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LAN AIRLINES S.A.TRANSPORTE AEREO S.A.

Boeing 767-300

Append ix A(Configuration Deviation List CDL)

Revision 02March 25, 2011

This document is applicable to the following aircraft

CC-BJA, CC-CDP, CC-CDM, CC-CEB, CC-CML, CC-CRG, CC-CRH,CC-CRV, CC-CWF, CC-CWG, CC-CWV, CC-CWY, CC-CXC,

CC-CXE, CC-CXG, CC-CXI, CC-CXJ, CC-CXK, CC-CXL,CC-CXH, CC-CZT, CC-CZU and CC-CZW

Based on Airplane Flight Manual Appendix CDL.Date: Feb 18, 2011

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RECORD OF REVISIONSLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

REVISION N° O2 PAGE 1

APPENDIX A (CDL) B767-300 DATE 25-MAR-2011

APPENDIX A (CDL)

RECORD OF REVISIONS

REV. NUMBER EDITED DATE UP-DATED BY

Original Apr 20, 2010 M. Delavenne

01 Oct 12, 2010 G. Vera / E. Lopez

02 Mar 25, 2011 E. Lopez

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LEFT INTENTIONALLY BLANK

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CONTENTLAN AIRLINES S.A.TRANSPORTE AEREO S.A.

REVISION N° 01 PAGE 1

CONTENTS

ITEM PAGE REVISION REV DATE

Cover - - - * 02 Mar 25, 2011

Record of Revisions 1 * 02 Mar 25, 2011

Content 1 * 02 Mar 25, 2011

Log of Revisions 1 * 02 Mar 25, 2011

Highlight of Change 1 thru 2 * 02 Mar 25, 2011

CDL General Notes 1 thru 2 * 02 Mar 25, 2011

CDL Item General Index 1 thru 3 * 02 Mar 25, 2011

ATA 21 Air Conditioning 21-1 thru 21-5 Original Apr 20, 2010

ATA 23Communications 23-1 thru 23-2 * 02 Mar 25, 2011

ATA 27Flight Controls 27-1 thru 27-6 * 02 Mar 25, 2011

ATA 28Fuel 28-1 thru 28-3 Original Apr 20, 2010

ATA 32Landing Gear 32-1 thru 32-5 Original Apr 20, 2010

ATA 33Lights 33-1 thru 33-11 * 02 Mar 25, 2011

ATA 52Doors 52-1 thru 52-8 * 02 Mar 25, 2011

ATA 53Fuselage 53-1 thru 53-5 * 02 Mar 25, 2011

ATA 54Nacelles/Pylons 54-1 thru 54-7 Original Apr 20, 2010

ATA 55Stabilizer 55-1 thru 55-10 Original Apr 20, 2010

ATA 56Windows 56-2 Original Apr 20, 2010

ATA 57Wings 57-1 thru 57-21 * 02 Mar 25, 2011

ATA 71Power Plant 71-1 thru 71-3 * 02 Mar 25, 2011

ATA 78Exhaust 78-1 thru 78-5 * 02 Mar 25, 2011

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LOG OF REVISIONSLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

REV N° DATE PAGE NUMBERS REMARKS AFM Appendix

CDL Revision

Original Apr 20, 2010 All Pages Now the APPENDIX A

correspond to CDL instead ofDDG.

01 Oct 12, 2010 Title, LR, Highlights, LEP Incorporate aircraft CC-CML ,and delete aircraft CC-CXD

02 Mar 25, 2011 Cover, Record of Revisions,Content, Log of Revisions,Highlight of Change page 1to page 2, CDL GeneralNotes page 1 to page 2,CDL Item General Index

23-1 to 23-2, 27-1 to 27-6,

33-1 to 33-11, 52-1 to 52-8,53-1 to 53-5, 57-1 to 57-21,71-1 to 71-3, 78-1 to 78-5

Added aircraft CWG

Delete aircraft CWH

Added DDG Rev. 32

Added DDG Rev. 33

- - - - - -

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HIGHLIGHTS OF CHANGELAN AIRLINES S.A.TRANSPORTED AEREO S.A.

HIGHLIGHTS OF CHANGE (DDG Rev. 32 and 33

Original Revision is issue to change the content of APPENDIX A. Now the content correspond to Configuration

Deviation List (CDL), Originally the content of APPENDIX A was Dispatch Deviation Guide (DDG).

HIGHLIGHTS OF CHANGE according DDG revision 32Chapter 00 - Introduction3.00-01-00.1 - Deleted CDL Revision number.3.00-01-00.1 - Revised in accor dance with AFM CDL General Limitations.3.00-01-00.2 - Revised paragraph in Weight Reductions.3.00-01-00.2 - Revised factor in Enroute Diversion Speed Effects.3.00-01-00.2 - Revised diversion speed and factor in Enroute Diversion Speed3.00-01-00.2 - Revised paragraph in Enroute Fuel Mileage Effects.

Chapter 21 - Air Conditioning Ram Air Inlet Doors3.21-53-01.1 - Consolidated table and revised annotation.

Ram Air Exhaust Doors3.21-53-02.1 - Consolidated table and revised annotation.3.21-53-02.1 - Revised adjustment in accordance with AFM CDL.Ram Air Inlet and Exhaust Door s3.21-53-03.1 - Consolidated table and revised annotation.

Chapter 23 - Communications Static Dischargers (Trailing and Tip Type)3.23-61-01.2 - Revised label for Vertical Fin Tip/Rudder Dischargers.

Chapter 27 - Flight ControlsInboard Trailing Edge Flap-To-Fuselage Seals3.27-51-01.1 - Consolidated table and revised annotation.Inboard Flap Torque Tube Slot Doors (Three Segment Door)3.27-51-02.1 - Revised Number Installed in accordance with AFM CDL.

Krueger Seal End Seals3.27-82-01.1 - Deleted redundant text.

Chapter 32 - Landing GearMain Landing Gear Wing Doors (2 Shock Strut Doors, 2 Trunnion Doors,2 Drag Strut Doors)3.32-12-01.1 - Consolidated table and revised annotation.

Chapter 33 - LightsMain and Bulk Cargo Door Light Covers3.33-31-01.1 - Consolidated table and revised annotation.Wing Tip Aft Navigation Light Lens3.33-44-01.1 - Added Note in accordance with AFM CDL.

Chapter 52 - Doors

Potable Water Service Doors - Standard Configuration3.52-49-02.1 - Consolidated table and revised annotation.Potable Water Service Doors - Alternate Configuration3.52-49-03.1 - Consolidated table and revised annotation.Outboard Wing Leading Edge Pressure Fueling Door3.52-49-04.1 - Consolidated table and revised annotation.

Aft Toilet Service Door3.52-49-06.1 - Deleted obsolete Note.

Chapter 53 - FuselageWing Root Jacking Point Access Panels3.53-30-01.1 - Revised annotation to delete "All Engines".

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Chapter 55 - StabilizerHorizontal Stabilizer-To-Elevator Seals3.55-16-01.1 - Consolidated table and revised annotation.

Chapter 57 - WingsVortex Generators3.57-00-01.1 - Consolidated table and revised annotation.Wing Leading Edge Slat Linkage Fairing Panels3.57-41-01.1 - Revised AMM reference to correct typographical error.Wing Thermal Anti-Icing Duct Seal - Door Assembly3.57-41-02.1 - Item format standardized.Fixed Leading Edge Seals3.57-41-03.1 - Consolidated table and revised annotation.Main Landing Gear Trunnion Support Fairings3.57-51-01.1 - Standardized text.3.57-51-01.1 - Consolidated table and revised annotation.Trailing Edge Flap Hinge Fairings

3.57-51-02.1 - Consolidated table and revised annotation.Main Landing Gear Forward Trunnion Fairings (On Wing Fixed Trailing Edge)3.57-51-05.1 - Standardized text.Main Landing Gear Aft Trunnion Fairings (On Wing Fixed Trailing Edge)3.57-51-06.1 - Standardized text.Chapter 71 - Power PlantFan Cowl Pressure Relief Access Doors3.71-11-01.1 - Added annotation.3.71-11-01.1 - Consolidated table and revised annotation.Fan Cowl Oil Tank Access Doors3.71-11-02.1 - Revised proviso reference to title of 71-11-01.Chapter 78 - ExhaustThrust Reverser Track Fairings

3.78-31-02.1 - Consolidated table and revised annotation.Thrust Reverser Cascade Vane Segments3.78-31-04.1 - Added annotation.

Highlights o f change according DDG Rev 33.Chapter 00 - Introduction3.00-01-00.1 - Revised sentence to include "the airplane has".Chapter 57 - WingsWing Leading Edge Slat Linkage Fairing Panels3.57-41-01.1 - Added Item 57-41-02.Fixed Leading Edge Seals3.57-41-03.1 - Added Item 57-41-02

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GENERAL NOTESLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

IS3netcrotidounc3tiCoCDn LDL - Introduction - 00-01-00INTRODUCTIONII

IINTRODUCTION

General Notes

This section contains locations, illustrations and performance information for all of the APPENDIX A(CDL) items from the 767 Airplane Flight Manual (AFM) Appendix Configuration Deviation List (CDL).

Limitations

The associated limitations must be listed on a placard affixed in the cockpit in clear view of the pilot-in-command and other appropriate crew members.

Operation with those missing parts requiring a reduction of VMO/MMO is permitted only when theairplane has the airspeed limit speed hand (or the airspeed tape on the PFD) and the Mach airspeedwarning system programmed for the altitude/speed schedule specified for the applicable missingpart.

The pilot in command will be notified of each operation with a missing or damaged part(s) by listingthe missing or damaged part(s) in the flight or dispatch release.

