

F27 615527-1 MAT ASSY, 2FT x 12FT 2 615526-1 16 208MAT ASSY, 2FT x 6FT 3 615526-2 4 52

F-28 615600-1 EDGE CLAMP, TYPE 4 512596-1 25 25

EDGE CLAMP, TYPE II 5 512597-1 25 25EDGE CLAMP, TYPE III 6 512598-1 40 40EDGE CLAMP, TYPE IV 7 512599-1 40 40

Figure 14-1. VTOL Matting Installation, Forward Operating Site (Sheet 2 of 2)

14.3

Section XIV NAVAIR 51.60A.1Group Acrmbly Port* List

NOTE: MAT DATALocation of items 19,20,21 & 22 is fortypical Installation. Quantity and (ACTUAL QTY’S USED FOR INSTALLATION)

location may vary for specific VSTOLinstallation depending soil and

AH’7A n-T-V fV-T HTV OFTenvironmental conditions. ARJ-’1 QTY-6FT OTY-lZf I gQ pT

NOTE: (C) 75 1050 26,100Heavy duty matting not ^\ fiO 330 8,640included in total. ^ ^ ^ ^^g

(4) 236 1416 36,816

Q _____4 33 840

TOTAL 435 3231 82,764

F28-^ ^ ^g

^-^^^^3^3^^(^8

(17&18)

Figure 14-2. VSTOL Uatfing Installation (Direct) Forward Operating Facility (Sheet 1 of 2)

FIGURE "UNITS USABLE


INDEX NO. NUMBER 2 3 4 5 6 7______________________ ASS’Y. CODE

14-2 617260-1 MATTING INSTALLATION (DIRECT), VSTOL Ref

Forward Operating Facility

-Fl 511152-1 PACKING ASSEMBLY, AIRCRAFT TIEDOWN (see

figure 14-9) 2

-F13 610860-1 KEYLOCK AND PALLET ASSEMBLY (see Figure 14-13)

-F18 614589-1 PACKAGE ASSEMBLY, BLAST DEFLECTOR ADAPTER(see figure 14-14) 1

-F25 615285-1 PALLET AND SPACER ASSEMBLY, AM-2 MOD4 (see

figure 14-17) 1

-F26 616003-1 PALLET AND MAT ASSEMBLY (see figure 14-18) 5-F27 615527-1 PALLET AND MAT ASSEMBLY, AM-2, MOD4 (see

figure 14-19) 202-F28 615600-1 PALLET ASSEMBLY, EDGE CLAMPS AND STAKES (see

figure 14-22) 2

-F29 615524-1 KEYLOCK PALLET ASSEMBLY, ADJUSTABLE (see

figure 14-21) .. 1

-F31 616095-1 ADJUSTABLE 90 CONNECTOR PALLET (seefigure 14-25)

^-SF1 612137-1 REPLACEMENT MAT AND PALLET ASSEMBLY (seefigure 14-23) 2

14-4

NAVAIR 51.60A.1 Section XIYGroup Assembly Parts List

T-5I3579-1 (REF) ,-615526-1 (REF) ,-613593-1 (REF)/ 615526-2 (REF) / CENTERLINE LIGHT

*---18 (REF)--\---------<------ 30 FT-0----\-f-- *--- 9 1/2 (REF)---/------\, / --43/4(REF)-- y< W^w^^^^^^y^S^rt f^^RS^S^ SS^S. i-ig^JLJtfJO^K^ ^^^^$^^!^^\\-fSECTION A-A

413370-1513850-2 (REF)-, STARTER-n. ^-5)3850-1 (REF)

\ KEYLOCK \ /--\.--------------V--120 FT.O APPROX (REF)----------------------^----)

p^s^^^^a^ "~^^^^^c^SECTION B-B

MATTING COMPONENTS

PKG PACKAGE __________________PACKAGE CONTENTS_______________ QTY/NO. PART NO. DESCRIPTION ITEM PART NO. QTY/PKG INSTL

Fl 511152-1 TIEDOWNS, AIRCRAFT (1) 416557-1 120 240

F13 610860-1 KEYLOCK ASSY, STARTER 12FT (2) 413370-1 9 9

KEYLOCK ASSY, STARTER 3FT (3) 413370-3 1

KEYLOCK ASSY, STARTER 9FT (4) 413370-4 1 1

KEYLOCK ASSY, TYPICAL 12FT (5) 508389-1 60 60


KEYLOCK ASSY, TYPICAL 9 FT (7) 508389-4 10 10KEYLOCK ASSY, FEMALE 12FT (8) 417034-1 9 9KEYLOCK ASSY, FEMALE 3FT (9) 417034-3KEYLOCK ASSY, FEMALE 9FT_____________ (10) 417034-4

F18 614589-1 ADAPTER, TYPE I, BLAST DEFLECTOR (11) 416875-1 200 200

ADAPTER, TYPE 2, (12) 416876-1 120 120

ADAPTER, TYPE 3_____________________ (13) 416877-1 120 120

F25 615285-1 SPACER ASSY, 1FT x 12FT (14) 615286-1 25 25SPACER ASSY, 2FT 6FT________________ (15) 615286-2 6 6

F26 616003-1 MAT ASSY, 6FT, CROSSDECK AND GUIDE RAIL (16) 513579-1 16 80

F27 615527-1 MAT ASSY, 2FT x 12FT (17) 615526-1 16 3232MAT ASSY, 2FT 6FT___________________ (18) 615526-2 4 808

F28 615600-1 EDGE CLAMP, TYPE (19) 512596-1 25 50EDGE CLAMP, TYPE II (20) 512597-1 25 50EDGE CLAMP, TYPE III (21) 512598-1 40 80

EDGE CLAMP, TYPE IV__________________ (22) 512599-1 40 80

F29 615524-1 KEYLOCK ASSY, ADJ., MALE 6FT (23) 511871-1 2 2KEYLOCK ASSY, ADJ., MALE 3FT (24) 511871-2 4 2KEYLOCK ASSY, ADJ., FEMALE 6FT (25) 511875-1 2 2

KEYLOCK ASSY, ADJ., FEMALE 3FT (26) 511875-2 4 4KEYLOCK ASSY, ADJ., RIGHT 12FT (27) 614554-1 20 20

KEYLOCK ASSY, ADJ., LEFT 12FT__________ (28) 614554-2 20 20

F31 616095-1 90 CONNECTOR ASSY, ADJUSTABLE (29) 513850-1 21 21

90 CONNECTOR ASSY, ADJUSTABLE________ (30) 513850-2 21 21

SF1 612157-1 REPLACEMENT MAT ASSY (3D 508386-1 12 24

Figure 74-2. VSTOL Morfi’ng Installation (Direct) Forward Operating Facility (Sheet 2 or 2)

14.5

Section XIV NAVAIR 51.60A.1Group Acsembly Ports Lit

NOTE: MAT DATALocation o( items 19,20,21 & 22 is (or

typical Installation. Quantity and (ACTUAL QTY’S USED FOR INSTALLATION)location may vary for a specific VSTOLinstallation depending soil and f^TV 1’)TTT

environmental conditions. AREA QTY-6FT QTY-12FT gQ. FT

NOTE: (C) 75 1050 26,100Heavy duty matting not (^) 24 132 3,436included in total. ^ ^ ^ ^^(f) 236 1416 36,816

Q 4 33 840

TOTAL 399 3035___ 77,560

,--^||&:----F28 (20) F2B(22)-^^ ^F28 (20)

F3I <29)-^^^^?^^^’F28 (21) ^--^^^^. C4^^.^^^^^

V^^T’T^l’^^V (R) ^^^^^0^)INSTALLATION / ^i^, --^---^

F27 (17, 1’6)

Figure 14-3. VSTOL Hatting Installation (Conversion) Forward Operating Facility (Sheet of 2)

FIGURE UNITS L.SAItl.1:

AND PART DESCRIPTION PHK "’<

INDEX NO. NUMBER 2 3 4 5 6 7_____________________________ ASS’V. ’01)1

14-3 617260-2 MATTING INSTALLATION (CONVERSION), VSTOL Ref



figure 14-9)

-F13 610860-1 KEYLOCK AND PALLET ASSEMBLY (see figure 14-13)

-F18 614589-1 PACKAGE ASSEMBLY, HLAST DEFLECTOR ADAPTER(see figure 14-16)


figure 14-17)

-F26 616003-1 PALLET AND MAT ASSEMBLY (see figure 14-18) 5

-F27 615527-1 PALLET AND MAT ASSEMBLY, AM-2, MOD4 (see

figure 14-19) 190

-F28 615600-1 PALLET ASSEMBLY, EDGE CLAMPS AND STAKES

(see figure 14-22)


figure 14-21)

-F31 616095-1 ADJUSTABLE 90 CONNECTOR PALLET (seefigure 14-25) 1

-SF1 612137-1 REPLACEMENT MAT AND PALLET ASSEMBLY (see

figure 14-23) 2

14-6


c-513579.1 (REF) /-615526-1 (REF) ,-613593.1 (REF)

Y’33’ 615526.2 (RE F) / CENTERLINE LIGHT

----18 (REF)--\--------+-------30 FT-0----\-^- *--- 9 1/2 (REF)--j------\ / -*-4 3/4 (REF)*- y

’^q^rr^q "~T^^^^^^SECTION A-A

MATTING COMPONENTS

PKG PACKAGE ___________________PACKAGE CONTENTS______________ ^y/NO. PART NO. DESCRIPTION ITEM PART NO. QTY/PKG INSTL

_F_l____511152-1 TIEDOWNS AIRCRAFT___________________ (1) 416557-1 120 240

F13 610860-1 KEYLOCK ASSY, STARTER 12FT (2) 413370-1 9 9KEYLOCK ASSY, STARTER 3FT (3) 413370-3KEYLOCK ASSY, STARTER 9FT (4) 413370-4KEYLOCK ASSY, TYPICAL 12FT (5) 508389-1 60 60KEYLOCK ASSY, TYPICAL 3FT (6) 508389-3 10 10KEYLOCK ASSY, TYPICAL 9FT (7) 508389-4 10 10KEYLOCK ASSY, FEMALE 12FT (8) 417034-1 9 9KEYLOCK ASSY, FEMALE 3FT (9) 417034-3 1KEYLOCK ASSY, FEMALE 9FT_____________ (10) 417034-4

F18 614589-1 ADAPTER, TYPE I, BLAST DEFLECTOR (11) 416875-1 200 200ADAPTER, TYPE 2 (12) 416876-1 120 120ADAPTER, TYPE 3_____________________ (13) 416877-1 120 120

F25 615285-1 SPACER ASSY, FT 12FT (14) 615286-1 25 25SPACER ASSY, 1FT x 6FT (15) 615286-2 6 6

F26 616003-1 MAT ASSY 6FT, CROSSDECK AND GUIDE RAIL (16) 513579-1 16 80

F27 615527-1 MAT ASSY, 2FT x 12FT (17) 615526-1 16 3040MAT ASSY, 2FT x 6FT (18) 615526-2 4 760

F28 615600-1 EDGE CLAMP, TYPE (19) 512596-1 25 25EDGE CLAMP, TYPE II (20) 512597-1 25 25EDGE CLAMP, TYPE III (21) 512598-1 40 40EDGE CLAMP, TYPE IV__________________ (22) 512599-1 40 40

