1F-15C-2-12JG-20-1.pdf

TO 1F-15C-2-12JG-20-1

DISTRIBUTION STATEMENT D - Distribution authorized to the Department of Defense and U.S. DoD contractors only (Critical Technology) (1 January 1994).

Other requests shall be referred to AFLCMC/WWQ, 235 Byron Street, Suite 19A, Robins AFB, GA. 31098-1670.

WARNING - This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C., Sec 2751, et seq.) or the Export Administration Act of 1979 (Title 50, U.S.C., App. 2401 et seq.), as amended. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25.

HANDLING AND DESTRUCTION NOTICE - Comply with distribution statement and destroy by any method that will prevent disclosure of contents or reconstruction of the document.

Published Under Authority of the Secretary of the Air Force.

TECHNICAL MANUAL

JOB GUIDE

SERVICING - AIRCRAFT

CLEANING

USAF SERIES

F-15C/D

AIRCRAFT

McDonnell Douglas Corporation

F33657-77-C-0200

FA8530-15-D-0005

15 FEBRUARY 1981 CHANGE 23 - 15 JUNE 2018

BASIC AND ALL UPDATES HAVE BEEN MERGED TO MAKE THIS A COMPLETE PUBLICATION

A Change 23

NOTE: The portion of the text affected by the changes is indicated by a vertical line in the margins of the page. Changes to illustrations are indicated by minia-ture pointing hands. Changes to wiring diagrams are indicated by miniature pointing hands or by shaded areas. A vertical line running the length of a fig-ure in the outer margin of the page indicates that the figure is being added.

Dates of issue for original and changed pages are:

USAF

TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 56, CONSISTING

OF THE FOLLOWING:

LIST OF EFFECTIVE PAGES

INSERT LATEST CHANGED PAGES.

DESTROY SUPERSEDED PAGES.

*Zero in this column indicates an original page.

Page *Change No. No.

Page *Change No. No.

Title A B Added C Blank i ii Blank iii iv v vi 1-1 1-2 1-3 1-4 1-5 1-6 1-7 1-8

Original . . . . . . . . . . . . . . . . . . 0. . . . . . . . . . 15 February 1981 Change . . . . . . . . . . . . . . . . . . . 1. . . . . . . . . . . . . . 15 July 1982 Change . . . . . . . . . . . . . . . . . . . 2. . . . . . . . . . . . . . 15 July 1984 Change . . . . . . . . . . . . . . . . . . . 3. . . . . . . . . . . . . . 1 April 1985 Change . . . . . . . . . . . . . . . . . . . 4. . . . . . . . . . 15 February 1986 Change . . . . . . . . . . . . . . . . . . . 5. . . . . . . . . . 1 November 1986 Change . . . . . . . . . . . . . . . . . . . 6. . . . . . . . . . 1 September 1988 Change . . . . . . . . . . . . . . . . . . . 7. . . . . . . . . . . . . 1 March 1989 Change . . . . . . . . . . . . . . . . . . . 8. . . . . . . . . . 1 November 1989 Change . . . . . . . . . . . . . . . . . . . 9. . . . . . . . . . . . 1 January 1994 Change . . . . . . . . . . . . . . . . . . . 10. . . . . . . . . . . . 1 August 1994 Change . . . . . . . . . . . . . . . . . . . 11. . . . . . . . . 1 November 1995 Change . . . . . . . . . . . . . . . . . . . 12. . . . . . . . . . . 15 August 1996 Change . . . . . . . . . . . . . . . . . . . 13. . . . . . . . . . 1 February 1997 Change . . . . . . . . . . . . . . . . . . . 14. . . . . . . . . . . . . 15 June 1997 Change . . . . . . . . . . . . . . . . . . . 15. . . . . . . . . . . 15 March 1999 Change . . . . . . . . . . . . . . . . . . . 16. . . . . . . . 15 September 1999 Change . . . . . . . . . . . . . . . . . . . 17. . . . . . . . . . . . . 15 May 2000 Change . . . . . . . . . . . . . . . . . . . 18. . . . . . . . . . . . . . 1 May 2004 Change . . . . . . . . . . . . . . . . . . . 19. . . . . . . . 15 November 2005 Change . . . . . . . . . . . . . . . . . . . 20. . . . . . . . . . . . 1 August 2008 Change . . . . . . . . . . . . . . . . . . . 21. . . . . . . . . 15 February 2011 Change . . . . . . . . . . . . . . . . . . . 22. . . . . . . . 15 November 2012 Change . . . . . . . . . . . . . . . . . . . 23. . . . . . . . . . . . . 15 June 2018