The operator will list in the aircraft logbook an appropriate notation covering the missing or damagedpart(s) on each flight.

If an additional part is lost in flight the airplane may not depart the Airport at which it landed followingthis event until it again complies with the limitation of this appendix. This, of course, does notpreclude the issuance of a ferry permit to allow the airplane to be flown to a point where thenecessary repairs or replacements can be made.

No more than one part for any one sub-system in this appendix may be missing unless specificallydesignated combinations are indicated herein. Unless otherwise specified herein, parts from differentsub-systems may be missing. The performance penalties are cumulative unless specificallydesignated penalties for combination of missing parts are indicated.

Where performance penalties are listed as negligible, no more than three negligible items may bemissing or damaged without taking further penalty. For each missing or damaged item more thanthree reduce the takeoff, landing, and enroute climb limits 100 pounds.

Weight Reductions

The performance penalties are cumulative unless specifically designated penalties for combination ofmissing parts are indicated. Where performance penalties are listed as negligible, no more than three

negligible items may be missing without taking further penalty. For each missing or damaged itemmore than three reduce the takeoff, landing and enroute climb limits by 100 pounds (46 kilograms).Where performance penalties are listed as no penalty, any cumulative number of items listed as nopenalty may be missing without further penalty.

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GENERAL NOTESLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

Enroute Diversion Speed Effects

The enroute climb weight penalties listed are based on operating speeds that approximate the

maximum lift-to-drag ratio speed. To account for the difference in level off altitude when operating atother speeds, multiply the enroute climb weight penalty listed by the following appropriate factor:

Diversion Speed Factor

LRC 1.6

290 KIAS 2.3

310 KIAS 3.0

330 KIAS 3.8

350 KIAS 4.5

Enroute Fuel Mileage Effects

The drag effects of many 767 CDL items are so small that enroute fuel mileage changes arenegligible. For items with significant drag effects, a fuel mileage decrement of 0.45% per 1000 lb. ofenroute climb penalti should be applied, unless a specific fuel milage decrement is identified in theitem.

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GENERAL INDEXLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

GENERAL INDEX OF CDL ITEMS

Configuration Deviation List (CDL) items corresponding to the Model 767

Airplane Flight Manual Appendix CDL.

ITEM DESCRIPTION PAGE

ATA 21 - AIR CONDITIONING

21-32-1 Cabin Pressure Safety Relief Valve Flapper Doors 21-221-53-1 Ram Air Inlet Doors 21-321-53-2 Ram Air Exhaust Doors 21-421-53-3 Ram Air Inlet and Exhaust Doors 21-5

ATA 23 – COMMUNICATIONS

23-61-1 Static Discharger (Trailing and Tip Type) 23-2

ATA 27 - FLIGHT CONTROLS

27-51-1 Inboard Trailing Edge Flap-To-Fuselage Seals 27-227-51-2 Inboard Flap Torque Tube Slot Doors (Three Segment Door) 27-327-81-1 Slat End Pan Seal 27-427-81-2 Krueger Seal Bullnose Assembly 27-527-82-1 Krueger Seal End Seals 27-6

ATA 28 – FUEL

28-22-1 Override Boost Pump Access Panels 28-228-44-1 Fuel Quantity Measuring Sticks 28-3

ATA 32 - LANDING GEAR

32-10-1 Bogie Beam Shield 32-232-12-1 Main Landing Gear Wing Doors 32-332-71-1 Tail Skid Fairing 32-432-71-2 Tail Skid Lever Door 32-5

ATA 33 - LIGHTS

33-31-1 Main and Bulk Cargo Door Light Covers 33-233-41-1 Wing Illumination Light Covers 33-333-42-2 Nose Gear Taxi Light 33-433-44-1 Wing Tip Aft Navigation Light Lens (Without Winglets) 33-533-44-1 Wing Tip Aft Navigation Light Lens (With Winglets) 33-633-44-2 Wing Tip Strobe Lights Lens (Without Winglets) 33-7

33-44-2 Wing Tip Strobe Lights Lens (With Winglets) 33-833-44-3 Upper and Lower Body Anti-Collision Light Lens 33-933-45-1 Logo Illumination Light Covers 33-1033-51-1 External Emergency Escape Light Covers 33-11

ATA 52 – DOORS

52-36-1 Bulk Cargo Door Handle 52-252-49-1 Electrical/Electronics External Power Door 52-352-49-2 Potable Water Service Doors - Standard Configuration 52-452-49-3 Potable Water Service Doors - Alternate Configuration 52-5

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INDEX OF CDL ITEMS

52-49-4 Outboard Wing Leading Edge Pressure Fueling Door 52-652-49-5 Main Cargo Loading Control Doors 52-752-49-6 Aft Toilet Service Door 52-8

ATA 53 – FUSELAGE

53-16-1 Nose Landing Gear Hinge Cover Doors 53-253-30-1 Wing Root Jacking Point Access Panels 53-353-65-1 Main Cargo Doors Control Switch Panels 53-453-85-1 APU Louvered Pressure Relief Door 53-5

ATA 54 - NACELLES/PYLONS

54-51-1 Deleted 54-2

54-52-1 Aft Fairing Primary Nozzle-To-Strut Seals 54-354-53-1 Nacelle Strut Pressure Relief Doors 54-454-53-2 Nacelle Strut Access Doors 54-6

ATA 55 - STABILIZER

55-10-1 Horizontal Stabilizer-Auxiliary Box 55-255-10-2 Horizontal Stabilizer-Fixed Trailing Edge 55-355-16-1 Horizontal Stabilizer-To-Elevator Seals 55-455-20-1 Inboard Elevators 55-555-20-2 Outboard Elevators 55-655-30-1 Vertical Stabilizer - Auxiliary Box 55-755-30-2 Vertical Stabilizer - Fixed Trailing Edge 55-8

55-31-1 Vertical Stabilizer-To-Fuselage Seals 55-955-40-1 Rudder 55-10

ATA 56 - WINDOWS

56-11-1 Windshield Aerodynamic Sealant (#1 and #3 Windows) 56-2

ATA 57 - WINGS

57-00-1 Vortex Generators 57-257-20-1 Inspar Upper Wing Panel 57-357-41-1 Wing Leading Edge Slat Linkage Fairing Panels 57-457-41-2 Deleted 57-557-41-3 Fixed Leading Edge Seals 57-6

57-41-4 Leading Edge Slat Mechanism Lubrication Access Doors 57-757-41-5 Inboard Wing Fixed Leading Edge 57-957-41-6 Outboard Wing Fixed Leading Edge 57-1057-43-1 Wing Leading Edge Slat Wedge 57-1157-51-1 Main Landing Gear Trunnion Support Fairings 57-1257-51-2 Trailing Edge Flap Hinge Fairings 57-1357-51-3 Inboard Trailing Edge Fixed Panel 57-1457-51-4 Outboard Trailing Edge Fixed Panel 57-1557-51-7 Main Landing Gear Side Brace Trunnion Aft Fairings 57-1657-53-1 Inboard Trailing Edge Flaps 57-17

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INDEX OF CDL ITEMS

57-53-2 Outboard Trailing Edge Flaps 57-1857-60-1 Inboard Ailerons 57-1957-60-2 Outboard Ailerons 57-2057-70-1 Spoiler Panels 57-21

ATA 71 - POWER PLANT

71-11-1 Fan Cowl Pressure Relief Access Doors 71-271-11-2 Fan Cowl Oil Tank Access Doors 71-3

ATA 78 - EXHAUST

78-31-1 Thrust Reverser Sleeve Actuator Access Panels 78-278-31-2 Thrust Reverser Track Fairings 78-3

78-31-3 Fan Thrust Reverser Blocker Doors 78-478-31-4 Thrust Reverser Cascade Vane Segments 78-5

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21. AIR CONDITIONINGLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

REVISION N° Original PAGE 21-1

APPENDIX A (CDL) B767-300 DATE 20-APR-2010

21-32-01 Cabin Pressure Safety Relief Valve Flapper Doors 21-2

21-53-01 Ram Air Inlet Doors 21-3

21-53-02 Ram Air Exhaust Doors 21-4

21-53-03 Ram Air Inlet and Exhaust Doors 21-5

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21-32-01 Cabin Pressure Safety Relief Valve Flapper Doors

Any number may be missing.

Performance limited weights are reduced by the following:

Number Installed Takeoff & Landing Enroute Climb

4 Negligible penalty Negligible penalty

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21-53-01 Ram Air Inlet Doors

One may be missing.

NOTE: When missing in combination with Ram Air Exhaust Doors, use penalties in APPENDIX A(CDL) Item 21-53-03.

NOTE: Ram Air Exhaust Door on the same side must be locked open. Refer to MEL Item 21-53-01.

For -300/-80C2:

2 700 lb (318 kg) 700 lb (318 kg)

For -300/PW:

Number Installed Takeoff & Landing Enroute Climb2 500 lb (227 kg) 900 lb (409 kg)

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21-53-02 Ram Air Exhaust Doors

One or both may be missing.

NOTE: When missing in combination with Ram Air Inlet Doors, use penalties in APPENDIX A(CDL) Item 21-53-03.

For -300/-80C2:

2 900 lb (409 kg) 800 lb (363 kg)

For -300/PW:

2 600 lb (272 kg) 1000 lb (454 kg)

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21-53-03 Ram Air Inlet and Exhaust Doors

One ram air inlet door and two ram air exhaust doors may be missing in any combination.

NOTE 1: Use these penalties when Ram Air Inlet and Exhaust Doors are missing in anycombination.

NOTE 2: For missing Ram Air Inlet Door, Ram Air Exhaust Door on the same side (if not missing)must be locked open. Refer to MEL Item 21-53-01.