F29 615524-1 KEYLOCK ASSY, ADJ., MALE 6FT (23) 511871-1 2 2

KEYLOCK ASSY, ADJ., MALE 3FT (24) 511871-2 4 2

KEYLOCK ASSY, ADJ., FEMALE 6FT (25) 511875-1 2 2


KEYLOCK ASSY, ADJ.. LEFT 12FT__________ (28) 614354-2 20 20

F31 616095-1 90 CONNECTOR ASSY, ADJUSTABLE (29) 513850-1 21 2190 CONNECTOR ASSY, ADJUSTABLE________ (30) 51.3850-2 21 21

SFI 612157-1 REPLACEMENT MAT ASSY (31) 508386-1 12 24

F;9ire 14-3. VSTOL Matting Installation (Conversion) Forward Operating Facility (Sheet 2 of 2)

14.7

Sectioni XIV NAVAIR 51-60A-1Group Assembly Parts List

NOTE! MAT DATALocation of items )9, 20, 21 & 22 is fortypical Installation. Quantity and (ACTUAL QTY’S USED FOR INSTALLATION)

location may vary for specific VSTOLinstallation depending soil and TOTALenvironmental conditions. AREA QTY-6FT QTY-12FT gQ ^

75 1050 26,10060 330 8,640

300 1800 46,800TOTAL 435 3180 81,540

F58 d’?\

^^-^:>^,--F28 (20)F28 (22)"^ /^O8)

F3’ (29)^^^^^^<^8i13) (2 3 8. 4) ^/-1^^^^^-^^’^^^^F2Ba9)-^ /^. (I) ^^^^ 8^^^, ^^-^^’’’’’^"^ A

(17 & 18)

Figure 74-4. VSTOL Matting Installation (Hot Expandable) (Sheet 1 of 2)

FIGURE UNITS USA HI. I:AND PART DESCRIPTION PER ON

INDEX NO. NUMBER 2 3 4 5 6 7______ ASS’Y. COPE

14-4 617260-3 MATTING INSTALLATION (NO EXPANSION) VSTOL Ref


-Fl 511152-1 PACKING ASSEMBLY, AIRCRAFT TIEDOWN (seefigure 14-9) 2

-F13 610860-1 KEYLOCK AND PALLET ASSEMBLY (see figure 14-13)-F18 614589-1 PACKAGE ASSEMBLY, BLAST DEFLECTOR ADAPTER

(see figure 14-16)-F25 615285-1 PALLET AND SPACER ASSEMBLY, AM-2 MOD4 (see

figure 14-17) .-F27 615527-1 PALLET AND MAT ASSEMBLY, AM-2, MOD4 (see

figure 14-19) 199-F28 615600-1 PALLET ASSEMBLY, EDGE CLAMPS AND STAKES (see

figure 14-22) 2-F29 615524-1 KEYLOCK PALLET ASSEMBLY, ADJUSTABLE (see

figure 14-21)

-F31 616095-1 ADJUSTABLE 90 CONNECTOR PALLET (see

figure 14-25) 1-SF1 612137-1 REPLACEMENT MAT AND PALLET ASSEMBLY (see

figure 14-23) 2

14-8

NAYAIR 51-60A-1 Section XIVGroup Assembly Parts List

,-513579.1 (REF) /-615526-1 (REF) /-613593-1 (REF)r 615526.2 (REF) / CENTERUNE LIGHT

----18 (REF)--^--------<------30 FT.O----\ *---9 1/2 (REF)--f------\ / -.43/4 (REF)*. ,/

Fio^^^g^"~T^^-^!’^SECTION A.A

MATTING COMPONENTS

PKG PACKAGE ___________________PACKAGE CONTENTS______________ Q^Y/NO. PART NO.__________DESCRIPTION__________ ITEM PART NO. QTY/PKG INSTL

Fl 511152-1 TIEDOWNS AIRCRAFT___________________ (1) 416557-1 120 240

F13 610860-1 KEYLOCK ASSY, STARTER 12FT (2) 413370-1 9 9


KEYLOCK ASSY, STARTER 9FT (4) 413370-4KEYLOCK ASSY, TYPICAL 12FT (5) 508389-1 60 60



KEYLOCK ASSY, FEMALE 12FT (8) 417034-1 9 9

KEYLOCK ASSY, FEMALE 3FT (9) 417034-3KEYLOCK ASSY, FEMALE 9FT (10) 417034-4 1

F18 614589-1 ADAPTER, TYPE I, BLAST DEFLECTOR (11) 416875-1 200 200

ADAPTER, TYPE 2 (12) 416876-1 120 120

ADAPTER, TYPE 3_____________________ (13) 416877-1 120 120

F25 615285-1 SPACER ASSY, 1FT x 12FT (14) 615286-1 25 25

SPACER ASSY, 2FT 6FT________________ (15) 615286-2 6 6

F27 615527-1 MAT ASSY, 2FT x 12FT (16) 615526-1 16 3184MAT ASSY, 2FTx 6FT___________________ (17) 615526-2 4 796

F28 615600-1 EDGE CLAMP, TYPE (18) 512596-1 25 50

EDGE CLAMP, TYPE II (19) 512597-1 25 50

EDGE CLAMP, TYPE III (20) 512598-1 40 80

EDGE CLAMP, TYPE IV________ (21) 512599-1 40 80

F29 615524-1 KEYLOCK ASSY, ADJ., MALE 6FT (22) 511871-1 2 2

KEYLOCK ASSY, ADJ., MALE 3FT (23) 511871-2 4 2KEYLOCK ASSY, ADJ., FEMALE 6FT (24) 511875-1 2 2


KEYLOCK ASSY, ADJ., LEFT. 12FT (27) 614354-2 20__ 20

F31 616095-1 90 CONNECTOR ASSY, ADJUSTABLE (28) 513850-1 21 2190 CONNECTOR ASSY, ADJUSTABLE_______ (29) 513850-2 21___ 21

SF1 612157-1 REPLACEMENT MAT ASSY (30) 508386-1 it 24

Figure 14-4. VSTOL Marring Installation (Not Expandable) (Sheet 2 or 2)

14-9

Section XIV NAVAIR 51-60A-1Group Assembly Ports List

MAT DATA

(ACTUAL QTY’S USED FOR INSTALLATION)

TOTALAREA QTY-6FT QTY-12FT g? p.^.

(C) 180 3510 86.400(y 60 330 8,640

Q 60 393 10,152(R) 979 6269 162,204

Q 60 393 10,152

(C) 60 330 8,640

Q 120 660 17,280

Qy 981 2310 67,212 v^ F31 W}-, W

(C) 21 42 1’260 F’ (1)V\^--^V/ F3^ (30)TOTAL 2521 14,237 371,940* ^^--’"’ X1^Fn <2’3’’0

Heavy duty matting not included in total âr-’^â- Ôlj37j (Ktr/ ^-îc^^’’^^^ ^^Bbt-^"?^r-CENTERLlNE .-^^L ^’y-T

DETAIL M^ ,,, r^ ^V l-IGHn.r^^c^ / / LF"rF13(^7, (,,/^ ’5’6’U^::^^ DETA1L N

Â-^, ,a,--7’S ’^ --S’^^-^^^^^ ’t ARRESTING(%^jS?^--A^&c^^;^B’3^S^’^~’’’^ I-F26 ARRESTING GEAR

F28-^3"f^^ê^B^^ (16) GEAR

DETAIL a^?^^^-^^’ ---(9^^/ ^-DETAIL C

F31 (29)-’ .F31 (30)F13 (2, 3 & 4)

Figure 14-5. SATS Mofring /nsro/hrtion (Direct fSheef o/ a

FIGURE ~"NITS USAB1.L


INDEX NO. NUMBER 1 2 3 4 5 6 7_____________________________ ASS-Y. CODE

14-5 617261-1 MATTING INSTALLATION-DIRECT Shon Airfield for Ref

Tactical Support


figure 14-9) 3

-F13 610860-1 KEYLOCK AND PALLET ASSEMBLY (see figure 14-13) 5

-F18 614589-1 PACKAGE ASSEMBLY, BLAST DEFLECTOR ADAPTER(see figure 14-16)


figure 14-17)

-F26 616003-1 PALLET AND MAT ASSEMBLY (see figure 14-18) 49

-F27 615527-1 PALLET AND MAT ASSEMBLY, AM-2, MOD4 (see

figure 14-19) 890

-F28 615600-1 PALLET ASSEMBLY, EDGE CLAMPS AND STAKES (see

figure 14-22) 3


figure 14-21) 2

.F31 616095-1 ADJUSTABLE 90 CONNECTOR PALLET (see

figure 14-25) 2

-SF1 612137-1 REPLACEMENT MAT AND PALLET ASSEMBLY (see

figure 14-23) 4

14-10


______MATTING COMPONENTS_____________________________PKG PACKAGE ___________________PACKAGE CONTENTS_______________ QTY/NO. PART NO. DESCRIPTION ITEM PART NO. QTY/PKG INSTL


F13 610860-1 KEYLOCK ASSY, STARTER 12FT (2) 413370-1 9 36KEYLOCK ASSY, STARTER 3FT (3) 413370-3 4





KEYLOCK ASSY, STARTER 12FT (8) 417034-1 9 36KEYLOCK ASSY, STARTER 3FT (9) 417034-3 7 4

KEYLOCK ASSY, STARTER 9FT____________ (10) 417034-4 4

F26 616003-1 MAT ASSY, 6FT, CROSS DECK AND GUIDE RAIL (11) 513579-1 16 704

F27 615527-1 MAT ASSY, 2FT x 12FT (12) 615526-1 16 10,992MAT ASSY, 2FT x 6FT__________________ (13) 615526-2 4 2748

F28 615600-1 EDGE CLAMP, TYPE (14) 512596-1 25 25

EDGE CLAMP, TYPE II (15) 512597-1 25 25

EDGE CLAMP, TYPE III (16) 512598-1 40 40

EDGE CLAMP, TYPE IV_________________ (17) 512599-1 40 40

F29 615524-1 KEYLOCK ASSY, ADJUSTABLE, MALE 6FT (18) 511871-1 2 2

KEYLOCK ASSY, ADJUSTABLE, MALE 3FT (19) 511871-2 4 4KEYLOCK ASSY, ADJUSTABLE, FEMALE 6FT (20) 511875-1 2 2

KEYLOCK ASSY, ADJUSTABLE, FEMALE 3FT (21) 511875-2 4 4

KEYLOCK ASSY, ADJUSTABLE, RIGHT I2FT (22) 614354-1 20 20

KEYLOCK ASSY, ADJUSTABLE, LEFT 12FT (23) 614354-2 20 20

F31 616095-1 90 CONNECTOR ASSY, ADJUSTABLE (24) 513850-1 21 21

90 CONNECTOR ASSY, ADJUSTABLE______ (25) 513850-2 21 21

SF1 612157-1 REPLACEMENT MAT ASSY (26) 508385-1 12 24

Figure 14-6. SATS Matting Installation fConversion-VSTOL to SATS) (Sheet 2 of 2)

14.13

Section XIV NAVAIR 51-60A-1Group Afmbly Port* Ut

c’jo

in * ^i" \ DETAIL M /-F13\3f m-V / /A 1H

f7 PLACES! ^< /F13-i ’’s^^k. \ / (5 PLACES)

Fl a)^(29^^ ^^^^^TA1L^ ^ ((326’3 & 4)

DETA,L^-^\-^^ (P6LA7C&ES8{ DETA1L D^/-v^^.C^^^CS-^6^3593.^ (REF) Y ’^F26(16) MAT DATAS?2-S<^Btei--3C^’^ ItJF’ /

(?) ~’<^^W?^DETAII- c Ll^^ /’^-<’^-77\V^^ / (ACTUAL QTY’S USED FOR INSTALLATION)

<^--^^7^ / \ \ \ .ARRESTING-^ -----------------------TOrAL^(5.6 FT*) / \ (C) X, GEAR ^-s^^ QTY-6FT QTY-12FT SQ FT

<4 PLACES) t- F13 \ ’-F13 (2.3&4) ______---------------------^----(2. 3 & 4) \ F31 (30) (j\ H28 32,177 795,784

\_c- (2) 60 330 8,640--r-27 ^^O7. 18) (j) 60 399 10,152

(R) 979 6,269 162,204

Q 60 393 10,152

Qy 60 330 8,640NOTE: (?) 446 3,338 88,824Location of items 14, 15, 16 and 17 for ^M OS1 2 310 67 21^typical installation. Quantity and

location n,ay vary for specific EA (C) 448 3,360 86,016

installation depending soil and (10) 21 42 1,260environmental conditions. TOTAL 4243 48,957 T,22’5.88i7’’

Heavy duty matting not included in total.