Change 23 B/(C blank)

LIST OF EFFECTIVE PAGES

INSERT LATEST CHANGED PAGES.

DESTROY SUPERSEDED PAGES.

*Zero in this column indicates an original page.

Page *Change No. No.

Page *Change No. No.

1-8A - 1-8B 1-9 1-10 - 1-11 1-12 1-13 1-14 1-15 1-16 1-17 1-18 - 1-21 1-22 1-23 1-24 - 1-25 1-26 1-26A - 1-26B 1-27 1-28 1-29 1-30 - 1-31 1-32 - 1-33 1-34 - 1-35 1-36 - 1-37 1-38 - 1-39 1-40 1-41 1-42 Blank

TABLE OF CONTENTS

System/Subsystem/

Function/Paragraph Title Subject Number

INTRODUCTION

Purpose Scope Applicability Notations Illustrations Input Conditions Function/Task Arrangement Follow-on Maintenance Improvement Report Glossary Record of Applicable Time Compliance

Technical Orders

GENERAL MAINTENANCE

Aircraft Washing and Cleaning, Preparation, Washing and Cleaning and Lubrication After Washing. . . . . . . . . . . . . . 12-20-01

Change 21 i/(ii blank)

INTRODUCTION

PURPOSE.

This manual provides step-by-step maintenance information for the F-15C and F-15D aircraft washing and cleaning.

SCOPE.

The procedures in this manual are in a function/task arrangement with the number of each step shown on the illustration to locate the applicable hardware. Normally, illustrations and text are on facing pages; except in operational checkout procedures where a foldout illustration may follow several pages of text.

APPLICABILITY NOTATIONS.

Information and instructions contained in this manual unique to one model are identified as F-15C or F-15D. Data applicable to specific aircraft within a series are identified by USAF serial numbers.

ILLUSTRATIONS.

Illustrations show equipment location for each task. Task step numbers and illustration index numbers are identical.

Switches, controls, and indicators are located on illustrations, but may not be shown in the position required in text.

iii

INPUT CONDITIONS.

The input conditions at the start of each function contain the information required to prepare the aircraft for maintenance and the recommended number of people to complete the function. The required consumable supplies, support equipment, support data, special tools, and safety precautions are also provided.

FUNCTION/TASK ARRANGEMENT.

A function is made up of a task or series of tasks and illustrations which support a system or component. A function supporting a component gives all tasks required to support that component. Typical tasks are removed, installation, adjustment, rigging, operational checkout, cleaning, and so forth. All steps within a task must be done to complete the task. All tasks within a function must be done to complete the function.

Following the procedures in this technical manual is mandatory. However, when doing Red Ball maintenance, only those steps required to complete the task must be done per approved local procedures. Technicians must be sure the intent of the task has been satisfied.

FOLLOW-ON MAINTENANCE.

All steps listed under follow-on maintenance must be done when the tasks required for a given function have been completed.

iv Change 16

IMPROVEMENT REPORTS.

Recommendations for improvements to prescribed requirements and procedures will be submitted by AFTO Form 22, Technical Order System Publication Improvement Report, in accordance with TO 00-5-1. When completing the form, insert the applicable S/S/SN number in block 8 instead of a paragraph number. In block 10 enter the task title before the summary of deficiency. The remainder of the form shall be completed per TO 00-5-1.

GLOSSARY.

Nonstandard abbreviations and symbols are described below.

All abbreviations and symbols used in the maintenance manual set are described in TO 1F-15C-2-OOGV-00-1.