For -300/-80C2:

4 1300 lb (590 kg) 1400 lb (635 kg)

For -300/PW:Number Installed Takeoff & Landing Enroute Climb

4 900 lb (409 kg) 1800 lb (817 kg)

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23. COMMUNICATIONSLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

REVISION N° 02 PAGE 23-1

23-61-01 Static Discharger (Trailing and Tip Type) 23-2

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23. COMMUNICATIONSLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

23-61-01 Static Discharger (Trail ing and Tip Type)

A minimum of fifteen static dischargers is required when operations are dependent upon the use of

ADF, HF, VOR, or Marker Beacon capability. Trailing edge or tip type dischargers must be installedin three of the five most outboard positions on each wing, horizontal stabilizer/elevator assembly, andvertical stabilizer/rudder assembly.

Static dischargers are not required when operations are not dependent upon use of ADF, HF, VOR,or Marker Beacon capability.

39 No penalty No penalty

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27. FLIGHT CONTROLSLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

27-51-01 Inboard Trailing Edge Flap-To-Fuselage Seals 27-2

27-51-02 Inboard Flap Torque Tube Slot Doors (Three Segment Door) 27-3

27-81-01 Slat End Pan Seal 27-4

27-81-02 Krueger Seal Bullnose Assembly 27-5

27-82-01 Krueger Seal End Seals 27-6

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27-51-01 Inboard Trailing Edge Flap-To-Fuselage Seals

For -300/-80C2:

2 3400 lb (1543 kg) 500 lb (227 kg)

For -300/PW:

2 2300 lb (1043 kg) 600 lb (272 kg)

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27-51-02 Inboard Flap Torque Tube Slot Doors (Three Segment Door)

Any number or combination may be missing.

Increase the landing approach speed VREF by 2 knots.

NOTE: When missing in combination with Trailing Edge Flap Vortex Generators (APPENDIX A(CDL) Item 57-00-01) use penalties for Trailing Edge Flap Vortex Generators only.

For -300/GE & PW:

Number Installed Landing Climb Landing Field Length Quick Turnaround

6 4700 lb (2132 kg) 7600 lb (3448 kg) 4100 lb (1860 kg)

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27-81-01 Slat End Pan Seal

For -300

2 200 lb (91 kg) 350 lb (159 kg)

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27-81-02 Krueger Seal Bul lnose Assembly

For -300/-80C2

2 2200 lb (998 kg) No penalty

For-300/PW:

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27-82-01 Krueger Seal End Seals

Two flat seals or bulb seals may be missing.

For -300

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28. FUELLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

28-22-01 Override Boost Pump Access Panels 28-2

28-44-01 Fuel Quantity Measuring Sticks 28-3

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28-22-01 Override Boost Pump Access Panels

One may be missing.

NOTE 1: Wires in the cavity must be protected. Inspect wires before reinstalling door. Pull and collarpump circuit breaker. (Open and collar circuit breaker for associated fuel pump). ReferenceMEL Item 28-22-02 for dispatch requirements.

NOTE 2: Placing speed tape over the cavity is a method for protecting the wires.

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28-44-01 Fuel Quantity Measur ing Sticks

NOTE: Missing fuel quantity measuring sticks may impact, in some manner, the following MELitems: 28-41-01, 28-41-02, 28-41-06 and 28-44-01. Refer to the MEL for dispatchrequirements.

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32. LANDING GEARLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

32-10-01 Bogie Beam Shield 32-2

32-12-01 Main Landing Gear Wing Doors (2 Shock Strut Doors, 2 Trunnion Doors,2 Drag Strut Doors)

32-71-01 Tail Skid Fairing 32-4

32-71-02 Tail Skid Lever Door 32-5

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32-10-01 Bogie Beam Shield

The Bogie Beam Shield should be replaced as soon as possible and the electrical conduits beneaththe main landing gear truck should be inspected prior to reinstallation.

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32-12-01 Main Landing Gear Wing Doors (2 Shock Strut Doors, 2 Trunnion Doors, 2

Drag Strut Doors) Any one of six doors may be missing.

Limit speed to 270 KIAS/0.73 Mach.

NOTE 1: Set the ALTERNATE Vmo/Mmo switch (if installed) to ALTN.

NOTE 2: For ALTERNATE Vmo/Mmo switch not installed, refer to the General Limitations on Appendix A (CDL) General Notes page 1 for operational limitations.

For -300/-80C2:

6 409 kg (900 lb) 454 kg (1000 lb)

For -300/PW:

6 272 kg (600 lb) 544 kg (1200 lb)

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32-71-01 Tail Skid Fairing

May be missing.

NOTE: May be missing in combination with APPENDIX A (CDL) Item 32-71-02.

For -300:

1 91 kg (200 lb) 136 kg (300 lb)

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32-71-02 Tail Skid Lever Door

May be missing.

NOTE: May be missing in combination with APPENDIX A (CDL) Item 32-71-01.

For -300:

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33. LIGHTSLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

33-31-01 Main and Bulk Cargo Door Light Covers 33-2

33-41-01 Wing Illumination Light Covers 33-3

33-42-02 Nose Gear Taxi Light 33-4

33-44-01 Wing Tip Aft Navigation Light Lens (Aircraft without Winglets) 33-5

33-44-01 Wing Tip Aft Navigation Light Lens (Aircraft with Winglets) 33-6

33-44-02 Wing Tip Strobe Lights Lens (Aircraft without Winglets) 33-7

33-44-02 Wing Tip Strobe Lights Lens (Aircraft with Winglets) 33-8

33-44-03 Upper and Lower Body Anti-Collision Light Lens 33-9

33-45-01 Logo Illumination Light Covers 33-10

33-51-01 External Emergency Escape Light Covers (Overwing and Ground Illumination) 33-11

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33-31-01 Main and Bulk Cargo Door Light Covers

NOTE: Refer to MEL Item 33-31-2, Exterior Cargo Loading Area Lights, for dispatch requirements.

For GE and PW:

4 No penalty 45 kg (100 lb)

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33-41-01 Wing Illumination Light Covers

NOTE: Refer to MEL Item 33-41-01, Wing Illumination Lights, for dispatch requirements.

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33-42-02 Nose Gear Taxi Light

Not applicable. Nose Gear Taxi lights are not installed.

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33-44-01 Wing Tip Aft Navigation Light Lens (Aircraft without Winglets)

NOTE 1: The minimum number of strobe/anticollision lights required by the operating rules must beoperative.

NOTE 2: Any combination of APPENDIX A (CDL) Items 33-44-01, 33-44-02 and 33-44-03 may bemissing.

NOTE 3: Refer to MEL Item 33-43-01, Position Lights, for dispatch requirements.

(See next page for item 33-44-01 for aircraft with Winglets)

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33-44-01 Wing Tip Aft Navigation Light Lens (Aircraft with Winglets)

None may be missing.

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33-44-02 Wing Tip Strobe Lights Lens (Aircraft without Winglets)

NOTE 3: Refer to MEL Item 33-44-01 for dispatch requirements.

For -300:

(See next page for item 33-44-2 for aircraft with Winglets)

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33-44-02 Wing Tip Strobe Lights Lens (Aircraft with Winglets)

None may be missing.

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33-44-03 Upper and Lower Body Anti-Collision Light Lens

One or both may be missing. When the lens is missing, disconnect electrical power and remove the

light bulb, reflector, lens cover, and lens cover support. With the rest of the light assembly intact,cover the opening with appropriate materials (speed tape, for example) to prevent moisture or debrisfrom entering the light assembly.

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33-45-01 Logo Illumination Light Covers

NOTE 1: Openings created by missing light covers must be covered with "speed tape" (Permacel IIor 3M425). Pull and collar logo light CB. Inspect condition of "speed tape" every otherflight.

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33-51-01 External Emergency Escape Light Covers (Overwing and GroundIllumination)

NOTE: Refer to MEL Item 33-51-02, Exterior Emergency Lighting System, for dispatch requirements.

8 or 14 Negligible penalty Negligible penalty

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52. DOORSLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

52-36-01 Bulk Cargo Door Handle 52-2

52-49-01 Electrical/Electronics External Power Door 52-3

52-49-02 Potable Water Service Doors - Standard Configuration 52-4

52-49-03 Potable Water Service Doors - Alternate Configuration 52-5

52-49-04 Outboard Wing Leading Edge Pressure Fueling Door 52-6

52-49-05 Main Cargo Loading Control Doors 52-7

52-49-06 Aft Toilet Service Door 52-8

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52-36-01 Bulk Cargo Door Handle

May be missing.

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52-49-01 Electrical/Electronics External Power Door

May be missing.

NOTE: Any combination of the authorized numbers of APPENDIX A (CDL) Items 52-49-01, 52-49-02, 52-49-03, 52-49-04 and 52-49-05 may be missing.

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52-49-02 Potable Water Service Doors - Standard Configuration

NOTE: Any combination of the authorized numbers of APPENDIX A (CDL) Items 52-49-01, 52-49-02,52-49-03, 52-49-04 and 52-49-05 may be missing.

For -300/GE or -300/PW:

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52-49-03 Potable Water Service Doors - Alternate Configuration

NOTE: Any combination of the authorized numbers of APPENDIX A (CDL) Items 52-49-01, 52-49-02,52-49-03, 52-49-04 and 52-49-05 may be missing.

For -300/GE or -300/PW:

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52-49-04 Outboard Wing Leading Edge Pressure Fueling Door

(One installed/Standard configuration) May be missing with the penalty in the table.

(Two installed/Optional configuration) Both may be missing with the penalty in the table. If only one ismissing use the performance decrement for Standard configuration.