FIGURE UNITS L’SABl.K


INDEX NO. NUMBER 2 3 4 5 6 7_______ ASS’Y. COOK

14-7 617262-1 MATTING INSTALLATION-DIRECT EXPEDITIONARY Ref

AIRFIELD-Fl 511152-1 PACKING ASSEMBLY, AIRCRAFT TIEDOWN (see

figure 14-9) 4-F13 610860-1 KEYLOCK AND PALLET ASSEMBLY (see figure 14-13) 9-F18 614589-1 PACKAGE ASSEMBLY, BLAST DEFLECTOR ADAPTER

(see figure 14-16) 2

-F25 615285-1 PALLET AND SPACER ASSEMBLY, AM-2 MOD4 (seefigure 14-17) 2

-F26 616003-1 PALLET AND MAT ASSEMBLY (see figure 14-18) 49-F27 615527-1 PALLET AND MAT ASSEMBLY, AM-2, MOD4 (see

figure 14-19) 3060-F28 615600-1 PALLET ASSEMBLY, EDG3 CLAMPS AND STAKES (see

figure 14-22) 4-F29 615524-1 KEYLOCK PALLET ASSEMBLY, ADJUSTABLE (see

figure 14.21) 4-F31 616095-1 ADJUSTABLE 90 CONNECTOR PALLET (see

figure 14-25) 2-SF1 612157-1 REPLACEMENT MAT AND PALLET ASSEMBLY (see

figure 14-23) g

Figur* 14-7. Expeditionary Airfield Mailing Installation (Direct) (Sheet 1 of 2)

14-14

HAYAIR 51.40A.1 S.ctloa XIVGroup A**mbly Part* List

nnso-a (REP)-, (-SIMS&-UREF)

^^4ia^>ii^^^ "-liT^^^^^s^^^2223!f^^fe^^^^^^^M^JLt 1 ^r ---l^_- -___LJ__^-^

41337M-’ MATTING COMPONENTSSTARTER ,_____-__________,---------------------------------------------------------|------KEYLOCK lECTIOHA-A

p^ PACKAGE _________________PACKAGE CONTENTS_____________ QTY/

NO. PART NO._________DESCRIPTION___________ ITEM PART NO. QTY/PKG INSTL

S13W-1 (REP)-. (.CATAPULT y-31357.l (REP) C RUNWAY Fl ~"5U152-1 TIEDOffNS. AIRCRAFT_________________ Jl)^ 416557.1 120 480

JV^-- ^Âsl tagâg^l fP e?^ Z^W33&a ^WV/^ ----feSS^^^ ’^^gy^ F" 6l0860-l KEYLOCK ASSY, STARTER 12FT (2) 413570-1 9 I

^: -Ô E^^^^^Q^^Ê._-:^^^^^S KEYLOCK ASSY. STARTER 3FT 0) 413370.3 1 9

< l^ 41 4 KEYLOCK ASSY. STARTER 9FT (4) 413370-4 1 9

41353S.1 (REP^-7 (13S93-1 (REP)-7 <H52<-1 (REP)-/ KEYLOCK ASSY, STARTER 12FT (5) 508389-1 60 540WOE RAIL

.CT^W K.KCEHTERLIME LIGHT A1352<-2 (REP) KEYLOCK ASSY, STARTER 3FT (0 508389-3, 10 90

SîmN ^-DKEYLOCK ASSY. STARTER 9FT (7) 508389-4 10 90

KEYLOCK ASSY. STARTER 12FT (8) 417034-1 9 81

fT^ fJ 1^1 1-1 ! f "r ^ "^ KEYLOCK ASSY. STARTER 3FT (9) 417034-3 1 9

"’/ "ft 1124M-1 (REF>-^ ^H KEYLOCK ASSY, STARTER 9FT___________ (10) 417034- 1 9/ y II Al?49&1 fREF) yl

/ // -4- I ^^, / / /\^ 614589.1 ADAPTER. TYPE I, BLAST DEFLECTOR (ID 416B75-1 200 400

/ / ^/ /"_"" ""^ !L J ~:l’a’y’"- \/’ /’Â ADAPTER, TYPE 2. BLAST DEFLECTOR <l2) 416876-1 120 240

<////. -rtT’ <Ty = --:---^.^ (REP) : = : = ^ ^:: :?t) ,^ ADAPTER. TYPE >. BLAST DEFLEOOR 03) 416877.1 I2g_ _j40^

/~~ /^\ Ar / *- ^^--^/ ^ M ~F2r 615285-1 SPACERASSY. 1FT. 12FT (14) 615286.1 25 50

y ^ .^ :: : :^ y S_ ^ Z ^ 1 I "’/ A SPACER ASSY. 2FT6FT______________ (15) 615286.2 6 12

/ ^ ^\~ { W3t.l (REP)--- e

^ fl p^ 616003-1 MAT ASSY. 6FT. CROSS DECKAND GUIDE RAIL (16) 513579-1 16 784

’’S / n F27 615527-1 HAT ASSY, 2FT 12FT (17) 615526-1 16 48.960s l. -II MAT ASSY. 2FT x 6FT________________ (18) 615526-2 4 12.240

-J u- /^S^^SEF! ~~fU’ 615600-1 EDGE CLAMP. TYPE I (19) 512596-1 25 100

" EDGE CLAMP. TYPE U 00) 512597-1 25 100

DETAIL C DETAIL 0EDGE CLAMP. TYPE 01 (21) 512598-1 40 160

--_.,, EDGE CLAMP. TYPE W_______________ (22) 512599-1 40 160J U k-jfl-a ^-TYPE U GO) -----------------------------------/\ / F29 615524-1 KEYLOCK ASSY. ADJUSTABLE. MALE 6FT (23) 511871-1 2

j ’^p-^ ^.fL- KEYLOCK ASSY, ADJUSTABLE, MALE 3FT (24) 511871-2 4 16

^(\ \\ T T\ ---_ ^-< 4 KEYLOCK ASSY. ADJUSTABLE. FEMALE 6FT (25) 511875-1 2

C y\ \ ’--\- KEYLOCK ASSY. ADJUSTABLE, FEMALE 3FT (26) 511875-2 4 16M ^---^ IL >q U KEYLOCK ASSY. ADJUSTABLE, RIGHT 12FT (27) 614354-1 20 80

tf T^l’^’-^X -A -TUXTa ’’ "V

--+/--KEYLOCK ASSY. ADJUSTABLE. LEFT 12FT (28) 614354-2 20 M

^^^-^J ^^^^ -^^^ I^T ^^Â--\-f TTPEm-1 WF7 ^’ * j .^-TYPEinOl) F31 616095-1 90CONNECTOR ASSY. ADJUSTABLE (29) 513850-1 21 B4

J^J 01) (REPt .r-t^fTtUrT-P-4-^ r-13 ___t y^^QNNECTORASS-f. AOJUSTABLE_______ <30) -513850-2 2t 94

DETAIL H DETAIL N SFI 612157-1 REPLACEMENT MAT ASSY_______ (3D 508386.1 12 96

W MATS ^--* FT MAT ’-----’----------’----------------------------"20.12 FT &1*4 FT MATS Fiyun 14-7. ExfJifiwwry AhfhU MattingDAGGERED) ^-12 PT MAT hstaHotiw (Dh^t) (Sh^t 2 of 2)

-I-"""’ ^tK t ’:: -PROVIDE APPBOX. - W r~TYPE I--~^ 4? \ ---?-----^ 133 ROWS AS SHOWN -^__-.n ^--^- N. TOR EACH ^ -Y^ /0 _^--, 1\ I* IHSTALLAT10M ^- 1 ri /

___| | IMAREA ^-1 ^---TYPE B (23)

^-^ -----J OCTAIL " (1 "^-----TYPEKDTYPEff----31 ---/ ’* --f-01) T --/-t---^ _/ -*,’U-12

OCTAIL P DETAIL Q

14.15

Section XIV MAYA1R 5MOA-1Group Acwnbly Parts Llt

-5 ^,, Tt’TAIL .*

(7 PLACES)

DETAIL R-i ^--^t^^^ ’^^^^R^^’^’^’^^"

y--TYPE n (20) _^-< ’^^’^\. ^’>-^^^-yyC^S^^ DCTAILt<

<< ^__ ^^^-^-TYPE m (21) J ^"^^-TTPE HI (21) ^k ^-^fZ^’^^1^^’-= DETAIL M ^^-^ wiJ 0. 3< UAT rATADETAIL M (5, A. 7)

HA I UA1A

(4 PLACES) (ACTUAL QTY’S USED FOR INSTALLATION)

TOTALAREA QTY-tiFT QTY.12FT p^

J’’ 1128 27.857 682.104446 3,353 85.824448 3.360 86.016

T------------:------n TOTAL 2022 34,570 853.944

FIGURE "~UNITS USABLE

A FT MAT AND PART DESCRIPTION PER ON

34, FT S S = ? ^ ^-^ INDEX NO. NUMBER 1 2 3 4 5 6 7 ASS’Y. CODE(REF) fc-fc- ^ -----------------------------------------14^ 617262-2; MATTING INSTALLATION-CooTefioo (SATS to Ezpedicioury Ref