ECS ENVIRONMENTAL CONTROL SYSTEM

LUBRICATE BY HAND

^LUBRICATE WITH OIL CAN

LUBRICATE FLUSH FITTING

WITH GREASE GUN

LUBRICATE BALL FITTING

WITH GREASE GUN

Change 5 v

RECORD OF APPLICABLE TIME COMPLIANCE

TECHNICAL ORDERS.

The record of applicable time compliance technical orders is a list of all TCTO which affect the technical content (text or illustration) of this manual. Only current TCTO are listed. A TCTO is deleted from the list when any of the below occurs:

a. The equipment configuration to which the TCTO is applicable is no longer covered in the manual.

b. The TCTO is rescinded.

c. The TCTO is superseded or replaced.

Record of Applicable Time Compliance Technical Orders

TCTO No. Title TCTO Date

NONE

vi Change 4

Change 23 1-1 12-20-01

AIRCRAFT WASHING AND CLEANING,

PREPARATION, WASHING AND CLEANING AND

LUBRICATION AFTER WASHING.

INPUT CONDITIONS.

Applicability: All

Required Conditions:

• Aircraft safe for maintenance (05-00-01)

• Landing gear forward doors open (05-00-12)

• Arresting hook lowered (32-90-03)

Personnel Recommended: Three

Support Equipment:

• Protector, augmentor (2 req)

• Protector, angle of attack transmitter (2 req)

• Protector, engine air inlet (2 req)

• Protector, pitot static probe (2 req)

• Protector, secondary heat exchanger exhaust

• Plug, secondary heat exchanger inlet (2 req)

• Cover, aft gun bay louver

• Cover, forward gun bay louver

• Trailer, compressed gas air/nitrogen

• Grease gun

• Protector, canopy and windscreen

Support Data:

• 12-10-02

• TO 1-1-691

Supplies (Consumables):

NOMENCLATURE f^A^^^11 QTY

| Barrier, material MIL-B-131, CLASS 1 AR (81349)

I Grease, aircraft MIL-G-81322 AR (81349)

Lubricating oil, W-L-800 AR general purpose (81348)

Nitrogen, technical BB-N-411 TYPE 1 AR

CLASS 1 GRADE A

(81348) or

Nitrogen, technical BB-N-411 TYPE 1 AR (Alternate) CLASS 1 GRADE B

(81348)

Plastic sheet LP378TY4CLIGRB AR

FNSH1-0-0030X

50X96 (81348)

Tape, pressure MIL-T-21595 TYPE 1 AR sensitive (81349)

Tape, pressure A-A-883, TYPE 1, AR sensitive adhesive 1/2 IN

(58536) or

Tape, pressure PPP-T-42TY1-1 AR sensitive (81348)

12-20-01 1-2 Change 17

Personal Safety Equipment:

• Face shield or goggles

• Gloves, protective

• Rain suit (or equivalent)

• Water resistant boots

• Safety harness

Safety Conditions:

WARNING

To prevent injury to personnel, remain clear of MLG forward doors, unless forward doors are open and MLG ground safety pin is installed.

Avoid any skin contact with aircraft grease. Wash hands thoroughly before eating, drinking or smoking. Do not apply to hot surfaces; toxic gases may be released.

Nitrogen is harmful if inhaled. Do not breathe gas. Keep container closed. Use with adequate ventilation.

To prevent injury to personnel, eye protection will be worn when servicing with nitrogen or air.

Lubricating oil may cause eye and skin irritation.

Avoid contact with eyes, skin and clothing. Wash thoroughly after handling.

TO 1F-15C-2-12JG-20-1

Change 18 1-3

PREPARATION.

NOTE

Be sure canopy is closed and locked.

Be sure all doors, covers and fairings are in position with all fasteners installed and latches secured.

Protective plugs, covers and protectors are required to prevent cleaners and water from entering aircraft.

If protective plugs, covers and protectors are not available for all areas of aircraft, use barrier paper to seal aircraft openings.

Pressure sensitive tape or adhesive tape may be used to secure and seal protective plugs, covers and protectors as required.