NOTE 1: For both the one and two doors installed, the Power Control Limit (or Battery Power)Switch must be locked in the "NORM" position, the Fueling Valve Switches in the "OFF"position, and the Defueling Valve Switches in the "CLOSE" position. Required placardinformation must be reproduced within the fueling bay.

NOTE 2: Any combination of the authorized numbers of APPENDIX A (CDL) Items 52-49-01, 52-49-02, 52-49-03, 52-49-04 and 52-49-05 may be missing.

For Standard configuration and 300/GE:

1 Negligible penalty 45 kg (100 lb)

For Standard configuration and 300/PW4000:

For Optional configuration and 300/GE & PW:

2 91 kg (200 lb) 136 kg (300 lb)

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52-49-05 Main Cargo Loading Control Doors

NOTE: Any combination of the authorized numbers of APPENDIX A (CDL) Items 52-49-01,

52-49-02, 52-49-03, 52-49-04 and 52-49-05 may be missing.

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52-49-06 Aft Toilet Service DoorMay be missing.

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53. FUSELAGELAN AIRLINES S.A.TRANSPORTED AEREO S.A.

53-16-01 Nose Landing Gear Hinge Cover Doors 53-2

53-30-01 Wing Root Jacking Point Access Panels 53-3

53-65-01 Main Cargo Doors Control Switch Panels 53-4

53-85-01 APU Louvered Pressure Relief Door 53-5

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53-16-01 Nose Landing Gear Hinge Cover Doors

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53-30-01 Wing Root Jacking Point Access Panels

For -300:

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53-65-01 Main Cargo Doors Contro l Switch Panels

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53-85-01 APU Louvered Pressure Relief Door

May be missing.

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54. NACELLES/PYLONSLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

54-51-01 Nacelle Strut-To-Wing Seals - DELETED 54-2

54-52-01 Aft Fairing Primary Nozzle-To-Strut Seals 54-3

54-53-01 Nacelle Strut Pressure Relief Doors 54-4

54-53-02 Nacelle Strut Access Doors 54-6

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54-51-01 DELETED (Nacelle Strut-To-Wing Seals)

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54-52-01 Aft Fairing Primary Nozzle-To-Strut Seals

For -300/GE:

4 (2 per strut) 272 kg (600 lb) 635 kg (1400 lb)

For -300/PW:

4 (2 per strut) Negligible penalty 136 kg (300 lb)

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54-53-01 Nacelle Strut Pressure Relief Doors

A maximum of two may be missing (one per strut).

NOTE 1: May be missing in combination with APPENDIX A (CDL) Item 54-53-02. When Items

54-53-01 and 54-53-02 are missing in combination, use only one penalty.

NOTE 2: For all engine types, any combination of the authorized numbers of APPENDIX A (CDL)

items 54-53-01 and 54-53-02 may be missing.

For -300/GE and PW:

4 (2 per strut) Negligible penalty Negligible penalty

(Continued on next page)

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54-53-02 Nacelle Strut Access Doors

NOTE 1: May be missing in combination with APPENDIX A (CDL) Item 54-53-01. When Items 54-53-01 and 54-53-02 are missing in combination, use only one penalty.

NOTE 2: For all engine types, any combination of the authorized numbers of APPENDIX A (CDL)items 54-53-01 and 54-53-02 may be missing.

For -300/-80C2:

For -300/-PW4000:

(Continued on next page for GE engines)

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55. STABILIZERLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

55-10-01 Horizontal Stabilizer -Auxiliary Box 55-2

55-10-02 Horizontal Stabilizer - Fixed Trailing Edge 55-3

55-16-01 Horizontal Stabilizer-To-Elevator Seals 55-4

55-20-01 Inboard Elevators 55-5

55-20-02 Outboard Elevators 55-6

55-30-01 Vertical Stabilizer - Auxiliary Box 55-7

55-30-02 Vertical Stabilizer - Fixed Trailing Edge 55-8

55-31-01 Vertical Stabilizer-To-Fuselage Seals 55-9

55-40-01 Rudder 55-10

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55-10-01 Horizontal Stabilizer -Auxi liary Box

None may be missing. May have damage due to on-ground hail.If a performance restriction is required due to on-ground hail damage, as assessed in the StructuralRepair Manual 51-10-04, for each damaged panel the performance limited weights are reduced bythe following:

For -300/-80C2:

2 304 kg (670 lb) 341 kg (750 lb)

For -300/-PW4000:

2 196 kg (430 lb) 409 kg (900 lb)

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55-10-02 Horizontal Stabilizer - Fixed Trailing Edge

None may be missing. May have damage due to on-ground hail.

If a performance restriction is required due to on-ground hail damage, as assessed in the StructuralRepair Manual 51-10-04, for each damaged trailing edge the performance limited weights arereduced by the following:

For -300/-80C2:

2 341 kg (750 lb) 386 kg (850 lb)

For -300/-PW4000:

2 218 kg (480 lb) 459 kg (1010 lb)

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55-16-01 Horizontal Stabilizer-To-Elevator Seals

A maximum of 320 inches (80 inches per surface) may be missing.

For -300/-80C2:

34 409 kg (900 lb) 363 kg (800 lb)

For -300/-PW4000:

34 272 kg (600 lb) 454 kg (1000 lb)

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55-20-01 Inboard Elevators

NOTE: If either of the inboard elevators are damaged, the forward Center of Gravity (C.G) Limitmust be shifted aft by 3.0% MAC (except for dispatch with Alternate Forward C.G.).

If a performance restriction is required due to on-ground hail damage, as assessed in the StructuralRepair Manual 51-10-04, for each damaged elevator the performance limited weights are reduced bythe following:

For -300/-80C2:

2 295 kg (650 lb) 336 kg (740 lb)

For -300/-PW4000:

2 191 kg (420 lb) 400 kg (880 lb)

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55-20-02 Outboard Elevators

NOTE: If either of the outboard elevators are damaged, the forward Center of Gravity (C.G.) Limitmust be shifted aft by 3.0% MAC (except for dispatch with Alternate Forward C.G.).

If a performance restriction is required due to on-ground hail damage, as assessed in the StructuralRepair Manual 51-10-04, for each damaged elevator the performance limited weights are reduced bythe following:

For -300/-80C2:

2 440 kg (970 lb) 495 kg (1090 lb)

For -300/-PW4000:Number Installed Takeoff & Landing Enroute Climb

2 282 kg (620 lb) 595 kg (1310 lb)

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55-30-01 Vertical Stabilizer - Auxi liary Box

If a performance restriction is required due to on-ground hail damage, as assessed in the StructuralRepair Manual 51-10-04, for each damaged panel the performance limited weights are reduced by:

For -300/-80C2:

2 323 kg (710 lb) 363 kg (800 lb)

For -300/-PW4000:

2 209 kg (460 lb) 436 kg (960 lb)

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55-30-02 Vertical Stabilizer - Fixed Trailing Edge

If a performance restriction is required due to on-ground hail damage, as assessed in the StructuralRepair Manual 51-10-04, for each damaged trailing edge the performance limited weights arereduced by:

For -300/-80C2:

2 527 kg (1160 lb) 595 kg (1310 lb)

For -300/-PW4000:

2 336 kg (740 lb) 713 kg (1570 lb)

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55-31-01 Vertical Stabilizer-To-Fuselage Seals

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55-40-01 Rudder

May not be missing. May have damage due to on-ground hail.

If a performance restriction is required due to on-ground hail damage, as assessed in the StructuralRepair Manual 51-10-04, the performance limited weights are reduced by:

For -300/-80C2:

1 46 kg (100 lb) 55 kg (120 lb)

For -300/-PW4000:

1 Negligible 64 kg (140 lb)

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56. WINDOWSLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

56-11-01 Windshield Aerodynamic Sealant (#1 and #3 Windows) 56-2

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56. WINDOWSLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

56-11-01 Windshield Aerodynamic Sealant (#1 and #3 Windows)

May be missing.

1 per window Negligible penalty Negligible penalty

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57. WINGSLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

57-00-01 Vortex Generators 57-2

57-20-01 Inspar Upper Wing Panel 57-3

57-41-01 Wing Leading Edge Slat Linkage Fairing Panels 57-4

57-41-02 Wing Thermal Anti-Icing Duct Seal – Door assembly 57-5

57-41-03 Fixed Leading Edge Seals 57-6

57-41-04 Leading Edge Slat Mechanism Lubrication Access Doors 57-7

57-41-05 Inboard Wing Fixed Leading Edge 57-9

57-41-06 Outboard Wing Fixed Leading Edge 57-10

57-43-01 Wing Leading Edge Slat Wedge 57-11

57-51-01 Main Landing Gear Trunnion Support Fairings 57-12

57-51-02 Trailing Edge Flap Hinge Fairings 57-13

57-51-03 Inboard Trailing Edge Fixed Panel 57-14

57-51-04 Outboard Trailing Edge Fixed Panel 57-15

57-51-07 Main Landing Gear Side Brace Trunnion Aft Fairings 57-16

57-53-01 Inboard Trailing Edge Flaps 57-17

57-53-02 Outboard Trailing Edge Flaps 57-18

57-60-01 Inboard Aileron 57-19

57-60-02 Outboard Aileron 57-20

57-70-01 Spoiler Panels 57-21

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57-00-01 Vortex Generators

Wing Vortex Generators: A total of two may be missing, but not more than one per group. Operations

must be limited to a maximum altitude of 18,000 feet.Trailing Edge Flap Vortex Generators: A total of four (two from each flap) may be missing. Increaselanding approach speed VREF by 2 knots.