39 MATS ,,(20.13 FT I Airfield)IM FTMATS ^^-13 FT MAT .p^ 511152-1 PACKING ASSEMBLY. AIRCRAFT TIEDCWN (seeSTAGGERED) ^

^ " fipae 14-9)) -F13 610860-1 KEYLOCK AND PALLET ASSEMBLY( Kpuv 14-13) 4

^-h FT MAT -F18 614589-1 PACKAGE ASSEMBLY, BLAST DEFLECTOR ADAPTER

---^^’^ (see figure 14-16) 1

^ r -F25 615285-1 PALLET AND SPACER ASSEMBLY, AM-2 MOD4 (xe

fiare 14.17) .. I-F27 615527.1 PALLET AND MAT ASSEMBLY. AM-2. MOD4 (ee

^^--u FT MAT(iture 14-19) 2161

y ^ -F28 615600-1 PALLET ASSEMBLY. EDGE CLAMPS AND STAKES (ee

’_______ J (;|ure 14-22) I_,__^--PROVIDE APPROX. 133 BOS .F29 615524-1 KEYLOCK PALLET ASSEMBLY. ADJUSTABLE (-< AS SHOWN FOB EACH

.^,,iT INSTALLATION IM AREA figwe 14.21) 2

^ -SFl 612137-1 REPLACEMENT MAT AND PALLET ASSEMBLY (xeM n(u*e 14-23) 4

OETA1L R

Fiqwv 14-8. ExpuJUIonoff Ai’f/M NoHfng lintalhllM (Conversion SATS oEfpidllioiwfr A<Wr/d ^ (SA, ] of 2)

4-16

NAVAIR 51-60A-1 Section XIVGroup Ascmbly Port* Llt

MATTING COMPONENTS

PKG PACKAGE PACKAGE CONTENTS QTY/NO. PART NO. DESCRIPTION ITEM PART NO. QTY/PKG INSTL


F13 610860-1 KEYLOCK ASSY, STARTER 12FT (2) 413370-1 9 36KEYLOCK ASSY, STARTER 3FT (3) 413370-3 1 4KEYLOCK ASSY, STARTER 9FT (4) 413370-4 4



KEYLOCK ASSY, STARTER 9FT (7) 508389-4 10 40KEYLOCK ASSY, STARTER 12FT (8) 417034-1 9 36KEYLOCK ASSY, STARTER 3FT (9) 417034-3 4

KEYLOCK ASSY, STARTER 9FT___________ (10) 417034-4_____1 4

F18 614589-1 ADAPTER, TYPE I, BLASTDEFLECTOR (11) 416875-1 200 200

ADAPTER, TYPE 2, BLAST DEFLECTOR (12) 416876-1 120 120

ADAPTER, TYPE 3, BLAST DEFLECTOR____ (13) 416877-1 ___120 120

F25 615285-1 SPACER ASSY, 1FT x 12FT (14) 615286-1 25SPACER ASSY, 2FT x 6FT (15) 615286-2 _____o 6

F27 615527-1 MAT ASSY, 2FT x 12FT (16) 615526-1 16 34,576

MAT ASSY, 2FT x 6FT____________ (17) 615526-2 _____4 8,64.

F28 615600-1 EDGE CLAMP, TYPE (18) 512596-1 25 ’25EDGE CLAMP, TYPE II (19) 512597-1 25 25

EDGE CLAMP, TYPE III (20) 512598-1 40 40EDGE CLAMP, TYPE IV________________ (21) 512599-1 40 40

F29 615524-1 KEYLOCK ASSY, ADJUSTABLE, MALE 6FT (22) 511871-1 2 4

KEYLOCK ASSY, ADJUSTABLE, MALE 3FT (23) 511871-2 4 8



KEYLOCK ASSY, ADJUSTABLE, RIGHT 12FT (26) 614354-1 20 40

KEYLOCK ASSY, ADJUSTABLE, LEFT 12FT (27) 614354-2 20 40

SF1 612157-1 REPLACEMENT MAT ASSY______________ (28) 508386-1 12 48

Figure 14-8. Expeditionary Airfield Matting Installation(Conversion SATS to Expeditionary Airfield) (Sheet 2of 2)

14-17

Section XIV nv<"n ^ ^fU-1Group Assembly Parts List

5^^^/"’^ ^ ^-- .-"----

I- ’;--, ’^a-"’ /

^ ^ ^’"^ ^-^:^--..’:^-,,-,^."’

’^ ’Y’’ r^’’’1-’- "-^8-^? ’"(^!;.

3-^ : ^^^ ^Figure 14-9. Tiedown Container (F1)

FIGURE UNITS UNITS USABLEAND

MIIURFH DESCRIPTION PER PER ONINDEX NO. ^MBfcK

2 3 4 5 6 7 ASSY INSTL CODE

14-9- 51H52-1 PACKAGE ASSEMBLY, Aircraft tiedowns-I 116557-1 TIEDOWNS 120-2 MISCELLANEOUS COMPONENTS

50904-4-1 FIXTURE, Drill 2

MS16995-78 SCREW 240GGG-D-751 DRILL, 5/16-in. dia 10

TY B; CL-1

GGG-K-275 KEY, Hex, 3/32 5TYPE I, CLGGG.K-275 KEY, Hex, 3/16 5TYPE 1,CLGGG-K-275 KEY, Hex, 5/16 5TYPE I, CLGGG-T-70 TAP, Plug, 3/8-16 20

TYI.SER. AH3LIM, ST b.

GGG-T-70 TAP, Bottoming, 3/8-16 5TY 1, SER. AH3LIM, STGGG-W-680 HANDLE, Tap 5TY II, Size 2

-3 No Number CONTAINER

14-18

NAVAIR 51-60A-1 Section XIVGroup Assembly Parts List

;^^^^^^ NOTE

$S. This pallet is no longer issued for new pro-

^S^. \^ curement, Information provided herein is

\\\;^\ \ /~ n intended for use with pallets of this type

^\ \^^^\ \ / still in use.

____________________4-^5-/ ^^ ^S

Figure 14.10. Full Mot Po,/er (F11)

FIGURE PART UNITS UNITS USABLEAND MITMRFR DESCRIPTION PER PER ON

INDEX NO.^MOUK


14-10- 610165-5 PALLET AND MAT ASSEMBLY-1 320660-1 BAR, Locking 13-2 322310-2 BOLT 4

-3 MS35690-802 NUT, Plain 4-4 AN415-2 PIN, Locking 4

-5 MS20392-6-35 PIN, Flat hd 4

-6 410567-4 FILLER, Wood 2

-7 410567-12 FILLER, Wood 2

.8 410567-18 FILLER, Wood 8

-9 323247.1 PLATE, End 2

-10 413479-1 TIE ROD 4

-11 615526-1 or MAT ASSEMBLY, 2 ft x 12 ft 11

509862-1

-12 615526-2 or MAT ASSEMBLY, 2 ft x 6 ft 2

509862-2

-13 610164-5 FRAME, End 2

14.19

Section XIV NAVAIR 51-60A.1Group Assembly Parts List

NOTE

M This pallet is no longer Issued (or pro-

,^-^^^s^S"^. curement. Information provided herein is

^/--’,^^-S^^^-^’’^ intended for use with pallets of this type

rf^^^^^"^ ’\ s\\\\ in use.

10-" ^-|2 ^9 ^-^

Figure 14.1?. Half Mar Pallet (F12)

FIGURE UNITS UNITS "USABLE"AND PART DESCRIPTION PER PER ON

INDEX NO. NUMBER 2 3 4 5 6 7 Assy ]NSTL CODE

14-11- 612915-1 PALLET AND MAT ASSEMBLY, Half mat-1 i20660-l BAR, Locking 12-2 610128-2 HALF MAT, 2 ft x 6 ft 12

612915-2 PALLET ASSEMBLY. 1

-3 322310-2 BOLT 4-4 323247-1 PLATE, End 2-5 410567-4 FILLER, Wood 2-6 410567-12 FILLER, Wood 2-7 410567-18 FILLER, Wood 8-8 413479-3 TIE ROD 4-9 610164-25 FRAME, End 2-10 AN415-2 PIN, Locking 4-11 MS35690-810 NUT 4-12 MS20392-6C35 PIN, Flat hd 4

___________________________________________________________________________I

14.20

NAVAIR 51-60A-) Section XIVGroup Assembly Ports List

NOTE /This pallet is no longer issued for pro- ’<^C^ ^-ss(R)""curement. Information provided herein is ^^’ v^. ^ ssf^’’1’^ -3-’intended for with pallets of this type ^^~ v^ ^^^!s!s^’^still in use. 7--’ ^\ ^^’esr^^

Figure 14.12. Half Mar Pa//et (F32)

FIGURE PART UNITS UNITS USABLEAND MnMRFR DESCRIPTION PER PER ON

INDEX NO.NUMBI-K


14-12- 616204-1 PALLET AND MAT ASSEMBLY-1 320660-1 BAR, Locking 20

-2 615526-2 MAT ASSEMBLY, 2 ft 6 ft 18

616204-2 PALLET ASSEMBLY (Fillet welded)

-3 616204-3 FILLER, Wood. 2

-4 616204-4 FILLER, Wood. 2

-5 616204-5 STRAPPING 71 ft

-6 616204-6 SEAL. 6-7 613371-1 FRAME, End 2

14-21

Section XIV NAVAIR 51-60A.1Group Assembly Ports List

{

^Sk

’^Y^^^^^^ ^\ r20 a 21

’e~’ "-^ II^’^T’^^^ ^II

10-’

Figure i4-73. Key/ocfc Pallt(F13)

14-22

NAVAIR 51.60A-1 Section XIVGroup Assembly Parts List

FIGUREPART UNITS UNITS USABLE

ANDMiTunPR

DESCRIPTION PER PER ONINDEX NO. NUMBfcK1 2 3 4 5 6 7 ASSY INSTL CODE

14-13- 610860-1 KEYLOCK AND PALLET ASSEMBLY

610860-2 PALLET ASSEMBLY.-1 322310-2 BOLT 4

-2 MS35690-802 NUT, Plain 4

-3 AN415-2 PIN, Locking 4

-4 MS20392-6-35 PIN, Flat hd 4

-5 323247-1 PLATE, End 2

-6 410567-12 FILLER, Wood 2

-7 410567-19 l-’ll.l-ER, Wood 8

-8 413479-1 TIE ROD 4

-9 610164-5 FRAME, End 2

-10 420235-1 TOOL, Removal 2

-11 415531-1 KEY, "T" Handle wrench, 5/16 hex. 2

-12 615526-1 MAT ASSEMBLY, 2 ft x 12 ft 2

-13 413370-1 KEYLOCK ASSEMBLY, Starter (12 ft) 9

413370-2 BAR

413371-1 KEYLOCK, Starter

MS24667-76 SCREW 2

-14 413370-3 KEYLOCK ASSEMBLY, Siarcer (3 ft)

413370-2 BAR413371-1 KEYLOCK, Starter

MS24667-7& SCREW 2

-15 413370-4 KEYLOCK ASSEMBLY, Starter (9 ft)

413370-2 BAR413371-1 KEYLOCK, Starter

MS24667-76 SCREW 2

-16 508389-1 KEYLOCK ASSEMBLY, Typical (12 ft) 60

413379-1 SCREW

508390-1 KEYLOCK, Typical 1

-17 508389-3 KEYLOCK ASSEMBLY, Typical (3 ft) 10

413379-1 SCREW

508390-1 KEYLOCK, Typical-18 508389-4 KEYLOCK ASSEMBLY, Typical (9 ft) 10

413379-1 SCREW508390-1 KEYLOCK, Typical

-19 417034-1 KEYLOCK ASSEMBLY, Female (12 ft) 9

413370-2 BAR

417034-5 KEYLOCK, Female ’.

