L

5 yearl5r000 hourControl Rod Inspection

Chapter 5-10-00

Aviation Services Unlimitedo Inc.Hgr #60 Wiley Post Airport

Bethany, OK 73008C.R.S. #X6UR264N

L

Aileron Rods

002t \L*nn nn,Ytnlp I naNTENANcE

EnAaAnnru:rrsrc'rgttD I MANUAL

TOC

MAIN

SYSTEM AND COMPONENT

(g) Flexible Shaftlnboard Left

(b) Rod AssemblY

(c) Tube

(h) Flexible Shaft 193545-505Inboard Right

tffiir@.'1(allr fls6lAsssnbly t n 51302G501 t

PART NUIII|BER

193545-501

OVERHAULOR

REPLACE

X-Ray Insp.(See Note)

513506-503,' X-RaY InsP.

-503RD or -503RE (See Note)

51 3512-3 X-Ray lnsp.(See Note)

REPLACE

10,000

10,000

NOTE: (1) 1O years or 1O,OOO hours, whichever occurs first, and each 5 years or

5000 hours, whichever occurs first, thereafter - perform X-Ray

inspection in accordance with Non-Destructive Testing Manual.

(2) For rod assemblies with greater than 9 years or greater than 9000 hours

on March 1, 1996, inspection is due l yeat or 1000 hours, whichever

occurs first, from March 1, 1996.

(3) When Rod Assembly 513506-5O3RE / -503RD are replaced by Tube

Assembly 513506-505 (stainless steel), the X-Ray requirement has been

eliminated.

t

5'1 0'00 ,J3#33

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Aileron Control Installation - \MngFigure 4(Sheet 1)

{/

Fig.4Page 0

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DETAIL A

tf

\DETAIL B

Aileron Control Installation - \MngFigure 4(Sheet 2)

Fig.4Page I

Jul 31/200527-10O0

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I

DETAIL C

Aileron Control Installation - WingFigure 4(Sheet 3)

Fig.4Page2

Jul31/2005

(

27-10-00

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DETAIL D

Alleron Control Installation - \MngFigure 4(Sheet 4)

Fig.4Page 3

Jul 31/2005

+:

27-10-00

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(

FIGURE &ITEM NO.

PART NUMBER NOMENCIATURE

234567

AIRCRAFTEFFECTIVIW

CODE

UNITSPER

ASSY

4-

225

230

240

250

260

270

2E0

290

Moo310

315

- 320

325

330 I*ol

3so I

AN960416

MA1782G4

MS2466t134

NAS7S5-009

ST4BW

6&1832

SM4€M5

NAS509€

MS55$2

5003513-503

513505-3

513512-1

513026-501

513512-3

513025-501

513501-13

513501-15

513501-7

MS1782S.3

MS24665-71

AN960€16L

513501-1 1

51351+503

.WASHER

.NUT

.COTTER PIN

.'::''*

..ROD END

. .ROD END (ALT)

..ROD END (ALT)

.,NUT

. .LOCK, ROD END

..FrfitNG

..TUBE

.ROD ASSY

..FITTING

..TUBE

.GUIDE ROLLER

ATTACHING PARTS

.SCREW(SUPERSEDED BY rTEM 320)

.SCREW(SUPERSEDES |TEM 315)

.WASHER

.NUT

.COTTER PIN

.WASHER

.BUSHING

.STRAP

(v02e0e)

(vD3279)

(w78e6)

I

1

1

1

1

2

2

2

2

2

2

1

1

2

1

4

1

1

1

1

1

1

1

1

- ITEM NOT ILLUSTRATED

Fig.4Page 6

Jul 311200527-10-00

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T

FIGURE &ITEM NO.