For -300/GE or -300/PW:

Number Installed Landing Climb Landing Field Length Quick Turnaround

14 Wing50 TE Flap

Negligible penalty2132 kg (4700 lb)

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57-20-01 Inspar Upper Wing Panel

If a performance restriction is required due to on-ground hail damage, as assessed in the StructuralRepair Manual 51-10-04, for each damaged panel the performance limited weights are reduced bythe folowing:

For -300/-80C2:

2 200 kg (440 lb) 227 kg (500 lb)

For -300/-PW4000:

2 127 kg (280 lb) 273 kg (600 lb)

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57-41-01 Wing Leading Edge Slat Linkage Fairing Panels

A maximum of six (three per side) in any combination may be missing provided none of the Leading

Edge Slat Mechanism Lubrication Access Doors (APPENDIX A (CDL) Item 57-41-04) are missing.NOTE 1: Avoid icing conditions if any inboard slat linkage fairings are missing from either inboard

NOTE 2: Any combination of CDL Items 57-41-01, 57-41-02 and 57-41-03 may be missing.

NOTE 3: For removal of outboard leading edge slat actuator seal door see AMM 57-41-56/401.

NOTE 4: For removal of inboard leading edge slat actuator seal door see AMM 57-41-59/401.Performance limited weights are reduced by the following:

For -300/All Engines:

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57-41-02 Wing Thermal Anti-Icing Duct Seal - Door Assembly

NOTE: Any combination of APPENDIX A (CDL) Items 57-41-01, 57-41-02 and 57-41-03 may bemissing.

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57-41-03 Fixed Leading Edge Seals

All inboard slat Sliding Seals (four per side) and one Curtain Seal per outboard slat (five per side),

may be missing.NOTE 1: Curtain Seal configuration must be symmetrical. Sliding Seal configuration may be

asymmetrical.

For -300/-80C2:

Number Installed Takeoff Enroute Climb Landing Climb

50 No penalty No penalty 1225 kg (2700 lb)

For -300/PW4000:

Number Installed Takeoff Enroute Climb Landing Climb

50 No penalty No penalty 1180 kg (2600 lb)

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57-41-04 Leading Edge Slat Mechanism Lubr ication Access Doors

A maximum of four per airplane in any combination may be missing provided none of the Wing

Leading Edge Slat Linkage Fairing Panels (APPENDIX A (CDL) Item 57-41-01) are missing.Performance limited weights are reduced by the following:

40 (20 per side) No penalty 431 kg (950 lb)

(continued)

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The Leading Edge Slat Lubrication Panels which fall into the list of 20 access panels from CDL item57-41-04 are:

511DB/611DB511EB/611EB511HB/611HB511MB/611MB521CB/621CB521DB/621DB521FB/621FB521GB/621GB521KB/621KB521LB/621LB521MB/621MB

521NB/621NB521UB/621UB521VB/621VB521WB/621WB521XB/621XB521AGB/621AGB521AHB/621AHB521AJB/621AJB521AKB/621AKB

(note: 500 series left wing, 600 series right wing)

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57-41-05 Inboard Wing Fixed Leading Edge

If a performance restriction is required due to on-ground hail damage, as assessed in the StructuralRepair Manual 51-10-04, for each damaged panel the performance limited weights are reduced bythe following:

For -300/-80C2:

2 504 kg (1110 lb) 567 kg (1250 lb)

For -300/-PW4000:

2 323 kg (710 lb) 681 kg (1500 lb)

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57-41-06 Outboard Wing Fixed Leading Edge

For -300/-80C2:

2 264 kg (580 lb) 295 kg (650 lb)

For -300/-PW4000:

2 168 kg (370 lb) 354 kg (780 lb)

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57-43-01 Wing Leading Edge Slat Wedge

If a performance restriction is required due to on-ground hail damage, as assessed in the StructuralRepair Manual 51-10-04, for each damaged slat wedge the performance limited weights are reducedby the following:

For -300/-80C2:

12 132 kg (290 lb) 150 kg (330 lb)

For -300/-PW4000:

12 87 kg (190 lb) 177 kg (390 lb)

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57-51-01 Main Landing Gear Trunnion Suppor t FairingsOne may be missing.

Limit speed to 270 KIAS/0.73 MachNOTE 1: Place the ALTERNATE Vmo/Mmo switch (if installed) to ALTN.

NOTE 2: For ALTERNATE Vmo/Mmo switch not installed, refer to the APPENDIX A (CDL) GeneralNotes, Limitations on 1 for operational limitations.

NOTE 3: Any combination of the authorized numbers of APPENDIX A (CDL) Items 57-51-01 and 57-51-02 may be missing.

For -300/-80C2:

2 227 kg (500 lb) 227 kg (500 lb)

For -300/-PW4000:

2 136 kg (300 lb) 272 kg (600 lb)

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57-51-02 Trailing Edge Flap Hinge Fairings

Each fairing is comprised of three sections. All or part of one fairing may be missing.

1. If the forward section is removed, the mid and aft sections must be removed also.

2. If the mid section is removed, the aft section must be removed. The forward section may remaininstalled.

3. The aft section may be removed without removing the forward or mid sections.

NOTE: Any combination of the authorized numbers of APPENDIX A (CDL) Items 57-51-01 and 57-51-02 may be missing.

For -300/-80C2:

6 1180 kg (2600 lb) 1315 kg (2900 lb)

For -300/PW:

6 772 kg (1700 lb) 1724 kg (3800 lb)

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57-51-03 Inboard Trailing Edge Fixed Panel

For -300/-80C2:

2 1642 kg (3620 lb) 1851 kg (4080 lb)

For -300/PW:

2 1044 kg (2300 lb) 2219 kg (4890 lb)

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57-51-04 Outboard Trailing Edge Fixed Panel

For -300/-80C2:

2 1570 kg (3460 lb) 1765 kg (3890 lb)

For -300/PW:

2 998 kg (2200 lb) 2119 kg (4670 lb)

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57-51-07 Main Landing Gear Side Brace Trunnion Aft Fairings

Both may be missing.

For -300:

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57-53-01 Inboard Trailing Edge Flaps

If a performance restriction is required due to on-ground hail damage, as assessed in the StructuralRepair Manual 51-10-04, for each damaged flap the performance limited weights are reduced by thefollowing:

For -300/-80C2:

2 409 kg (900 lb) 459 kg (1010 lb)

For -300/PW:

2 259 kg (570 lb) 549 kg (1210 lb)

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57-53-02 Outboard Trailing Edge Flaps

If a performance restriction is required due to on-ground hail damage, as assessed in the StructuralRepair Manual 51-10-04, for each damaged flap the performance limited weights are reduced by thefollowing:

For -300/-80C2:

2 817 kg (1800 lb) 921 kg (2030 lb)

For -300/PW:

2 522 kg (1150 lb) 1103 kg (2430 lb)

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57-60-01 Inboard Aileron

If a performance restriction is required due to on-ground hail damage, as assessed in the StructuralRepair Manual 51-10-04, for each damaged aileron the performance limited weights are reduced bythe following:

For -300/-80C2:

2 277 kg (610 lb) 309 kg (680 lb)

For -300/PW:

2 177 kg (390 lb) 372 kg (820 lb)

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57-60-02 Outboard Aileron

If a performance restriction is required due to on-ground hail damage, as assessed in the StructuralRepair Manual 51-10-04, for each damaged aileron the performance limited weights are reduced bythe following:

For -300/-80C2:

2 368 kg (810 lb) 413 kg (910 lb)

For -300/PW:

2 232 kg (510 lb) 495 kg (1090 lb)

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57-70-01 Spoiler Panels

If a performance restriction is required due to on-ground hail damage, as assessed in the StructuralRepair Manual 51-10-04, for each damaged spoiler panel the performance limited weights arereduced by the following:

For -300/-80C2:

12 168 kg (370 lb) 186 kg (410 lb)

For -300/PW:

12 109 kg (240 lb) 223 kg (490 lb)

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71. POWER PLANTLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

71-11-01 Fan Cowl Pressure Relief Access Doors 71-2

71-11-02 Fan Cowl Oil Tank Access Doors 71-3

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71-11-01 Fan Cowl Pressure Relief Access Doors

For PW:

For 80C2:

One or both may be missing provided the Fan Cowl Oil Tank Access Door (APPENDIX A (CDL) item71-11-02) on the same nacelle is not missing.

For GE and PW:

2 (1 per nacelle) Negligible penalty Negligible penalty

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71-11-02 Fan Cowl Oil Tank Access Doors

One or both may be missing provided the Fan Cowl Pressure Relief Access Door (APPENDIX A CDL

item 71-11-01) on the same nacelle is not missing.Performance limited weights are reduced by the following:

For -300:

2 (1 per nacelle) No penalty 91 kg (200 lb)

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78. EXHAUSTLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

78-31-01 Thrust Reverser Sleeve Actuator Access Panels 78-278-31-02 Thrust Reverser Track Fairings 78-3

78-31-03 Fan Thrust Reverser Blocker Doors 78-4

78-31-04 Thrust Reverser Cascade Vane Segments 78-5

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78-31-01 Thrust Reverser Sleeve Actuator Access Panels

A maximum of eight (four per nacelle) in any combination may be missing.

NOTE: Any combination of the authorized numbers of APPENDIX A (CDL) items 78-31-01, 78-31-02,78-31-03, and 78-31-04 may be missing.

For -300/GE:

12 (6 per nacelle) Negligible penalty Negligible penalty

For -300/PW:

12 (6 per nacelle) Negligible penalty 91 kg (200 lb)

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78-31-02 Thrust Reverser Track Fairings

NOTE: Any combination of the authorized numbers of APPENDIX A (CDL) items 78-31-01, 78-31-02,78-31-03, and 78-31-04 may be missing.