MS24667-76 SCREW 2


413370-2 BAR 1

417034-1 KEYLOCK, Female 1

MS24667-76 SCREW 2


413370-2 BAR417034-5 KEYLOCK, Female 1

MS24667-76 SCREW 2

14.23

Section XIV NAVAIR 51-60A-Group Assembly Ports List

NOTE

Hi This pallet is no longer issued for new pro-

^--"^,i,r^, curement. Information provided herein is

Cl ^-^^^^^’.^S’^i*. intended for use with pallets of this type

^’’’.^ ^ ’_ still in use.

sss*., /"’< !;’ /. J*’ ^-^-^^’^rf^--^’^’^ ^<

<p^^s \ r /\ ^

19-^ \^-10

Figure 14-14. 90 Connector (H Type) Pallet (F14)14-24


FIGUREDART UNITS USABLE

AND MIIURFBDESCRIPTION PER ON

INDEX NO.NUMHhK

2 3 4 5 6 7 ASSY CODE

14-14- 613406-1 PACKAGE ASSEMBLY 90CONNECTOR (H TYPE) AND

PALLET-1 322310-2 BOLT 4-2 323247-1 END PLATE 2

-3 410567-21 FILLER, WOOD 4

-4 413479-1 TIE ROD 4

-5 414730-1 FILLER, WOOD 4

-6 414730-3 FILLER, WOOD 10

-7 414730-4 FILLER, WOOD 2

-8 415040-1 90CONNECTOR 42

-9 509582.1 SUPPORT 2

-10 610164-5 END FRAME 2

-11 AN415-2 LOCKING PIN 4

-12 MS20392-6C35 PIN, STRAIGHT, HEADED, DRILLED SHANK 4

-13 MS35690-802 NUT, Plain 4

14.25


^---?^’S^Sk NOTE

J< ;?^^"^ \\ This pallet is no longer issued for new pro-

\pf fe^\ ^--SS5^^\ curement. Information provided herein is

s ^^\.^-^^^^^^ \\ /~^ intended for use with pallets of this type

N^K^ \\ / still in use.

^ ^^ ^h """"^^^’^PALLET ASSY \ais^- PALLET PSSf(SPOT WELDED) (FILLET WELDED)

Figure 14-15. Pallet and Hat Assembly (F15) (Fttll Mat)

FIGURE UNITS UNITS USABLEAND M TURFR DESCRIPTION PER PER ON

INDEX NO.^MOC,K


14-15- 615599-1 PALLET AND MAT ASSEMBLY (AM-2 MOD 2)-1 320660-1 BAR, Locking 20-2 615343-1 MAT ASSEMBLY (EB welded), 2 ft x 12 ft 16-3 615343-2 MAT ASSEMBLY (EB weldrd), 2 ft 6 ft 4

615599-2 or PALLET ASSEMBLY (Spot welded) 1

615599-3 PALLET ASSEMBLY (Fillet welded) 1-4 615599-6 FILLER, Wood (Used with 615599-2) 2

615599-7 FILLER, Wood (Used with 615599-3) 2-5 615599-4 FILLER, Wood (Used with 615599-2) 2

615599-8 FILLER, Wood (Used with 615599-3) 2-6 615599-5 BLOCK, Wood (Used wih 615599-2) 2-7 615599-9 STRAPPING 120 ft-8 615599-10 SEAL. 6-9 "’095-1 FRAME, End (Used with 615599-2) 2

6i-tj71-l FRAME, End (Used with 615599-3) 2

14.26

NAVAIR 51.60A-1 Section XIVGroup Assembly Ports List

^ ’ 5555a55^ ^^’^^^^Yw

Figure 14-16. Blast Deflector Adapter Pallet (F18)

FIGURE -,ART UNITS UNITS USABLEAND MHURCR

DESCRIPTION PER PER ONINDEX NO.

"UMBE.K2 3 4 5 6 7 ASSY INSTL CODE

14-16- 614589-1 PACKAGE ASSEMBLY, Blast deflector adapters-I 320660-1 BAR, Locking 240.2 416875-1 ADAPTER, Type 200

-3 416876-1 ADAPTER, Type 2 120

.4 416877-1 ADAPTER, Type 3 120

-5 MS35338-46 WASHER, Lock .. 26.6 MS51967.8 NUT 26

-7 MS90725-60 BOLT 26

-8 508254-1 RECEPTACLE, Record

-9 410617-1 SHACKLE 4

-10 614589-2 BASE.-11 614589-3 COVER

14.27


I, 2 \

’v^Figure 14-17. Pallet and Spacer Assembly (F25)

FIGURE DART UNITS UNITS USABLEAND MitunFR

DESCRIPTION PER PER ONINDEX NO. "UMBtK


14-17- 615285-1 PALLET AND SPACER ASSEMBLY, AM-2 MOD 4-1 320660-1 BAR, Locking 4-2 320660-1 BAR, Locking 32-3 615526-1 MAT ASSEMBLY 4-4 615286-1 SPACER ASSEMBLY, I ft x 12 ft. 25

-5 615286-2 SPACER ASSEMBLY, 1 ft x 6 ft 6615285-2 PALLET ASSEMBLY 1

.6 615285-3 FILLER, Wood 2

.7 615285-4 FILLER, Wood 2

.8 615285.5 STRAPPING 120ft-9 615285-6 SEAL 6-10 613371.1 FRAME, End 2

__________* FSN-VX5680-182-8561__________14.28

NAVAIR 51-60A-1 Section XIYGroup Assembly Ports List

^-^ \

4

Figure 14-18. Heavy Duty Pallet and Mat Assembly (F26)

FIGURE DART UNITS UNITS USABLE^D MITMRFB DESCRIPTION PER PER ON

INDEX NO.NUMBh-R


14.18- 616003-1 PALLET AND MAT ASSEMBLY, Cross deck

pendant and guide rail mac

-1 322310-2 BOLT 4

-2 MS35690-810 NUT 4


-4 MS20392-6C35 PIN, Flat hd 4

-5 413479-3 TIE ROD 4

-6 616003-2 PLATE, End 2

-7 616003-3 FILLER, Wood 4

-8 616003-4 FILLER, Wood 2

.9 610164-25 FRAME, End (Weldment) 2

-10 616003-5 STRAPPING 12ft

.11 616003-6 SEAL. 2

-12 513579-1 MAT ASSEMBLY (EB Welded) 6 ft 16

.13 320660-6 BAR, Locking 16

14-29

Section XII NAVAIR 51-60A.1Group Assembly Ports List

s-y- ’\^’^ PALLET ASSY T(I^^PALLET ASSY

(SPOT WELDED) (FILLET WELDED)

Figure 14-19. Pallet and Mat Assembly (FZ7)

FIGURE UNITS UNITS USABLEAND isjnuRFR

DESCRIPTION PER PER ONINDEX NO.

’’^"f1^2 3 4 5 6 7 ASSY INSTL CODE

14-19- 615527-1 PALLET AND MAT ASSEMBLY (AM-2 MOD 4)-1 320660-1 BAR, Locking 20.2 615526-1 MAT ASSEMBLY (EB welded), 2 ft x 12 ft 16.3 615526-2 MAT ASSEMBLY (EB welded), 2 ft 16 ft 4

615527-2 or PALLET ASSEMBLY (Spoi welded) I615527-j PALLET ASSEMBLY (Fillet welded)

-4 615527-6 FILLER, Wood (Used with 615527-2) 2615527-7 FILLER, Wood (Used with 615527-3) 2

-5 615527-4 FILLER, Wood (Used with 615527-2) 2615527-8 FILLER, Wood (Used with 615527-}) 2

-6 615527.5 BLOCK, Wood (Used with 615527-2) 2-7 615527-9 STRAPPING 120 ft.8 615527-10 SEAL 6-9 615095-1 FRAME, End (Used with 615527-2) 2

613371-1 FRAME, End (Used with 615527-3) 2

14-30

NAVAIR 51.60A-1 Sction XIVGroup Ascmbly Ports List

This pallet is no longer Issued for new pro- / ^\-s^"^^,^-^^^^ (R)curement. Information provided herein is / (l---’"’"^ ^^____intended for ue with pallets of this typestill in use.

Figure 14-20. Mof End Ramp Pallet


INDEX NO. NUMBER 2 3 4 5 6 7 ASSY INSTL CODE

14-20- 614355-1 RAMP PALLET ASSEMBLY-1 322310-2 BOLT 4-2 MS35690-802 NUT 4

-3 AN415-2 PIN, Locking 4-4 MS20392-6C35 PIN, Flat hd 4-5 417298-2 FILLER, Wood. 2-6 417298-3 FILLER, Wood. 2-7 417298-1 FILLER, Wood. 2-8 323247-3 PLATE, End 2

-9 511660-1 FRAME, End 2

-10 413479-5 TIE ROD 4-11 612717-1 or MAT, End (Ramp)

615074-1 MAT, End (Ramp)

14-31

Section XIV NAVAIR 51-60A-1Group Assembly Parts List

^ "^^ ’^\ ^ / /-10,11,12.13

\^C%. J^\ / r3

_^^^^^’^ ’\ / 2 \. S^^ !?:$ 1-"?::’ )\. [~Q

’\^ ^PALLET ASSY PALLET ASSY(SPOT WELDED) (FILLET WELDED)

Figure 14-2]. Adjustable Keylock Pallet Assembly (F29)

FIGURE PART UNITS UNITS USABLEAND MUMRPR DESCRIPTION PER PER ON

INDEX NO."u1^"^^


14-21- 615524-1 KEYLOCK PALLET ASSEMBLY, Adjustable615524-2 PALLET ASSEMBLY (Spot v/elded) 1

615524-3 PALLET ASSEMBLY (Fillet welded)

-1 615524-4 FILLER, Wood 2

-2 615524-5 FILLER, Wood (Used with 615524-2). 2

615524-9 FILLER, Wood (Used with 615524-3). 2-3 615524-7 FILLER, Wood (Used with 615524-2). 2

615524-8 FILLER, Wood (Used with 615524-3). 2

-A 615524-6 BLOCK, Wood (Used with 615524-2) 2

-5 615524-10 FILLER, Wood 4

14.32

NAVAIR 51.60A.1 Section XIVGroup As*embly Parts List


Mirunc-DDESCRIPTION PER PER ON

INDEX NO. NUMBbR2 3 4 5 6 7 ASSY INSTL CODE

14-21-6 615524-11 STRAPPING 120 ft

-7 615524-12 SEAL 6-8 615095-1 FRAME, End (spoc welded) (Used with 2

615524-2)

613371-1 FRAME, End (fillet welded) (Used with 2

615524-3)-9 615526-1 or MAT ASSEMBLY, 2 ft x 12 ft 4

615534-1

-10 511871-1 KEYLOCK ASSEMBLY, Male (6 (t) 2

-11 511871-2 KEYLOCK ASSEMBLY, Male (3 ft) 4

418102-1 SCREW, Keylock (Used with 511871-1) 2

418102-1 SCREW, Keylock (Used with 511871-2) 1

MS24667-51 CAPSCREW (Used with 511871-1). 16

MS24667-51 CAPSCREW (Used with 511871-2). 8

511879-1 PLATE, Top (Used with 511871-1) 4


511872-1 KEYLOCK, Male (6 ft) (Used with 511871-1) 1

511873-1 KEYLOCK, Male (3 ft) (Used with 511871-2) 1



MS24667-51 CAPSCREW (Used with 511875-1) 16

MS24667-51 CAPSCREW (Used with 511875-2) 8



511876-1 KEYLOCK, Female (6 ft) (Used with 511875-1)