PART NUMBER NOMENCTATURE

234567

AIRCRAFTEFFECTIVITY

CODE

UNITSPER

ASSY

4- 360

400

450

fi

410

420

430

40

5135't+fi7

51351+508

51350&503

51350S503RD

5135F503RE

513506-505

NA9464P+16

MS620+16D

4N960.416

MS17826-4

MS2466S134

NAS754-009

NA9464P+14

MS6204-14D

MS17826-4

MS2466$134

NAS75-4-022

1{AS77-4-10

ST4BW

.STRAP, LH

:l:'-'.RODASSY(SUPERSEDED BY |TEM 380)

.RODASSY(SUPERSEDES |TEM 370 & lS SUPERSEDED BYITEM 390)

.RODASSY(SUPERSEDES ITEM 370 AND 380)

.ROD ASSY(SUPERSEDES ITEMS 370, 380 AND 390)(REF. SB 't123-27-057 FOR MODEL 1123)(REF. SB 1124-27-144 FOR MODEL 1124)

ATTACHING PARTS

.BOLT

.BOLT (ALT)

.WASHER

.NUT

.COTTER PIN

.BUSHING

.BOLT

.BOLT (ALT)

.NUT

.COTTER PIN

.BUSHING

.BUSHING

.ROD END (v0290e)

1

1

1

,|

1

1

1

1

1

1

1

1

1

1

1

1

1

2

- ITEM NOT ILLUSTRATED

Fig.4PageT

Jul 31/200527-10-00

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FIGURE &ITEM NO.

PART NUMBER NOMENCLATURE

t234567

AIRCRAFTEFFECTIVITY

CODE

UNITSPER

ASSY

4- 700

710

720

730

740

750

760

770

780

790

600

Iro

820

ST4BW

60-1832

sM4{M5

NAS509€

l,lAS559'2

513510-3

51 351 1-1

5't3511-2

NA9464Pffi8

NAS6205€8D

MS1782S,5

MS24665-134

NASTS5-0O9

t A276441KP5A

MS2O2O1KPsA

NAST$5-302

MS428H+13

NAS50S4

51302G501

NAS464PS.17

MS6204-17D

MA17E2S5

MS2456$134

..ROD END

. .ROD END (ALT)

. .ROD END (ALT)

..NUT

..LOCK ROD END

..ROD

.BELLCRANK LH

.BELLCMNK RH

ATTACHING PARTS

.BOLT

.BOLT (ALT)

.NUT

.COTTER PIN

:::''-"

..BEARING

. .BEARTNG (ALT)

..BUSHING

.BOLT

.NUT

.ROD ASSY

AfiACHING PARTS

.BOLT

.BOLT(ALT)

.NUT

.COTTER PIN

(v0290e)

(vD327e)

(w78e6)

1

1

1

1

1

1

1

1

1

1

1

1

1

2

2

1

1

2

1

1

1

1

1

- ITEM NOT ILLUSTRATED

Fig.4Page 10

Jul 31/200527-10-00

L

Rudder Rods

0u24\/ln ln.rurttp / hrAtNrENANcE

ENAETArcN^FrNA'flE IfD T fu]ANUAL

TOC

MAIN

SYSTEilI AND COMPONENT

:S8neRudder Conlrol System

OVERHAULOR

PART NUMBER REPLACE

X-Ray Insp,(See Note)

REPLACE

Grt

;fFr

Hpn Shafl(Rudder 533114-50lPedal Support)

(41 ElevatorControlSystem

Tube (Elevator 533012-13Bellcrank Assembly)

Rod Assembly' .3900009-23-13r18 X-Ray Insp.(Brake Pedal) (See Note)

Fod Assemblf 3900009-23-8.38 , X-Ray lnsp.(Brake Pedal , (See Note)hterconnect)

NorE: (1) 10 years or 10,000 hours, whichever occurs first, and each s years or5000 hours, whichever occurs first, thereafter - perform X-Rayinspection in accordance with Non-Destructive Testing Manual.

(2) For rod assemblies with greater than 9 years or greater than 9000 hourson March 1, 1996, inspection is due 1 year or 1000 hours, whicheveroccurs first, from March 1, 1996.