For -300/-80C2:

8 (4 per engine) 181 kg (400 lb) 272 kg (600 lb)

For -300/PW:

8 (4 per engine) 136 kg (300 lb) 272 kg (600 lb)

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78-31-03 Fan Thrust Reverser Blocker Doors

For CF6-80C2:

One may be missing from each reverser half of one engine provided the thrust reverser isdeactivated. Deactivate associated thrust reverser per reference MEL Item 78-31-01.

For PW:

A maximum of four (one per cowl half) may be missing.

NOTE 1: Drag links (for missing door) must be removed for all engine types.

NOTE 2: Any combination of the authorized numbers of APPENDIX A (CDL) items 78-31-01, 78-31-02, 78-31-03, and 78-31-04 may be missing.

For -300/-80C2:

24 (6 per cowl half) 363 kg (800 lb) 726 kg (1600 lb)

For -300/PW4000:

24 (6 per cowl half) 1089 kg (2400 lb) 1043 kg (2300 lb)

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78-31-04 Thrust Reverser Cascade Vane Segments

For 300/PW:

A maximum of three per reverser side (six per engine) may be missing provided:

1. Segments are missing from one engine only and thrust reverser is deactivated.

2. No two adjacent segments are missing.

3. Top and bottom segments remain in place.

NOTE 1: Deactivate associated thrust reverser per MEL Item 78-31-01.

NOTE 2: Any combination of the authorized numbers of CDL items 78-31-01, 78-31-02, 78-31-03,and 78-31-04 may be missing.

36 (18 per engine) No penalty No penalty

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LAN AIRLINES S.A.TRANSPORTE AEREO S.A.

Boeing 767-300

Append ix B(Non-Essential Equipment & Furnishings (NEF))

Revision Original April 20, 2010

This document is applicable to all B767 Lan Airlines/Transpor te Aéreo

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RECORD OF REVISIONSLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

REVISION N° Original PAGE 1

APPENDIX B (NEF) B767-300 DATE 20-APR-2010

REV NUMBER EDITED DATE UP-DATED BY

Original 15/12/2007 M. Delavenne

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Highlights of change Revision Original

This revision is issue to change the name of this appendix from APPENDIX C to APPENDIX B

No technical change are introduce in this revision.

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LIST OF EFFECTIVE PAGESLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

REVISION N° Orig inal PAGE 1

SYSTEM PAGE REVISION REV DATE

Cover - - - Original 20 Apr, 2010

Record of Revisions RR-1 Original 20 Apr, 2010

Highlights of Change HC-1 Original 20 Apr, 2010

Contents CONT Original 20 Apr, 2010

Definitions DEF-1 Original 20 Apr, 2010

Preamble PRE-1 Original 20 Apr, 2010

NEF Program 1 thru 9 Original 20 Apr, 2010

Index of NEF Item 1 thru 3 Original 20 Apr, 2010

NEF Deferral List 1 thru 8 Original 20 Apr, 2010

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DEFINITIONSLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

NONESSENTIAL EQUIPMENT AND FURNISHINGS (NEF). NEF are those items installed on the

aircraft as part of the original type certification, supplemental type certificate, or other form ofalteration that have no effect on the safe operation of flight and would not be required by theapplicable certification rules or operational rules. They are those items that, if inoperative, damaged,or missing, have no effect on the aircraft’s ability to be operated safely under all operationalconditions. These nonessential items may be installed in areas including, but not limited to, thepassenger compartment, flight deck area, service areas, cargo areas, crew rest areas, lavatories,and galley areas. NEF items are not items already identified in the MEL or CDL of the applicableaircraft. They do not include items that are functionally required to meet the certification rule or forcompliance with any operational rule.

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PREAMBLELAN AIRLINES S.A.TRANSPORTED AEREO S.A.

INTRODUCTION

NONESSENTIAL EQUIPMENT AND FURNISHINGS (NEF)

NEF are those items installed on the aircraft as part of the original type certification, supplementaltype certificate, or other form of alteration that have no effect on the safe operation of flight and wouldnot be required by the applicable certification rules or operational rules. They are those items that, ifdamaged, inoperative, or missing, have no effect on the aircraft’s ability to be operated safely underall operational conditions. These nonessential items may be installed in areas including, but notlimited to:

Cargo Areas

Crew Rest Areas

Flight Deck Area

Galley Area Lavatories

Passenger Compartment

Service Areas

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NEF PROGRAMLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

NEF PROGRAM

NEF Program is as follows: A. A NEF List has been developed and NEF Items are tracked through the use of the aircraft’s

Maintenance Flight Log.

B. The NEF Item evaluation process will include the following items:

Is the item required for the operational rules in which the aircraft is operated?

Does it create the potential for fire/smoke or other hazardous conditions?

Could it have an adverse effect on other required systems or components?

Does its condition potentially affect the safety of crew, passengers, or service personnel?

Could it have a negative impact on emergency or abnormal procedures?

Does it create additional workload for the crew at critical times of flight or flightpreparation?

Crewmembers may need to evaluate the deferred NEF on a flight-by-flight basis.Note: The above evaluation process must be accomplished for the damaged,

inoperative, or missing items at its face value, and also for the underlying causeof the discrepancy.

C. The codes and definition of these,are the same defined in the MEL.

D. The NEF List and program description will be kept in the aircraft specific MinimumEquipment List (MEL) Binder.

E. If a discrepancy is discovered that is not covered by the aircraft’s Configuration DeviationList (CDL), MEL or NEF List. The Flight Crew, with the assistance of the MaintenanceDepartment, may perform the NEF Item Process to determine if the discrepancy can beadded, as a new item, to the NEF List. The discrepancy must meet the NEF Item Process orit will require the issue to be resolved before further flight.

NEF Item Process

NEF Item Process is the process to include a new item in the NEF List.

Process :

1. Verify that the discrepancy comply with the NEF Decision Tree (Figure 1) to be added inthe NEF List as a new item.

2. Fill the “Document Control NEF (MOC Department)”. This document must be filled byMaintenance Operational Control (MOC), and send to Maintenance Quality Control toevaluate if the new item can be included in the NEF list.

NOTE: An example of the “Document Control NEF (MOC Department)” is shows in page9

3. If the new item can be included in the NEF list:

a) Maintenance Quality Control must established the repair interval of the new item:

1) For item corresponding to ATA 25 repair interval D (120 calendar days). Notrepair interval extension is allowed.

7/25/2019 Mel boeing 767

2) For another ATA (different of ATA 25) repairs must be made within 45 calendardays or check A whichever occur first. Only one repair extension is allowed

subject to the approval of Maintenance Quality Control provided rectification isaccomplished at the earliest opportunity.

3) For especial case the repair interval must be defined by Maintenance QualityControl and Maintenance Operational Control (MOC).

b) Maintenance Quality Control must establish the damage allowed and remark orexception for each new item that will be included in the NEF list.

4. When the new item process has been completed, Maintenance Quality Control must sendto the in-charge of MEL person (Estandares Operacionales) the new NEF item to beincluded in the next revision of the Appendix B (NEF).

Register and control of the deferral NEF Item will be controlled by Procedimientos LAN

(PRL) N° QA-0046 “CREACION, ADMINISTRACION Y CONTROL DE LOS DIFERIDOS(MEL, CDL Y NEF)”

(NEF decisión tree discussion on next page)

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NEF DECISION TREE DISCUSSION

1.0 Discrepancy noted in aircraft logbook. The inoperative, damaged or missing item must beidentified and documented in the aircraft logbook (or other approved location) by:

1.0 Discrepancy noted in

aircraft logbook

1. Flight Crew; or

2. Company maintenance personnel; or

3. Personnel authorized and approved to perform such functions asoutlined in the maintenance program.

2.0 Can the item be deferred in accordance with (IAW) the MMEL, CDL, or the MEL?

1. If the inoperative, damaged, or missing item is listed in the MEL orCDL, then the deferral procedures for that item must be followed. If

the item is a subcomponent of a primary system identified in theMEL/CDL, where no previous relief was authorized, thesubcomponent may not be deferred in accordance with the NEFprocedures outlined in chapter 25 of the MEL.

2.1 Follow MEL/CDL procedures.

2.1 Follow MEL/CDL

procedures

1. If the item is identified in another part of the MEL/CDL, thenthe procedures approved for the deferral of such item mustbe followed.

3.0 Is item on the NEF deferral lis t?

3.0 Is item

on NEF

deferral list?

1. Is the item on the NEF list? If yes, then follow the NEF deferralprocedures in step 3.1. (Items that are not previously on the NEF listshould proceed to step 4.0.)

3.1 Defer item IAW the NEF deferral program.

3.1 De fer i tem

IAW the NEF

program

1. If the item is identified in the NEF deferral list, then theprocedures approved for the deferral of such item shall befollowed.

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4.0 Does the item affect the safety of flight?

4.0 Does the Itemaffect the safety of

flight?

1. Is it obvious from a maintenance or operational perspective thatthe item, in and of itself, could have an adverse effect on thesafe conduct of flight? If there is an obvious safety-of-flightissue, then the inoperative, damaged, or missing item may notbe deferred and step 4.1 shall be followed.

4.1 Repair item pr ior to f light.

4.1 Rep air Item p r ior to

f l ight.

1. The item may not be deferred and must be repairedprior to flight.

5.0 Can source (underlying cause) of the discrepancy be identi fied? (If applicable)

5.0 Can source

(underlying cause)of the discrepancy

be identified?

1. Can the source of the discrepancy be identified? This step mayor may not apply to the item under consideration. If the sourcecan be identified, then proceed to step 6.0, otherwise proceedto step 4.1.

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6.0 Can source (underlying cause) of discrepancy affect equivalent levels of safety?

6.0 Can source(underlying cause) of the discrepancy affectequivalent levels of

safety? **

1. If the source (underlying cause) of the discrepancy affectequivalent levels of safety, then it must be determined if itcan be isolated from all other systems so as to alleviateany safety concern.