511877-1 KEYLOCK, Female (3 ft) (Used with 511875-2) 1

-14 614554-1 KEYLOCK ASSEMBLY, Adjustable, right 20

-15 614554-2 KEYLOCK ASSEMBLY, Adjustable, left 20

511871-1 KEYLOCK ASSEMBLY, Male (6 ft) (Used 2

with 614554-1)

511871-2 KEYLOCK ASSEMBLY, Male (6 ft) (Used 4

with 614554-2)

511875-1 KEYLOCK ASSEMBLY, Female (6 ft) (Used 2

with 614554-1)

511875-2 KEYLOCK ASSEMBLY, Female (6 ft) (Used 4with 614554-2)

14.33

Section XIV NAVAIR 51-60A.1Group Assembly Ports List

6 ^’1 ^- ^

Ffgvi1* 14-22. Edy Clamp and Stake Pallet (F28)

14.34

NAVAIR 51.60A.1 Saction XIYGroup Assembly Ports List

FIGURE PART UNITS UNITS USABLEAND

KinMnFnDESCRIPTION PER PER ON

INDEX NO. ^UMBKK1 2 3 4 5 6 7 ASSY INSTL CODE

14-22- 615600-1. PALLET ASSEMBLY, Edge clamps and stakes615600-2 PALLET ASSEMBLY 1

-I MS90725-113 BOLT 28-2 MS27183-18 WASHER, Flat 44-3 MS35338-48 WASHER, Lock 44-4 MS51967-14 NUT 44-5 413972-1 BAR, Retainer 2-6 MS90725-116 BOLT 16-7 417800-1 SPACER 8-8 612417-1 SIDE 2-9 612415-2 END-10 612415-3 END-11 413823-2 COVER AND GASKET ASSEMBLY-12 612552-6 BASE ASSEMBLY 1-13 512596-1 EDGE CLAMP, Type 25-14 512597-1 EDGE CLAMP, Type 2 25-15 512598-1 EDGE CLAMP, Type 3 40-16 512599-1 EDGE CLAMP, Type 4 40-17 512600-1 STAKE ASSEMBLY 120-18 320660-5 BAR, Locking 80

FSN-VX5680-182-8558

14.35

Section XIV NAVAIR 51-60A-1Group Assembly Parts List

NOTE

This pallet is no lonaer issued for new pro-

curement. Information provided herein is

intended for use with pallets of this type

still in use.

P.^----’-^^--9

^ 1^^’-^??,0-^-^ ^^ ^r ^

4-/ 14-’ -|3

Figure 14-23. Replacement Mo Pallet (SF1)

14.36

NAVAIR 51.60A.1 Section XIVGroup Assembly Ports List


MriMRpnDESCRIPTION PER PER ON

INDEX NO. l^^wo^t11 2 3 4 5 6 7 ’^SS’^ INSTL CODE

14.23. 612157-1 REPLACEMENT MAT AND PALLET ASSEMBLY612157-2 PALLET ASSEMBLY 1

-I 322310-2 BOLT 4

-2 MS35690-802 NUT, Plain 4


-4 MS20392-6C35 PIN, Flat hd 4

-5 323247-1 PLATE, End 2

-6 410567-12 FILLER, Wood 4

-7 410567-19 FILLER, Wood 8

-8 413479-1 TIE ROD 4

-9 413753-1 FILLER, Wood. 2

-10 413753-2 FILLER, Wood. 2

-11 610164-5 FRAME, End 2

-12 508386-1 REPLACEMENT MAT ASSEMBLY 12

413363-1 CONNECTOR, Male 1

413364-1 CLAMP 1

413365-1 ADAPTER, Lower 1

413366-1 ADAPTER, Middle 1

413367-1 ADAPTER, Upper 1

413380-1 CAPSCREW. 5

508387-1 REPLACEMENT MAT 1

MS16562-252 PIN, Dowel 1

MS24667-74 SCREW 10

MS51021-73 SETSCREW. 2

320660-4 LOCKING BAR 1

-13 612157-3 WRENCH, Socket hd screw, 5/32 .. 2

-14 612157-4 WRENCH, Socket hd screw, 5/16 2

14.37

Section XIV NAVAIR 51.60A-1Group Assembly Ports List

^\h ^J^>^^ \

8--^ V-7

Figure 14-24. Replacement Mat Pallet (SF2)

14-38

NAVAIR 51-60A-1 Section XIYGroup Assembly Ports List

FIGURE PART UNITS UNITS USABLEAND

MHURCDDESCRIPTION PER PER ON

INDEX NO.NUMBbK


14-24- 616205-1 REPLACEMENT MAT AND PALLET ASSEMBLYAM-2 MOD 4

616205-2 PALLET ASSEMBLY (Fillet welded) 1

-1 616205-4 FILLER, Wood 2-2 616205-3 FILLER, Wood 2

-3 616205-5 STRAPPING 120 ft

-4 616205-6 SEAL. 6

-5 613371-1 FRAME, End 2

-6 616207-1 MAT ASSEMBLY, 2 ft x 12 h 18

320660-4 BAR, Locking

413363-1 CONNECTOR, Male

413364-1 CLAMP413365-1 ADAPTER, Lower 1

413366-1 ADAPTER, Middle

413367-1 ADAPTER, Upper413380-1 CAPSCREW 5

508387.1 REPLACEMENT MATMS16562-252 PIN, Dowel

MS24667-74 SCREW 10

MS51021-73 SETSCREW 2

-7 616205-7 WRENCH 2-8 616205-8 WRENCH 2

14.39

Section XIV NAVAIR 51.60A.1Group Assembly Part* List

>1 ^___________________,o-/ M^^________Figure 14.25. Adjustable 90 Connector Pallvf (F31)

FIGURE o.o- UNITS UNITS USABLEAND M,,DI-D DESCRIPTION PER PER ON

INDEX NO.NUMBER

2 3 4 5 6 7____________ ASSY INSTL CODE

14-25- 616095-1 ADJUSTABLE 90 CONNECTOR PALLETASSEMBLY

.1 615526-2 or MAT ASSEMBLY, 2 ft x 6 ft 4615534.2

.2 513850-1 90 CONNECTOR ASSEMBLY, Adjustable 21-3 513850-2 90 CONNECTOR ASSEMBLY, Adjustable 21

513849-1 KEYLOCK ASSEMBLY, End, prongs up. 3(Used with 513850-1)

513849-2 KEYLOCK ASSEMBLY, End, prongs down 3(Used with 513850.2)

513852-1 KEYLOCK ASSEMBLY, iFemale 1616095-2 PALLET ASSEMBLY 1

-4 616095.5 FILLER, Wood 2

-5 616095-4 FILLER, Wood 2

-6 616095-3 FILLER, Wood 2-7 616095-6 FILLER, Wood 4

-8 616095-7 STRAPPING 72ft

.9 616095-8 SEAL 6-10 613371-9 FRAME, End 2

14-40

NAVAIR 51-60A-1 Section XVNunrrico) fndx

SECTION XV

NUMERICAL INDEX

15-1. PURPOSE.b. Space (Blank Column)

15-2. This section consists of an alpha-numerical6-65814-20

listing of each part number, drawing revision, andfigure and index number for quick reference to theGroup Assembly Parts List. Refer to figure 15-1 ’>This W number is generallyfor a typical Numerical Index page. used by vendors.

15-3. COLUMN IDENTIFICATION. c- Dash (-)Example: 31-61460-1

15-4. PART NUMBER. 31-61570-1312014-1

15-5. The "Part Number" column contains all part 313292-1numbers that appear in the Group Assembly Parts List.The listing is arranged alpha-numerically, that is by d- Letters A through Zletters first, then by numbers. The part number arrange- Example: 891501-1ment begins at the extreme left position and continues, 891502-1L

one position at a time, to the right. The order of pre- 891502-1Rference for the extreme left position is as follows:

e. Numerals 0 through 9a. Letters A through Z Example: 9-S-4838-1

Example: AN560-816 90056-2A301021-1B87775-14 15-6. DRAWING REVISION.

b. Numerals 0 through 9 15-7. The "Drawing Revision" column lists by numberExample: 00-42916-1 or letter, changes to drawings which have been revised

20-41600-1 to improve the configuration of equipment and reflect

606225-1 any drawing changes incorporated into the manual.

The order of preference for the second and succeed- 15-8. FIGURE AND INDEX NUMBER.ing position to the right is as follows:

15-9. The "Figure and Index Number" column listsa. Slash (/) the figure and index numbers of illustration or illus-

Example: *3/4 x 1/2 PTR-S (rations on which the part listed may be found.*3/4 x 3/8 PTR-S662918-2 15-10. SOURCE. MAINTENANCE AND RECOVER.*6-658I4-20 ABILITY (SM&R)

*This type number is generally 15-11. The "Source, Maintenance and Recoverability"used by vendors, column lists the codes used by the Joint Services.

15.1

Sctlon XV NAVAIR 51.60A-Nunrrkal Index

The uniform code format is composed of three parts number and not stocked in supplyconsisting of a two (2) position Source Code, a two system.position Maintenance Code and a one (I) positionRecoverability Code as follows: b. Maintenance Codes (2 positions) codes entered

in the third and fourth positions of the uniform codea. Source Codes (2 positions) codes entered in format are as follows:

the first and second positions in the columnindicate the source for acquiring the. item for (1) Third Position: The maintenance code

replacement purposes and the codes used in entered in the third position will indicate the lowestthis manual are as follows, maintenance level authorized to remove/replace, and

use the item.Code Definition

Code DefinitionPA Item procured and stocked for antici-

pated or known usage that is not de- 0 Support item is removed, replaced,teriorative in nature. (Normally material used at the organizational level offound on "Initial Outfitting Lists"), maintenance.

PB Item procured and stocked for insur- H Support item is removed, replaced,ance purposes because essentiality used 3; (he intermediate level of main-dictates that a minimum quantity be tenance.available in the supply system.

D Support items that are removed, re-PC Item procured and stocked and which placed, used at depot level of main-

otherwise would be coded PA except tenance-that it is deteriorative in nature.

(2) Fourth Position: The maintenance codeMO Item to be manufactured or fabricated entered in the fourth position indicates whether the

at organizational level, itgn, 15 ^ ^ repaired and identifies the lowest main-

tenance level with the capability to perform completeMH Item to be manufactured or fabricated ^pg^ ^^ remove, replace, repair, assemble and

at intermediate level. (P-.

AO Item to be assembled at organizationallevel.

Code DefinitionAH Item to be assembled at intermediate

level.

0 The lowest level capable of corn-AD Item to be assembled at depot level, plete repair of the support item is

the organizational level.XA Item is not procured or stocked be-

cause the requirements for the item H. The lowest level capable of corn-will result in the replacement of the plete repair of the support item isnext higher assembly, the intermediate level.

XB Item is not procured or stocked. If not D The lowest level capable of corn-available through salvage, requisition, plete repair of the support item is

the depot level.XC loctallation drawing, diagram, instruc-

tion sheet, field service drawing, that Z Non-repairable. No repair is author-is identified by manufacturer’s part ized.