Visual Inspection(See Note)

NOTE: (1) 10 years or 10,000 hours, whichever occurs first, and each 5 years or5000 hours, whichever occurs first, thereafter - perform visual inspectionin accordance with Non-Destructive Testing Manual.

(2) For rod assemblies with greater than 9 years or greater than 9000 hourson March 1, 1996, inspection is due 1 year or 1000 hours, whicheveroccurs first, from March 1, 1996.

\.-_ 5'1 0'00 ,"13#3;

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16

DETAIL AS/N's 187 thru287

Rudder Control Installation - CockpitFigure 2(Sheet 2)

Fig.2Page 1

Aug 30/200327-20-00

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tAIRCRAFT

EFFECTIVITYCODE

2-1

10

533083

390000$2$25.38

AN2+13

533083-39

AN96G416L

MS17826-4

MS24665-134

MS27975-1

AN31&4R

3900009-23-8.38

MS270394-19

AN96M16L

MS2104214

MS27039-4-21

AN96S416L

MS2104214

BRE4O75

FJG6G1640

F+14Vn

PEDAL INSTL, RUDDER AND BRAKE(RUDDER CONTROL INSTL, COCKPTT)(REF.27-2OO0

.RODASSY

ATTACHING PARTS

.BOLT

.BOLT

.WASHER

.NUT

.COTTER PIN

.CLEVIS END

.NUT

.RODASSY

ATTACHING PARTS

.SCREW

.WASHER

.NUT

.SCREW

.WASHER

,NUT

.ROD END

.ROD END (ALT)

.ROD END (ALT)

.ROD END (ALT)

wTH "M" STAMPED ON SHANK)

(v81376)

(vD3279)

M/3134)

(w3134)

. ITEM NOT ILLUSTRATED

Fig.2Page I

Aug 30/200327-20-00

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AIRCRAFTEFFECTIVITY

CODE

543002-5

543002-9

s0302-25A

s0302-26A

543001-503

4N509-416R13

AN90&4161

MS2104214

3900009-23-1 3. 1 IMS2703$1-17

.ROD END (ALT)

ATTACHING PARTS

.:'l

.BELLCRANKASSY

,BELLCRANKASSY

.BELLCRANKASSY

ATTACHING PARTS

.BOLT

.WASHER

.NUT

.COTTER PIN

..BELLCRANK(usE wTH il3m2-1)

..BELLCRANK(usE vvrTH s43002-501)

..BEARING

,.BEARING

. BRACKET

ATTACHING PARTS

.SCREW

.WASHER

.NUT

.RODASSY

.SCREW

- ITEM NOT ILLUSTMTED

Flg.2Page I

Aug 30/200327-20-00

m24\il?AB.W8ittp / nlasrnttm

Enrct Atrcnffrrw.ritrcstro I PAETS CAW(rc

FIGURE &ITEM NO.

PART NUMBER NOMENCI.ATURE

23/.567

AIRCRAFTEFFECTIVITY

CODE

UN]TSPER

ASSY

250

260

tfl280

290

300

310

320

330

-rl

;