** Note: In making this determination, very close

coordination between the Flight Crew,

maintenance and operations personnel

may be required.

2. If, after review, the source of the discrepancy could beconsidered a safety-of-flight concern, the item must berepaired prior to flight (step 4.1). If the source of thediscrepancy is not a safety-of-flight concern then defer theitem in accordance with the approved NEF procedures instep 8.0. If it cannot be determined, or is uncertain, that thesource of the discrepancy is a safety-of-flight concern thenproceed to 7.0.

7.0 Can source (underlying cause) of discrepancy be isolated from the system with

applicable maintenance procedures?

7.0 Can source of discrepancy be

isolated from systemwith applicable

maintenance

procedures?

1. If applicable, the source (underlying cause) of the discrepancy

must be isolated from all other systems so as to alleviate thesafety-of-flight concern.

2. If the item cannot be safely isolated then the item must berepaired prior to flight (step 4.1).

3. If isolated, the isolation of the source must pass the entire testidentified in the evaluative process (steps 4.0-7.0) for the item.

4. If source can be isolated then proceed to step 8.0.

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8.0 Defer Item IAW the DGAC Approved NEF Program.

1. Defer the item if, after completing the previous 8 steps, the itemcan be deferred IAW the DGAC Approved NEF Program.

Note: Before an item can be deferred as an NEF item, theNEF program evaluation process for determining shallbe followed if an item can be considered a NEF.

Although NEF items are not safety-of-flight items, theyhave not been evaluated through the normal reviewprocess and therefore require the concurrence of theFlight Crew, Maintenance, and Operational personnel,if applicable. NEF items are not deferred under theauthority of an airframe and powerplant certificate butrather the item is deferred under the NEF program.

The evaluation p rocess should determine items such as:

a. Is the item required for the operational rules in which the

aircraft is operated?

b. Does it create the potential for fire/smoke or other

hazardous conditions?

c. Could it have an adverse effect on other required

systems or components?

d. Does its condition potentially affect the safety of

passengers, crew, or service personnel?

e. Could it have a negative impact on emergency or

abnormal procedures?

f. Does it create additional workload for the crew at critical

times of flight or f light preparation?

g. Crewmembers may need to evaluate the deferred NEF

on a flight -by-flight basis.

Note: The above evaluation process must be accomplished for theinoperative, damaged, or missing items at its face value, andalso for the underlying cause of the discrepancy.

8.0 Defer Item IAW theDGAC Approved NEFProgram

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9.0 Update NEF deferral li st as requi red.

9 .0 Upda te NEF De fe r ra l

L is t as requ i red.

1. Lan Airlines will continually add items to the NEF list as they seefit.

10.0 Provide NEF Items to DGAC.

10.0 Provide NEF items

to CHDO.

1. Lan Airlines will provide the items placed in the NEF List to theDGAC for review. This review is not to be conceived as arequirement to approve the NEF List items. It is merely a meansto provide oversight to ensure the program is effective.

Figure 1: NEF Decision Tree (On next Page)

10.0 Provided NEF ListItem to DGAC

7/25/2019 Mel boeing 767

Discrepancy noted inaircraft logbook

2.0Can the item bedeferred IAW the

MEL/CDL?

3.0is item on NEFdeferral list?

4.0Does the item affectthe safety of flight

5.0Can source

(underlying cause) ofdiscrepancy be identified?

Yes or N/A

6.0Can source

(underlying cause)of discrepancy affect

equivalent levels of safety?

Uncertain

7.0Can source

of discrepancy be isolatedfrom system with applicablemaintenance procedures?

FINISH

2.1 Follow MEL/CDLprocedures

8.0 Defer item IAW theapproved NEF program

9.0 Update NEFList

10.0 Provided NEF Listto DGAC.

3.1 Defer item IAWNEF program. Yes

4.1 Repair item priorto flight. Yes

** NOTE (6.0)Coordination with Captain/Flightoperations may be required

Figure 1: NEF Decision

7/25/2019 Mel boeing 767

Documento Control NEF (MOC Department)

DI SCREPANCY

NEF DECI SI ON TREE DI SCUSSI ON

QUESTI ON YES NO

1. Di scr epancy not ed i n ai r craf t l ogbook.

2. Can t he i t embe def err ed i n accordance wi t h ( I AW) t he MMEL, CDL, or

t he MEL?

3. I s i t em on t he NEF def err al l i st?

4. Does t he i t em af f ect t he saf et y of f l i ght ?

5. Can sour ce ( under l yi ng cause) of t he di scr epancy be i dent i f i ed? ( I fappl i cabl e)

6. Can sour ce ( under l yi ng cause) of di scr epancy af f ect equi val ent

l evel s of saf et y?

7. I t i s no a wear ?

8. I t i s not a Leak?

9. I t i s not a el ectr i cal syst em?

10. Can sour ce ( under l yi ng cause) of di scr epancy be i sol at ed f r omt he

syst emwi t h appl i cabl e mai nt enance pr ocedur es?

OBSERVATI ONS

MOC Number

Bar code

MOC Supervi sor Name

Si gnat ur e

TAI L NUMBER

DATE NEF # 1

NEF Number

7/25/2019 Mel boeing 767

INDEXLAN AIRLINES S.A.TRANSPORTED AEREO S.A.

INDEX OF NEF DEFERRAL LIST

25-20-1 PASSENGER CABIN

25-20-1-1) Carpet/Floor Covering 125-20-1-2) Tapestry 125-20-1-3) Interior Paint 125-20-1-4) Curtains/Tiebacks (Except in Crew Rest Areas) 125-20-1-5) Wall Covers, Ceiling Panels, Decorative Panels (Except Air Grilles) 125-20-1-6) Door Cover and Slide Container Cover 125-20-1-7) Air Grilles 125-20-1-8) Magazine Rack/Restraint 125-20-1-9) Seat Back/Bulkhead/Sidewall Literature Pockets 125-20-1-10) Cabin Windows 1

25-20-1-11) Electrical Outlet Cover (115 V) (For service purpose) 125-20-1-12) Window Blind 225-20-1-13) Individual Outlet of Gasper Fan 2

25-20-2 SEATS

25-20-2-1) Paint, Decorative Elements, Bachshell, Covers 225-20-2-2) Footrest, Legrest, Headrest 225-20-2-3) Armrest 225-20-2-4) Individual Reading lights 225-20-2-5) Passenger Seat Tray Table Assembly (& Latch) 225-20-2-6) Passenger Seat Cushions 2

25-20-2-7) SEAT Track Covers 325-20-2-8) Passenger Seat Call Light(s) 325-20-2-9) Passenger Seat Call Button(s)

25-20-3 PLACARDS/DECALS

25-20-3-1) Security Placard/Decal(s) 325-20-3-2) Miscellaneous Placards7Decals 3

25-20-4 IN-FLIGHT ENTERTEINMENT SYSTEM IFE

25-20-4-1) IFE System25-20-4-2) In-Seat Video Control 325-20-4-3) In-Arm Seat Video Display(s) 325-20-4-4) Video Monitor(s) (wall-or-overhead-mounted units) 325-20-4-5) Seat Back Video Monitor(s) 425-20-4-6) PC Power 425-20-4-7) Music System 425-20-4-8) Cabin Speaker(s) 4

7/25/2019 Mel boeing 767

23-20-5 LIGHTING SYSTEM

25-20-5-1) Reading Lights 4

25-20-5-2) Lens covers (Except Lens Covers of Emergency Lights with anylegend)

25-20-5-3) Emergency Escape Path Marking Covers 4

25-20-6 PASSENGER CABIN EQUIPMENT

25-20-6-1) Demo kit 425-20-6-3) Baby Bassinet (Included Restraint) 525-20-6-4) Kit de Mercancias Peligrosas 5

25-20-7 GALLEYS

25-20-7-1) Attendant Work Table 5

25-20-7-2) Galley Floor Covers 525-20-7-3) Trolley Compartments Panels, Guides 525-20-7-5) Coffe Maker, Water Boiler 525-20-7-6) Wine Chiller 525-20-7-7) Ovens and Control 525-20-7-8) Air Chiller 525-20-7-9) Trash Compactor (If installed) 525-20-7-10) Galley Heating and Ventilation System (If installed) 525-20-7-11) Galley Floor Heating System 525-20-7-12) Galley Sink Drain Screen 525-20-7-13) Clips or Documentation Support 625-20-7-14) Support for Ice-Cup 6

25-20-7-15) Mirrors 625-20-7-16) Galley Electrical Outlet (115 V) 625-20-7-17) Galley Ashtray (If installed) 625-20-7-18) Coat Hanger 6

25-20-8 COCKPIT

25-20-8-1) Cup Holders (If installed) 625-20-8-2) Sun Visors 625-20-8-3) Chart Holders Clips 625-20-8-4) Spare Bulb Kit and Content 625-20-8-5) Food Tray (If installed) 625-20-8-6) Carpet-Floor Covering 6

25-20-8-7) Foot Rest 625-20-8-8) Flight Deck Door Hold-Open device 625-20-8-9) Second Microphone Holder 625-20-8-10) Multipurpose Clips (Hat, Coats) 725-20-8-11) Coat Hanger Bar 7

7/25/2019 Mel boeing 767

25-20-9 LAVATORIES

25-20-9-1) Lavatories Folder Door Spring 7

25-20-9-2) Lavatories Panels, Trim (Side Wall, Ceiling) 725-20-9-3) Soap Dispenser 725-20-9-4) Mirrors 725-20-9-5) Toilet Cover 725-20-9-6) Lavatories Interior Compartments Door 725-20-9-7) Toilet Paper Holder 725-20-9-8) Paper Dispenser 725-20-9-9) Lavatory Coat Hook 725-20-9-10) Lavatories Lights System /Except Emergency Lights) 725-20-9-11) Lavatories Lights Covers 725-20-9-13) Wash Basin Drain Handle 825-20-9-14) Baby Bassinet 8

25-20-9-15) Miscellaneous Decals 825-20-9-16) Lavatory Speaker Grill Cover 8

25-20-23 COMMUNICATIONS

25-20-23-1) Passenger to Attendant Call System. Visual and Audio Alerting 8

7/25/2019 Mel boeing 767

APPENDIX BNON-ESSENTIAL EQUIPMENT & FURNISHINGS (NEF) LIST

LAN AIRLINES S.A.TRANSPORTE AEREO S.A

B 767-300NEF LIST

PAGEREVDATE

1Original20-APR- 2010

SYSTEM AND 1. 2. REPAIR INTERVAL

SEQUENCE 3. DAMAGE ALLOWED

NUMBERS ITEM 4. REMARK OR EXCEPTION

25-20-1-1) Carpet/FloorCovering

D May be dirty, worn, torn,frayed, stained, damaged ormissing.