15.2

NAVAIR 51-60A-1 Section XVNumerical Index

c. Recoverabiluy Code (1 position) code entered D Repairable item. When beyond lowerin the fifth position of the uniform format indicating level repair capability, return to depotthe desired disposition of the support item. Condemnation and disposal not author-

ized below depot level.Code Definition

Z Nonrepayable item. When unservice-0 Repairable item. When uneconomically able, condemn and dispose at the level

repairable, condemn and dispose at indicate<S in the third position.organizational level.

H Repairable item. When uneconomically d. Reserved for Service Option (1 position) Columnrepairable, condemn and dispose at 6 is reversed for internal management purposes ofintermediate level, each service. Not used in this manual.

PART DWG FIGURE AND SM & R PART DWG FIGURE AND SM & RNUMBER REV INDEX NO. CODE NUMBER REV INDEX NO. CODE

Figure 75-7. Typical Numerical Index Page

15.3

Section XV NAVAIR 51-60A-1numerical Index

PART DWG FIGURE AND SM & R PART DWG FIGURE AND SM & RNUMBER REV INDEXNO. CODE NUMBER REV INDEX NO. CODE

AN4I5-2 14 10 4 XAOZZ 320660-1 K 14 12 XAOZZ14 11 10 XAOZZ 14 15 XAOZZ^14 13 3 XAOZZ 14 l6 XAOZa14 14 11 XAOZZ 14 17 XAOZZ14 18 3 XAOZZ 14 19 XAOZZI4 20 3 XAOZZ 320660-4 K 14 23 12 XAOZZ14 23 3 XAOZZ 14 24 6 XAOZZ

GGG-D-751 14 9 2 XAOZZ 320660-5 K 14 17 2 XAOZZGGG-K-275 14 9 2 XAOZZ 14 22 18 XAOZZGGG-T-70 14 9 2 XAOZZ 320660-6 K 14 18 13 XAOZZGGG-W-680 14 9 2 XAOZZ 322310-2 B 14 10 2 XAOZZMS16562-252 14 23 12 XAOZZ 14 u 3 XAOZZ

14 24 6 XAOZZ 14 13 XAOZZMS16995-78 14 9 2 XAOZZ 14 14 1 XAOZZMS20392-6-35 14 10 5 XAOZZ 14 18 1 XAOZZ

14 13 4 XAOZZ 14 20 XAOZZMS20392-6C35 14 11 12 XAOZZ 14 23 XAOZZ

K 14 12 XAOZZ 323247-1 B 14 10 9 XAOZ214 18 4 XAOZZ 14 11 4 XAOZZ14 20 4 XAOZZ 14 13 5 XAOZZ14 23 4 XAOZZ 323247-1 B 14 14 2 XAOZZ

MS24667-51 14 21 12 XAOZZ 14 23 5 XAOZZ14 21 13 XAOZZ 323247-3 B 14 20 8 XAOZZ

MS24667-74 14 23 12 XAOZZ14 24 6 XAOZZ 410567-12 K 14 10 7 XAOZZ

MS24667-76 14 13 13 XAOZZ 14 11 6 XAOZZ14 13 14 XAOZZ 14 13 6 XAOZ214 13 15 XAOZZ 14 23 6 XAOZZ14 13 19 XAOZZ 410567-18 K 14 10 8 XAOZZ14 13 20 XAOZZ 14 11 7 XAOZZ14 13 21 XAOZZ 410567-19 K 14 13 7 XAOZ7

MS27183-18 14 22 2 XAOZZ 14 23 7 XAOZZMS35338-46 14 16 5 XAOZZ 410567-21 K 14 14 3 XAOZZMS35338-48 14 22 3 XAOZZ 410567-4 K 14 10 6 XAOZZMS35690-802 14 10 3 XAOZZ 14 n 5 XAOZZ

14 13 2 XAOZZ 410617-1 B 14 16 9 XAOZZ14 14 13 XAOZZ 413363-1 B 14 23 12 XAOZZ14 20 2 XAOZZ 14 24 6 XAOZZ14 23 2 XAOZZ 413364-1 C 14 23 12 YA077

MS35690-810 14 11 u XAOZZ 14 24 6 XAOZZ?14 18 2 XAOZZ 415365-1 C 14 23 12 XAOZZ

MS51021-73 14 23 12 XAOZZ 14 24 6 XAOZZ14 24 6 XAOZZ 413366-1 C 14 23 12 XAOZ7MS51967-14 14 22 4 XAOZZ 14 24 6 XAOZZMS51967.8 14 16 6 XAOZZ 413367.1 D 14 23 12 XA077

MS90725.113 14 22 XAOZZ 14 24 6 XAOZZMS90725.116 14 22 6 XAOZZ 413370.1 B 14 13 13 VAW7MS90725.60 14 16 7 XAOZZ 413370-2 B 14 13 13 XAOZZ320660.1 K 14 10 1 XAOZZ 413370-3 B 14 13 14 XAOZZ

14 11 1 XAOZZ 413370.4 B 14 13 15 XAOZZ

15-4

NAVAIR 51-60A-1 Section XVNumerical Index

PART DWG FIGURE AND SM & R PART DWG FIGURE AND SM & RNUMBER REV INDEX NO. CODE NUMBER REV INDEX NO. CODE

413371-1 D 14 13 13 XAOZZ 511152-1 C 14 Fl PAOHH14 13 14 XAOZZ 14 2 Fl PAOHH14 13 15 XAOZZ 14 3 Fl PAOHH

413379-1 A 14 13 18 XAOZZ 14 4 Fl PAOHH413380-1 14 23 12 XAOZZ 14 5 Fl PAOHH

14 24 6 XAOZZ 14 6 Fl PAOHH413479-1 E 14 10 10 XAOZZ 14 7 Fl PAOHH

14 13 8 XAOZZ 14 8 Fl PAOHH14 14 4 XAOZZ 14 9 PAOHH14 23 8 XAOZZ 511660-1 14 20 9 XAOZZ

413479-3 E 14 11 8 XAOZZ 511871-1 14 21 10 XAOHH14 18 5 XAOZZ 14 21 15 XAOHH

413479-5 E 14 20 10 XAOZZ 511871-2 14 21 11 XAOHH413753-1 A 14 23 9 XAOZZ 14 21 15 XAOHH413753-2 A 14 23 10 XA02Z 511872-1 14 21 11 XAOHH413823-2 14 22 11 XAOZZ 511873-1 14 21 11 XAOHH413972-1 14 22 5 XAOZZ 511875-1 14 21 12 XAOHH414730-1 D 14 14 5 XAOZZ 14 21 15 XAOHH414730-3 D 14 14 6 XAOZZ 14 21 12 XAOHH414730-4 D 14 14 7 XAOZZ 511875-2 14 21 13 XAOHH415040-1 B 14 14 8 XAOZZ 14 21 15 XAOHH415531-1 14 13 11 XAOZZ 14 21 13 XAOHH416557-1 A 14 p XAOZZ 511876-1 14 21 13 XAOHH416875-1 14 16 2 XAOHH 511877-1 14 21 13 XAOHH416876-1 14 16 3 XAOHH 511879-1 14 21 II XAOZZ416877-1 14 16 4 XAOHH 14 21 13 XAOZZ417034-1 A 14 13 20 XAOZZ 512596-1 A 14 22 13 XAOZZ

14 13 19 XAOZZ 512597-1 A 14 22 14 XAOZZ417034-3 A 14 13 20 XAOZZ 512598-1 A 14 22 15 XAOZZ417034-4 A 14 13 21 XAOZZ 512599-1 A 14 22 16 XAOZZ417034-5 A 14 13 21 XAOZZ 512600-1 14 22 17 XAOZZ417298-1 14 20 7 XAOZZ 513579-1 14 18 12 XAOHH417298-2 14 20 5 XAOZZ 513849-1 14 25 3 XAOHH417298-3 14 20 6 XAOZZ 513849-2 14 25 3 XAOHH417800-1 A 14 22 7 XAOZZ 513850-1 14 25 2 XAOHH418102-1 14 21 11 XAOZZ 513850-2 14 25 3 XAOHH420235-1 14 13 10 XAOZZ 513852-1 14 25 3 XAOHH508254-1 H 14 16 8 XAOZZ 516325-1 14 1 AOOHH508386.1 D 14 23 12 XAOHH508387-1 E 14 23 12 XAOHH

14 24 6 XAOHH508389.1 B 14 13 16 XAOZZ 610164.25 L 14 II 9 XAOHH508389-3 B 14 13 17 XAOZZ ^OHH

508389-4 B 14 13 18 XAOZZ , 10 9 XAOZZ

508390-1 C 14 13 16 XAOZZ610164-5 L 14 lo " XAOZZ

14 13 17 XAOZZ 14 13 9 XAOZZ14 13 18 XAOZZ 14 14 10 XAOZZ

509044-1 14 9 2 XAOZZ 14 23 11 XAOZZ509582.1 B 14 14 9 XAOZZ 610165-5 J 14 10 PAOHH509862-1 F 14 10 11 XAOHH 610860-1 F 14 2 F13 ’AOHH509862-2 F 14 10 12 XAOHH 14 3 Fl3 AOHH

15.5

Section XV NAVAIR 51-60A.1Numrical Index

PART DWG FIGURE AND SM & R PART DWG FIGURE AND SM & R

NUMBER REV INDEX NO. CODE NUMBER REV INDEX NO. CODE

610860-1 14 4 F13 PAOHH 14 5 F25 PAOHH14 5 F13 PAOHH 6l’i285-l B 14 7 F25 PAOHH14 6 F13 PAOHH 14 8 F25 PAOHH14 7 F13 PAOHH