1. Install protective plugs, covers and protectors on aircraft as listed below:

1.1. Pitot static probes.

1.2. Angle of attack transmitters.

TO 1F-15C-2-12JG-20-1

1-4 Change 17

\ N 1.2. ANGLE OF ATTACK

\ TRANSMITTERS (2)

^l.l. P1TOT STATIC

PROBE (2)

18C-)2JG-20(01-11

Figure 01. Sheet 1

1-5

1.3. Forward gun bay louver.

1.4. Aft gun bay louver.

y^ftft^^^f k CAUTION i

To prevent implosion or explosion of fuel systems, use vented covering, not tape.

1.5. Wing fuel vent masks, (temporary).

1.5A. If installed, pylon fuel vents, (temporary).

1.6. Jet fuel starter ventilation, (temporary).

1.7. Augmentors.

IWWWW^f( CAUTION S tfWWWWW^iW

To prevent corrosion and/or possible failure of landing gear wheel bearings and/or brake assemblies due to contamination by water, degreasers, and oil, entire wheel and tire assembly must be covered.

1.8. MLG tire, wheel and brake assemblies, (temporary).

1.9. NLG tire and wheel assembly, (temporary).

1-6 Change 16 t5. WING FUEL

VENT MASTS (2)

1.6. JET FUEL

STARTER

VENTILATION

1.4. AFT GUN /

BAY LOUVER L-^l

\ f \ // J^ /J--’ 1-7- AUGMENTOR (2)

1.3. FORWARD GUN \ / ><i-C^^- T

BAY LOUVER \ \) .^^’^’f’’-’^/.^^^

\ 1.8. MLG TIRE. WHEEL

\ AND BRAKE

ASSEMBLIES (2)

1.9. NLG TIRE AND

WHEEL ASSEMBLY

1.5A. PYLON FUEL VENTS

W\ MAJOR CHANSE

OCJB12-01-2-17

Figure 01. Sheet 2

Change 14 1-7

1.10. Bulkhead opening, (temporary).

1.11. L/R keel web avionics cooling exits, (temporary).

1.11A. NLG/door selector valve, (temporary).

1-8 Change 16

1.10. BULKHEAD OPENING ^tl<I^^> ^^ ^V

^^^^^^< ^| ^^’ ^^ NLG FORWARD

// ^wir\ \ 1-’11A IIILG/DOOR

^^:^^\ 1.11. KEEL WEB AVIONICS ^V^’f/W^}} COOLING EXIT (L/R) ^ ^’Y

__-J^ 0 0^:’-’ /^ ll-l MAJOR CHANGE NLG WHEELWELL LEFT SIDE <^

9^V \ MAJOR C^NBc ACJO)2-01-Z-t-021

Figure 01. Sheet 2A

Change 16 1-8A

1.12. Engine air inlets.

1.13. Secondary heat exchanger inlets.

1.14. Ram air-fuel pressurization, door 27L

(temporary).

1-8B Change 16

112. ENGINE Alfl \i \

INLETS (2) ~~~~~~n\_______ \ flHF1.13. SECONDARY HEAT ^’ \.r\ EXCHANGER INLETS (2) g \’-i/1 l>f--

^y i^

^ ^--\C_A>

114. RAM AIR-FUEL

PRESSUBIZATION

(DOOR 271.)

VIEW A-A

jrt" MAJOR CHANGE

ACJDU-01-3-021

Figure 01. Sheet 3

Change 16 1-9

1.15. Convergent exhaust nozzle controls, (temporary).

1.16. Engine vent scoops, (temporary).

1.17. AMAD ventilation exhaust, door 87 (temporary).

1.18. Ammo bay vent, door 45 (temporary).

1-10

Figure 01. Sheet 4

1-11

1.19. JFS intake (temporary).

1.20. JFS ventilation (temporary).

1.21. Gas generator fuel drain (temporary).

1.22. JFS exhaust (temporary).

1.23. Augmentor fuel drains (temporary).

1.24. ECS bay vent, door 15 (temporary).

1.25. Left and right ALE-45 chaff/flare dispensers, if

installed (temporary).