lMs2703e+34

I ANs60-416D

luszrocllI

I

153312S501

I

ltrrro.ro'.'I

lMs27o3e4-24

I

ANe6c416D

I MS2104214

I

lsssrr+sorAN960-12161

1900099{1S7s-1

MS43DD12-276

533002-503

533002-504

AN+26A

AN9604161

MS2104214

533002-7

53:m02-1+--

533002-12

NAS77-4-33

.30

..SCREW

..WASHER

..NUT

..SUPPORT

ATTACHING PARTS

..SCREW

..SCREW

..WASHER

..NUT

..SHAFT

,.WASHER

..WASHER

..SPACER

..PEDALASSY, LH

..PEDALASSY, RH

ATTACHING PARTS

..BOLT

..WASHER

..NUT

...BEARING

...PEDAL, LH

,..PEDAL, RH

..BUSHING

1

3

3

1

2

2

3

3

1

I

I1

1

1

1

1

1

I

2

1

1

4

.ITEM NOT ILLUETRATED

FE.2Page 11

Aug 30X200327-20-00

L

Nose Door Rods

\rnn--

-

AA4] .---'qnla.urt p I MA1wTENANaE

EnAa.4mnAFfrtgArEtto | frlllNUAL

TOC

MAIN

OVERHAULOR

SYSTETT ANO COi'PONENT PART NUtf,BER REPLACE REPLACE

NOTE: (1) Time count for inspection or testing shallcommence from the date thebottle was placed in service.

(2) Visual inspection of gas storage cylinder shall include both internal andexternal visual insoection.

(2) Bolts, Main \Alheel GY186-36Halves (WheelAssemblyP/N 5002806-1)

t, ",:x {3) t Rod Assembly 3900009-23-12.88 X-Ray Insp.

' (2 ea.l (NLG doors) (See Note)

400 Landingsor third tirechange

Page 206Jan 31/2006

trr (4) Rod AssemblY'(2 ea.) (NLG doors)

3900009-23-12.43 X-Raylnsp.(See Note)

ES12970-7 or 800 - Inspect. 3,2002236.0200.000 Ref.32-50-08,

Inspection / Check

ES12970-6 or 800 - Inspect. 3,2002236.0300.000 Ref. 32-50-08,

lnspection / Check

A01 ES 12970-7 1600 hr - Inspect.or 2236.02O0.000 Ref. 32-50-08,(See following Note) Inspection / Check

,,_ . (5) +Shaft Assembly (2 ea.l 283023-501 X-Ray Insp.*a'it' (NLG doors) (See Note)

NOTE: (1) 10 years or 10,000 hours, whichever occurs first, and each 5 years or5,000 hours, whichever occurs first, thereafter - perform X-Rayinspection in accordance with Non-Destructive Testing Manual.

(2) For rod assemblies with greater than 9 years or greater than 9,000 hourson March 1, 1996, inspection is due 1 year or 1,000 hours, whicheveroccurs first, from March 1, 1996.

(6) Steering BracketAssembly, Upper

(71 Steering BracketAssembly, Lower

__ (8) _ Sleeri1g BracketAssembly, Upper

5-1 0-00

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Nose Gear Door Mechanism lnstallationFigure 5(Sheet 1)

Fig.5Page 0

Aug 301200332-20-00

0[2n\m?lH.WJrXtp l//uusfnAfE0

r$ilcl ^m,AFrtwxsnrcuo

I PAEI$ clffiI00

FIGURE &ITEM NO.

PART NUMBER NOMENCIATURE

12u567

AIRCRAFTEFFECTIVIW

CODE

UNITSPER

ASSY

5- I

10

20

30

40

41

42

43

50

60

WO80

283002

2E301&501

AN+lOA

AN960-{16L

MS20365-428

BRE4lOOL

BACB1OA278L

FMS3E4

AN4.11A

AN96H16L

M520365-428

AN31GsR

283002401

39000092$12.88

BRE4O75

FeAtfrFJG6G'1840

FX,t44-148

MS20470AD3

AN31E4R

D@R MECHANISM INSTL, NLG(REF.32-20{0

.LINK

ATTACHING PARTS

.BOLT

.WASHER

.NUT

.ROD END

.ROD END (ALT)

.ROD END (ALT)

ATTACHING PARTS

.BOLT

.WASHER

.NUT

.NUT

FOR NHA)

(v81376)

(w0128)

.CONTROL ROD ASSY

.. RODASSY

..ROD END

. .ROD END (ALT)

. .ROD END (ALT)

. .ROD END (ALT)(WTH'M ON SHANK)

ATTACHING PARTS

. .RIVET (LENGTH TBDATASSY}

..NUT

(v81376)

(w3134)

(vD3279)

(\r/3134)

RF

1

1

1

1

1

1

1

1

1

1

1

2

1

2

2

2

2

2

2

90

100

- ITEM NOT ILLUSTRATED

Fig.5Page 2

Aug 301200332-20-00

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r$urr ArcnArrmusirutuo I PAffS 8AlAl08

FIGURE &ITEM NO.