^ 17 PAOHH14 8 F13 PAOHH

615285-2 B 14 17 5 XAOZZ

610860-2 14 3 ~XAOZZ 61’>285-3 B 14 17 6 XAOZZ

6^37:; : 14 \ SF1 PAOHH 615285-4 B 14 17 7 XAOZZ

14 3 SFI PAOHH 615285-5 B 14 17 8 PAOZZ

14 4 SF1 PAOHH 615285-6 B 14 17 9 PAOZZ

14 5 SF1 PAOHH 61-5286-I A 14 17 4 XAOHH

14 8 SF1 PAOHH 615286-2 A 14 17 5 XAOHH

612157-1 E 14 6 SF1 PAOHH 615343-1 A 14 15 2 XAOHH

14 7 SF1 PAOHH 615343-2 A 14 15 3 XAOHH

14 23 PAOHH 615524-1 B 14 2 F29 PAOHH

612157-2 E 14 23 XAOZZ 14 3 F29 PAOHH

612157-3 E 14 23 13 XAOZZ 14 4 F29 PAOHH

612157-4 E 14 23 14 XAOZZ 14 5 F29 PAOHH612415-2 B 14 22 9 XAOZZ 14 6 F29 PAOHH

612415-3 B 14 22 10 XAOZZ 14 7 F29 PAOHH

612417-1 14 22 8 XAOZZ 14 8 F29 PAOHH

612552-6 F 14 22 12 XAOZZ 14 21 PAOHH612717-1 14 20 11 XAOZZ 615524-10 B 14 21 5 XAOZZ

612915-1 D 14 11 615524-11 B 14 21 6 PAOZZ

612915-2 D 14 11 2 XAOZZ 615524-12 B 14 21 7 PAOZZ

613371-1 E 14 12 7 XAOZZ 615524-2 B 14 21 XAOZZ

613371-1 E 14 15 9 XAOZZ 615524-3 B 14 21 XAOZZ

14 17 10 XAOZZ 615524-4 B 14 21 XAOZZ

14 19 9 XAOZZ 615524-5 B 14 21 2 XAOZZ

14 21 8 XAOZZ 615524-6 B 14 21 4 XAOZZ

14 24 5 XAOZZ 615524-7 B 14 21 3 XAOZZ

613371-9 E 14 25 10 XAOZZ 615524-8 B 14 21 3 XAOZZ

613406-1 B 14 14 615524-9 B 14 21 2 XAOZZ

613600-1 14 F28 PAOHH 615526-1 A 14 10 11 XAOHH

614355-1 E 14 20 14 13 12 XAOHH

614554-1 14 21 14 XAOHH 14 17 3 XAOHH

614554-2 14 21 15 XAOHH 14 19 2 XAOHH

614589-1 B 14 2 F18 PAOHH 14 21 9 XAOHH14 3 F18 PAOHH 615526-2 14 10 12 XAOHH

14 4 F18 PAOHH 14 12 2 XAOHH14 5 F18 PAOHH 14 19 3 XAOHH14 7 F18 PAOHH 14 25 XAOHH14 8 F18 PAOHH 615527-1 A 14 1 F27 PAOHH14 16 PAOHH 14 2 F27 PAOHH

614589-2 14 16 10 XAOHH 14 3 F27 PAOHH614589-3 14 16 11 XAOHH 14 4 F27 PAOHH615074-1 14 20 11 XAOHH 14 5 F27 PAOHH615095-1 A 14 15 9 XAOZZ 14 6 F27 PAOHH

14 19 9 XAOZZ 14 7 F27 PAOHH14 21 8 XAOZZ 14 8 F27 PAOHH

615285-1 B 14 2 F25 PAOHH 14 19 PAOHH14 3 F25 PAOHH 615527-10 A 14 19 8 PAOZZ14 4 F25 PAOHH 615527-2 A 14 19 3 XAOZZ

615527-3 A 14 19 3 XAOZZ

15-6

-;R 51-60A-1 Section XVNunrricot Index

PART DWG FIGURE AND SM & R PART DWG FIGURE AND SM & RNUMBER REV INDEXNO. CODE NUMBER REV INDEX NO. CODE

615527-4 A 14 19 5 XAOZZ 616003-6 14 18 11 PAOZZ

615527-5 A 14 19 6 XAOZZ 616095-1 B 14 2 F31 PAOHH

615527-6 A 14 19 4 XAOZZ 14 3 F31 PAOHH

615527-7 A 14 19 4 XAOZZ 14 4 F31 PAOHH

615527-8 A 14 19 5 XAOZZ 14 5 F31 PAOHH

615527-9 A 14 19 7 PAOZZ 14 6 F31 PAOHH

615534-1 14 21 9 XAOHH 14 7 F31 PAOHH

615534-2 14 25 XAOHH 14 25 PAOHH

615599-1 A 14 15 616095-2 B H 25 3 XAOHH

615599-10 A 14 15 8 PAOZZ 616095-3 B 14 25 6 XAOZZ

615599-2 A 14 15 3 XAOZZ 616095-4 B 14 25 5 XAOZZ

615599-3 A 14 15 3 XAOZZ 616095-5 B 14 25 4 XAOZZ

615599-4 A 14 15 5 XAOZZ 616095-6 B 14 25 7 XAOZZ

615599-5 A 14 15 6 XAOZZ 616095-7 B 14 25 8 PAOZZ

615599-6 A 14 15 4 XAOZZ 616095-8 B 14 25 9 PAOZZ

615599-7 A 14 15 4 XAOZZ 616204-1 14 12

615599-8 A 14 15 5 XAOZZ 616204-2 14 12 2 XAOZZ

615599-9 A 14 15 7 PAOZZ 616204-3 14 12 3 XAOZZ

615600-1 A 14 2 F28 PAOHH 616204-4 14 12 4 XAOZZ

615600-1 A 14 3 F28 PAOHH 616204-5 14 12 5 PAOZZ

14 4 F28 PAOHH 616204-6 14 12 6 PAOZZ

14 5 F28 PAOHH 616205-1 14 24

14 6 F28 PAOHH 616205-2 14 24 XAOHH

14 7 F28 PAOHH 616205-3 14 24 2 XAOZZ

14 8 F28 PAOHH 616205-4 14 24 XAOZZ

14 22 PAOHH 616205-5 14 24 3 PAOZZ

615600-2 A 14 22 XAOZZ 616205-6 14 24 4 PAOZZ

616003-1 14 2 F26 PAOHH 616205-7 14 24 7 XAOZZ14 3 F26 PAOHH 616205-8 14 24 8 XAOZZ14 5 F26 PAOHH 616207-1 14 24 6 XAOHH14 6 F26 PAOHH 617260-1 14 2 AOOHH14 7 F26 PAOHH 617260-2 14 3 AOOHH14 18 PAOHH 617260-3 14 4 AOOHH

616003-2 14 18 6 XAOZZ 617261-1 A 14 5 AOOHH616003-3 14 18 7 XAOZZ 617261-2 A 14 6 AOOHH616003-4 14 18 8 XAOZZ 617262-1 A l4 7 AOOHH

616003-5 14 18 10 PAOZZ 617262-2 A 14 8 AOOHH

15.7

NAVAIR 51-60A-1

ALPHABETICAL INDEX

NAVAIR 51-60A.1 Alphabetical Inaex

ALPHABETICAL INDEX

Subject Page Subject Page

A F

Adapters 2-8 Female Keylock 2-5Adjustable 90 Connector 2-5 Field Configuration 1-1Adjustable Keylock Pallet 3-13,6-2,10-3 Field Laying Procedure 7-15Adjustable Keylocks 2-9,5-8,8-13 Fork Lift Truck Deployment 5-1AM-2 Matting 2-1

Mat Dimensions 2-1 GApproach Aprons 7-8

Grading 1-1B Group Assembly Parts List 14-1

Guide Rail 2-7,7-1Blast Deflector 2-7,3-8,7-17

Adapter Pallets 3-8,5-7,10-2 HInstallation 7-17

Half Mat Pallet 3-3,7-6,10-1C Hand Tools 4-1

Hard Surface Runway 1-1CBR (California Bearing Ratio) 1-1 Heavy Duty Mat Pallet 3-11,5-8,6-1Clamps, Edge 3-10 Heavy Duty Mats 2-8Connecting Bar 3-5Connector, Adjustable 3-6 IConnector Pallet, 90 3-6,6-1

Individual Mat Replacement 8-3D Inspection and Classification 11-1

Installation, Matting 7-1Deck Covering Repair 8-1 crew needed 7-1

Dents 8-1 Instructions 7-1Repair of 8-2 Sequence, SATS Field 7-1

Deployment, Pallet 5-1 with Guid^ K"! 7-1

Expeditionary Airfield 5-6 Without Guide Rail 7-1Forklift Truck 5-1 Instructions. 7-1Miscellaneous 5-7 Installation 7-1SATS Airfield 5-4 Pallet Deployment. 5-1VSTOL Airfield 5-1 Pallet Disassembly 6-1VTOL Airfield 5-1 Removal of Matting 9-1

Deployment 5-4 Repackaging Matting 10-1Depot Maintenance 11-1 Site Preparation 1-1Disassembly, Pallet 6-1 Intermediate Maintenance 12-1

E K

Edge Clamps and Stakes 3-10,5-7,10-2 Keylock 3-5.6-1,10-1Installation of 7-17 Adjustable 2-9

Edge Repairs 8-11 Female 2-5Expeditionary Airfield 5-6 Pallet 6-1

Index-1

Alphabetical Index HAVAIR 51-60A-1


Starter 2-4,7-1 Disassembly. 6-1

Typical 2-4,8-13 Edge Clamp and Stakes 6-1

Heavy Duty Mat 6-1

L Replacement Mat 6-2

Shipping 6-1

Locking Bar 2-1,2-9 Spacer Mat 6-1Tiedown Containers 6-1

M Parking and Storage Areas 1-1,7-16Prongs, Mat. 2-8,7-3,7-19

MaintenanceDepot 12-1 R

Intermediate 11-1Organizational 8-1 Flemoval Procedure 9-1

Mat Repackaging 10-1

Alignmentof 7-6 Repair 11-1

Coverage. 2-4 Replacement 3-15

Damaged 8-1 Mat Pallet 3-15,3-16,5-8,6-2

Deflection and Roughness 8-8 Mats 2-7

Edge Repair 8-11 Procedures 8-13

End Ramp 2-6,7-8 Runway Section 8-6

End Ramp Pallet 3-14,5-7 Rework, Matting 11-1

Full Length 3-1,6-1Heavy Duty 2-8 sLaying Procedure 7-1Pallet. 6-1 SATS Airfield Matting Deployment 5-4

Patterns 2-1,2-4,2-5 ^^ Matting 12-2

Removal 9-1 Shipping Pallets 6-1Site Preparation 1-1

Spacer 2-9,8-13 Grading 1-1

Miscellaneous Tools 4-1 Hard Surface Runway 1-1Survey 1-1

Skin Ruptures 8-2.Soil Condition l-l

Non-skid Surface. Mats 2-1 Spacer Mats. 2-9.8-13,10-3

Numerical Index 15-1 Special Containers n-iSpecial Tools 4-1

0 Stake Assemblies 7-17Starter Keylock 2-4,7-1

On-field Deployment 5-1 Storage Areas 7-16

Organizational Maintenance 8-1 Strap and Seal Pallets ll-lSurface Dent Repair 8-1

p Survey 1-1

Packaging 3-1 T

Half Mat Pallets 3-3 Taxiways 1-1 7-15Mat Pallets 3-1 Tiedown Container 3-9,5-7,6-1^10-2

Pallet 6-1 Tiedowns .’. 2-7Adjustable Keylock 6-2 Installation 7.16Blast Deflector. 6-1 Tie Rod Pallets n.iConnector 6-1 Tools and Equipment 4-1Deployment 5-1,5-7 Typical Keylock 2-4,8-13

Index-2

NAYAIR 51-60A-1 Alphabetical IBOM


U V

Unpacking Matting Components 11-1 VSTOL Airfield Matting Deployment 5-4VTOL Airfield Matting Deployment 5-1

lrKlex.3

NAVAIR 51-60A-1

LIST OF MATTING SERVICE CHANGES AND SERVICE BULLETINS

1. SERVICE CHANGES

a. Cancelled

1

2. SERVICE BULLETINS

a. Incorporated in this handbook

3 7 8 9 *Int 10

b. Cancelled

1 2

c. Voided

5 6

d. Not applicable to this handbook

4

^

Indicates incorporation by current issue

REGION NO. 4 FLYLEAF

u.s, HUEMen mmw OFFICE! in? m-7/taoM

navair - the expeditionary engineer · pdf filenavair 51.60a-1 tableofconfnf section page vii...

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