1.26. Relay panels in left and right wheelwells

(temporary).

1.27. Regenerative heat exchanger exhaust (temporary).

1.28. First ramp air exit louvers and bleed air exits

(temporary).

1.29. Forward gun port (temporary).

1.30. Windshield, canopy, and windshield anti-ice

nozzle (temporary).

To prevent possible damage to AIM-9 and AIM-120 electrical connectors on LAU-106 and LAU-128 missile launchers, connectors must be sealed to prevent water intrusion.

1.31. LAU-106 launcher electrical connectors

(temporary).

1.32. LAU-128 launcher electrical connectors

(temporary).

TO 1F-15C-2-12JG-20-1

1-12 Change 21

1.19. JFS INTAKE

1ELS

D

1 1.32. LAU-121 ELWELLS

LAUNCI

06 MISSILE

Msl<)

ECS BAY

^15)

1.23. AUGMEN

DRAINS

1.25. ALE-45 CHAFF/FLARE

DISPENSERS

f^ 1.28. BLEED AIR EXIT

F\ A \ /"-II /1-27- ^^E^’VE HEAT

V^^^^ A / EXCHANGER EXHAUST

C___^^. ^ ’^^T^l / ^m- FIRST RAMP hm

^r ^^~~^^ itSafe^ EXIT LOUVER

’^’’^^^^ ^__---^ 1.30. WINDSHIELD.

-’V ’^ ’1^ CANOPY

1.29. FORWARD ^’^GUN PORT \

1.30. WINDSHIELD

ANTI-ICE

NOZZLE

ACJD12-01-5-019

Figure 01. Sheet 5

Change 15 1-13

WASHING AND CLEANING.

WARNING

I To prevent injury to personnel due to slippery surfaces and cleaning solutions, make sure all appropriate safety equipment is worn.

NOTE

Alkaline water base cleaning is the primary method of cleaning exterior finished surfaces, unfinished titanium, gear wells, missile wells, inflight refueling compartment.

Solvent cleaning should be used only when conditions prevent the alkaline water base cleaning method from being used. Refer to

TO 1-1-691.

Before washing, make sure aircraft drain holes are not blocked.

1. Wash aircraft surface. Refer to TO 1-1-691.

i^ CAinTON J

Do not use alkaline cleaner or solvents to clean windshield and canopy transparencies.

2. Remove protective covers installed during preparation in step 1.30. Clean windshield and canopy transparencies (12-10-02).

1-14 Change 14

Figure 01. Sheet 6

1-15

To prevent damage to AIM-120 electrical connectors when electrical power is applied, connectors must be blown dry with low pressure dry nitrogen.

2A. Remove protective covers installed in step 1.31 and blow dry electrical connectors using low pressure nitrogen.

3. If required, solvent clean gun compartment. Refer to

TO 1-1-691.

4. Clean oily and greasy areas of cockpit that are not near the oxygen system or canopy and windshield transparencies. Refer to TO 1-1-691.

5. Vacuum clean cockpit.

6. Remove protective plugs, covers, protectors and masking tape installed during preparation in steps 1 through 1.29.

TO 1F-15C-2-12JG-20-1

1-16 Change 21 fVx \ ./--- y 2A. IAU-106 MISSILE |

J /w^< \ /y IAUNCHERS(4) ’

">^--^^ y4. ICOCKPIT

3. GUN COMPARTMENT

)5C-1ZIG-20-12(01-7)12-CM1

Figure 01. Sheet 7

Change 10 1-17

LUBRICATION AFTER WASHING.

Fuselage Hinged Doors.

NOTE

Make sure fittings are clean before lubrication is done.

Left side shown, right side opposite except as noted.