PART NUMBER NOMENCI.ATURE

12U567

AIRCRAFTEFFECTIVITY

CODE

UNITSPER

ASSY

110

- 120

130

140

150

160

170

180

190

Npw210

;: I

24o I

250 |

zoo I

",1"oI

t300

|

IAN+12AI

l*sozoo-toI

lnnmo-croI

lnr.rsoolrolI

I

Ms20365-428

lAN2+14

lonru*'uMS20364-428

283002-403

390m092312.43

MS27975-3

MS2(X70AD3

AN316.4R

AN2$14

4N96S.10

4N310-3

AN380-2-3

263013{01

2E301$502

AN4H6

l..BoLr| (SUPERSEDED BY |TEM 120)

I

l..aolrl(SUPERSEDES

|TEM 110)

I

l..wAsHERI

l..wAsHERI

..NUT

.. BOLT

..WASHER

. ::'

.CONTROL ROD ASSY

.. RODASSY

. . ROD END

ATTACHING PARTS

. .RrvET (LENGTH TBDATASSY)

..NUT

.. BOLT

..WASHER

..NUT

..COTTER PlN

.BELLCRANK, NOSE DOOR, LH

.BELLCRANK, NOSE DOOR, RH

ATTACHING PARTS

.BOLT

1

1

2

1

1

1

1

1

2

1

2

2

2

2

4

2

2

1

1

2

- ITEM NOT ILLUSTRATED

Fig. 5Page 3

Aug 301200332-20-00

mzr\m?ln.WJfttp /,uasrnrlm

EiNAf.

LFIGURE &ITEM NO.

PART NUMBER NOMENCLATURE

t2u567AIRCRAFT

EFFECTIVITYCODE

UNITSPER

ASSY

q610620

28302$501

MSI 6562-38

.SHAFTASSY

.PIN

2

4

.ITEM NOT ILLUSTRATED

EFFECTIVITY: ALL Fig.5Page 6

Aug 30/200332-20-00

f

Elevator Control

::2r\(*'mrfiA'Vtinn I ulffinnE

s.a.lmaAFrrslrrctn I Pfrlscn ln

t,

,r-r

7Nv

Elevator Control Installation - CockpitFigure 2

FtA.2Page 0

Aug 30/2fi)327-30-00

ffizr\lll]rn.VJintn I fll!,''nnw

ESAE mnAFnruslmrla I P|ns6fittnAIRCRAFT

EFFECTMTYCODE

UNlTSPER

ASSY

. :":- ROD END

.TUBEASSY

ATTACHING PARTS

.BOLT

.BOLT (ALT)

.WASHER(1 BETyI/EEN ROD END & ARM, & 1 UNDER

.NUT

.COTTER PIN

.'::''*

. .ROD END

. .ROD END (ALT)

. .ROD END

..FITTING

..TUBE

..NUT

. :":-'ROD END

.TORQUE TUBE INSTL

..ruBEASSY

...BEARING

...ruBE

..SLEEVE

..ARM

1\|.AS5592

50350S501

NAS464P+14

ttlAs6204-14D

At{s60Ptx16L

MSl782S4

NS2488$134

t{As7HS8

ST4BW

sM4€M5

6G1832

50351G501

50350$5

MS509€

i.lAs56s2

tr!:X)l2

533012-13RE

1R2416

s3(n12-13

533012-15

120

130

140

150

-160

n180

190

2W

210

.ITEM NOT ]LLUSTRATED

Fig.2Page2

Aug 30/200327-30-00