The Carpet/Floor Covering may bedamaged or torn provided must notpresent hazard to pax/crew or impedeemergency egress.

25-20-1-2) Tapestry D May be dirty, worn, torn,soiled, frayed, stained,damaged or missing.

25-20-1-3) Interior Paint D May be dirty, soiled, torn,frayed, stained, damaged ormissing.

25-20-1-4) Curtains/Tiebacks(Except in CrewRest Areas)

D May be dirty, worn, torn,soiled, frayed, stained,damaged or missing

For curtains in Crew Rest Areas Referto MEL item 25-25-6

25-20-1-5) Wall Covers,Ceiling Panels,Decorative Panels,Laminated Panels(Except Air Grilles)

D May be dirty, worn, torn,soiled, frayed or stained.

25-20-1-6) Door Cover andSlide ContainerCover

D May be dirty, soiled, orminor/insignificant damage.

May be minor/insignificant damageprovided Minor/insignificant damagedoes not affect the integrity of cover.

25-20-1-7) Air Grilles D May be dirty, soiled or minusdamage.

Minus damage may be acceptedprovided the integrity of the air grillesis not affected.

25-20-1-8) Magazine Rack/Restraint

D May be dirty, soiled, ordamage.

25-20-1-9) Seatback/

Bulkhead/SidewallLiterature Pockets

D May be damage or missing May be damage provided:

Must not present hazard to passengeror impede normal and emergencyegress.

25-20-1-10) Cabin Windows D Moisture between panes

25-20-1-11) Electrical OutletCover (115 V)(For ServicePurpose)

D Cover may be broken, looseor missing

May be broken, loose or missingprovided electrical plugs must beelectrically deactivated.

7/25/2019 Mel boeing 767

B 767-300NEF LIST

PAGEREVDATE

25-20-1-12) Window Blind D May be dirty, soiled, damageor inoperative

May be inoperative in any position,

25-20-1-13) IndividualsOutlet ofGasper Fan

D May be damage orinoperative

25-20-2 SEATS

25-20-2-1) Paint, DecorativeElements,Bachshell,Covers, etc.

D May be dirty, soiled, damageor loosing.

The decorative elements Bachshell,Covers, may be damaged or tornprovided:Must not present hazard to pax/crewor impede emergency egress.

25-20-2-2) Footrest, Legrest,Headrest

D May be inoperative. May be inoperative provided:a) Footrest, Legrest o Headrest does

not restrict any passenger fromaccess to main aircraft aisle, and

b) Footrest, Legrest o Headrest doesnot block an Emergency Exit, and

c) Footrest, Legrest o Headrest mustbe locked in retract position.

25-20-2-3) Armrest D May be dirty, soiled, damageor loose.

May be damage provided the armrestis operative.

NOTE : If the armrest is inoperative,Refer to MEL item 25-25-2.

25-20-2-4) IndividualReading Lights

D May be inoperative, damageor missing.

25-20-2-5) Passenger SeatTray Table

Assembly(& Latch)

D May be dirty, soiled,damage, inoperative or

missing.

May be damage or inoperativeprovided:

a) Passenger tray table does notrestrict any passenger fromaccess to main aircraft aisle, and

b) Passenger tray table does notblock an Emergency Exit, and

c) Passenger tray table must belocked in stowed position, and

d) Passenger tray table must beplacarded: INOPERATIVE-DO NOT

USE INOPERATIVO-NO USAR.

25-20-2-6) Passenger SeatCushion(s)

D May be worn, torn, frayed orstained

7/25/2019 Mel boeing 767

B 767-300NEF LIST

PAGEREVDATE

25-20-2 SEATS

25-20-2-7) SEAT TrackCovers

D May be damaged, loose ormissing

SEAT Track Covers may be damagedor missing provided any exposedwiring must be protected.

25-20-2-8) Passenger SeatCall Light(s)

D May be inoperative ormissing

25-20-2-9) Passenger SeatCall Button(s)

D May be inoperative ormissing

25-20-3 PLACARDS/DECALS

25-20-3-1) SecurityPlacards/Decals

D May be dirty or degraded Security Placards/decals may bedegraded provided they are legible oreasily understand their content.

25-20-3-2) MiscellaneousPlacards/Decals

D May be dirty, damaged ormissing.

25-20-4 IN-FLIGHT

ENTERTEINMENT

SYSTEM IFE

25-20-4-1) IFE System D May be inoperative May be inoperative providedPassenger securityannouncement/demostration is madethrough other available system.

25-20-4-2) In-Seat VideoControl.

D May be damaged, missing orinoperative.

25-20-4-3) In-Arm Seat VideoDisplay(s)

D May be damaged orinoperative.

May be inoperative provided VideoDisplay must be locked in stowedposition.

NOTE: If the In-Arm Seat VideoDisplay is used for “safety video”purpose, may be inoperative providedwall or overhead video monitor isoperative and visible from affectedoccupied seat.

25-20-4-4) Video Monitor(s)(wall-or-overhead-mounted units)

NOTE: If the wall-or-overheadmonitors are used for “safety video”purpose, may be inoperative providedin-arm seat video display or seat backvideo monitor is operative on eachoccupied seat.

7/25/2019 Mel boeing 767

B 767-300NEF LIST

PAGEREVDATE

25-20-4 IN-FLIGHT

ENTERTEINMENT

SYSTEM IFE

25-20-4-5) Seat Back VideoMonitor(s)

NOTE: If the seat back video monitorsare used for “safety video” purpose,may be inoperative provided wall oroverhead video monitor or adjacentseat back video monitor is operativeand visible from affected occupiedseat.

25-20-4-6) PC Power D May be inoperative.

25-20-4-7) Music System D May be inoperative

25-20-4-8) Cabin Speaker D May have static interference May have static interference providedPassenger Address System is audibleand intelligible.

NOTE : If Cabin Speaker isconsidered inoperative refer to MELitem 23-31-1.

25-20-5 LIGHTING SYSTEM

25-20-5-1) Reading Lights D May be inoperative ormissing

25-20-5-2) Lens Covers(Except LensCovers ofEmergency Lightswith any legend)

D May be damaged or missing Lens covers may be damaged ormissing provided lights operatesnormally.

25-20-5-3) Emergency EscapePath Marking

Covers

C May be damaged. Covers may be damaged providedEmergency Escape Path Marking

System operates normally and isreadily legible.

EQUIPMENT

25-20-6-1) Demo Kit D May be incomplete ormissing

May be incomplete or missingprovided Security Video in the IFEsystem operate normally.

7/25/2019 Mel boeing 767

B 767-300NEF LIST

PAGEREVDATE

EQUIPMENT

25-20-6-3) Baby Bassinet(Included Restraint)

D May be damage, inoperativeor missing.

25-20-6-4) Kit de MercanciasPeligrosas

A May be damage, missing orincomplete.

The aircraft may be continue the flightor series of flights and return to themain base (SCL) where repairs mustbe made.

25-20-7 GALLEYS

25-20-7-1) Attendant WorkTable

D May be soiled or damage

25-20-7-2) Galley FloorCovers

D May be worn, soiled, frayed,torn, damage or loose

Floor covers may be torn, damage orloose provided torn, damage or loosedoes not restrict passenger/crewegress in normal and emergencyconditions.

25-20-7-3) Trolleys

CompartmentsPanels, Guides

D May be damage or paint is

not in good conditions.

May be damage provided trolleys can

be locked in its stowed position.

25-20-7-5) Coffe Marker,Water Boiler

D May be inoperative

25-20-7-6) Wine Chiller D May be inoperative

25-20-7-7) Oven andControls

25-20-7-8) Air Chiller D May be inoperative

25-20-7-9) Trash Compactor D May be inoperative

25-20-7-10) Heating andVentilation System(if installed)

25-20-7-11) Floor HeatingSystem

25-20-7-12) Sink Drain Screen D May be damage, inoperativeor missing.

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B 767-300NEF LIST

PAGEREVDATE

25-20-7 GALLEYS

25-20-7-13) Clips orDocumentationSupport

D May be damage or missing.

25-20-7-14) Support for ice-cup D Puede estar dañada ofaltante

25-20-7-15) Mirrors D May be damage or missing.

25-20-7-16) Electrical Outlet(115V). D May be inoperative. May be inoperative provided affectedelectrical outlet must be placardedINOPERATIVE-INOPERATIVO.

25-20-7-17) Ashtrays(If installed)

D May be damage or missing. NOTE: For Exterior Lavatory doorashtray refer to MEL item 25-38-1.

mel boeing 767

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