1. Lubricate fuselage hinged doors as listed below:

1.1. Doors 3L/R.

1.2. Doors 6L/R.

1.3. Doors 10L/R.

1.4. Door 9 (left side only).

1.5. Doors 99L/R.

1-18

-T 1.4, OOOR 9

1.1. DOOM 31./H ((.EFT SIDE ONIY)

^^^^^^^^f \ r \ r

1.2. OOORS6L/R 1.3. DOORS 10UR 4 1.5. DOORS 99L/R

15C-12JG-20(01-81

Figure 01. Sheet 8

1-19

1.6. Doors 104L/R.

1.7. Doors 121L/R.

1.8. Doors 120L/R.

1.9. Doors 88L/R.

1.10. Doors 85L/R.

1-20

1.7. DOORS 121L/RB

1.B. DOORS 104L/R yK\ o^i-S. DOORS 120L/R

TOP VIEW

/’^^sl.ia DOORS 8517RB

1.9. OOOBS 88L/R { /^ / /

---St^^

BOTTOM VIEW ISC^G-MKH-S)

Figure 01. Sheet 9

1-21

Main Landing Gear and Doors.

NOTE

Make sure fittings are clean before lubrication is done.

1. Lubricate items listed below:

NOTE

Left MLG shown, right MLG similar.

1.1. Aft door hinge.

1.2. Aft door drive link.

1.3. Outboard door hinge.

1.4. Outboard door rollers.

1.5. Aft door cam follower.

1-22 Change 17

Figure 01. Sheet 10

Change 19 1-23

1.6. Bungee to collar bushing.

1.7. Retract actuator rod end bushing.

1.8. Retract actuator forward bushing.

1.9. Jury link center bushings.

1.10. Upper drag brace upper bushing.

1.11. Retract actuator wiper.

1.12. Upper jury link to cylinder bushing (2 places).

1.13. Bungee to bellcrank bushing.

1.14. Upper drag brace lower bushing (2 places).

1.15. Lower jury link lower bushing.

1.16. Lower drag brace upper bushing (2 places).

1.17. Lower drag brace lower bushing/swivel crank

assembly.

TO 1F-15C-2-12JG-20-1

1-24 Change 17

Figure 01. Sheet 11

Change 17 1-25

1.18. Swivel link bearing.

1.19. Spindle to swivel link bushing.

1.20. Spindle collar bushing.

NOTE

Cam follower PN 68B411092-101 does not require lubricant (no grease fitting in slot on top of cam follower).

1.21. If applicable, cam follower bearing.

1.22. Upper torque arm to torque collar bushings

(2 places).

1.23. Torque arm apex bolt.

1.24. Lower torque arm to piston assembly bushings

(2 places).

1.25. Strut piston.

TO 1F-15C-2-12JG-20-1

1-26 Change 22

<y< C*^ \ AW. SWIVEL LINK ,= / BEARMG J^* f t22. UPPER TORQUE ARM j49 F / TO TORQUE COLLAR BUSHMQS / / ytH. SPtOLE TO SWIVEL

^- h. / / I-INK BUSHMS99 F

’’^ ^tC-r-C ^/ .^’^SPINOLE COLLAR

123. TORQUE ARM APEX ’f^gq f ^^BOLT *^ ^< ^TT---L ^VSi. STRUT PISTON & i^// ^r 191 cm nujpD

124. LOWER TORQUE ARM TO \(, ^^ i^iBMr --L.

PISTON ASSEMBLY \\ ^^-’^ rw BUSMNGS Jft F ^"’^AY .stf

T MAJOR CHANGE ACJ012-01-11-1-023

Figure 01. Sheet 11A

Change 17 1-26A

1.26. Trunnion support bearing.

1.27. MLG uplatch and door cylinder rod end.

1.28. Strut cylinder bushings.

1.29. Trunnion collar bushing (2 places).

1.30. Trunnion support pin.

1-26B Change 17

Figure 01. Sheet 12

Change 17 1-27

Nose Landing Gear and Doors.

Make sure fittings are clean before lubrication is done.

Lubrication fitting may be either ball type (Z) or flush type (F).

1. Lubricate items listed below:

1.1. NLG door hinge.

NOTE

Cam follower PN 68B411092-101 does not require lubricant (no grease fitting in slot on top of cam follower).

1.2. If applicable, NLG door cam follower.

TO 1F-15C-2-12JG-20-1

1-28 Change 22

Figure 01. Sheet 13

Change 17 1-29

1.3. Upper jury link lower bushings (2 points).

1.4. L/R strut trunnion bushings.

1.5. Retract actuator upper fitting.

1.6. Steering actuator rod end.

1.7. L/R mooring rings.

1.8. Deleted.

1.9. Lower drag brace lower bearing.

1.10. If present, steering support arm.

1.11. Lower drag brace upper bushing (2 places).

1.12. Upper drag brace lower bushing (2 places).

TO 1F-15C-2-12JG-20-1

1-30 Change 22

Figure 01. Sheet 14

Change 22 1-31

1.13. Retract actuator wiper.

1.14. L/R Drag brace support bushings.

1.15. Lower jury link upper bushings.

1.16. Deleted.

1.17. NLG strut piston.

1.18. Nosewheel steering actuator rod.

1.19. Nosewheel steering link rod ends (2 places).

1.20. NLG retract actuator rod end (2 places).

1.21. Upper strut bushing.

1.22. Upper jury link upper bushings (2 places).

TO 1F-15C-2-12JG-20-1

1-32 Change 20

Figure 01. Sheet 15

Change 20 1-33

Movable Flight Control Surfaces.

Left side shown, right side opposite.

1. Lubricate items on aileron and flap as listed below:

1.1. Hinge pin.

1.2. Hinge pin.

1.3. Hinge pin.

TO 1F-15C-2-12JG-20-1

1-34

/’ ^/^^^^^^^---- 1.1. HINGE PIN f ^sS^sy^ -r<^^^^L----1-2- HINGE ’"<

1.3. HINGE PIN ^" .^^.^ ^fv^’ \

16C-12JG-20(0)-)6)

Figure 01. Sheet 16

1-35

Left side shown, right side opposite.

| 2. Lubricate left and right hinge arms.

1-36 Change 3

^’ ^^ ^^ SPEED BRAKE

’^^^^ ’^ ASSEMBLY 1REF)

2. HINGE ARM fF ^ ^’^^^ ^-

ITYPICAL BOTH

HINGE ARMS)

15C-12JG-20(01-17)B

Figure 01. Sheet 17

Change 3 1-37

Left rudder shown, right rudder opposite.

If required, apply steady pressure to rudder surface to expose lubrication points.

3. Lubricate items on rudder as listed below:

3.1. Hinge bearing.

3.2. Hinge bearing.

1-38 Change 12

12. HINGE L / / /

BEARINGf^ 1

15C-12JO-TOIOI-16)

Figure 01. Sheet 18

Change 12 1-39

| Arresting Hook.

1. Lubricate items listed below with lubricating oil:

1.1. Damper piston.

1.2. Bushings.

1.3. Bushings.

1.4. Bushings.

1.5. Rod ends.

1.6. Pivot arm assembly (both sides).

1.7. Bellcrank assembly (both sides).

1.8. Uplatch roller assembly.

FOLLOW-ON MAINTENANCE.

Close landing gear forward doors (05-00-12).

Raise arresting hook (32-90-03).

1 Q Oft ftl A U.S. GOVERNMENT PRINTING OFFICE 00 555-016

1-40 Change 17

1.3. BUSHINGS^, <k

1.2. BUSH INGS ^ V^^^art/7

V ^^^ W^Orf /17. BELLCRANKi^

a. "^^^ ASSEM8LY

1.1. DAMPER W ’^B^^^fc^

^/ ^1.7. BELLCRANK^T*

ROLLER s. // ASSEMBLY ^^s. //

^^,X^:^:=^^::::^ 6 PIVOT ARM "ASSEMBLY ^

DETAIL A-A

|^-| MAJOR CHANGE ,5C-12JG-20-,(0,-19)15-CATI

Figure 01. Sheet 19 ri- U.S. GOVERNMENT PRINTING OFFICE 99 755-014 f f\ Oft f\t

Change 12 1-41/(1-42 blank)