Attachment Four_TO 1C1356WC3_Scheduled Wash Inspection Workcards.pdf

ONE SET

TO 1C-135-6WC-3

SCHEDULED WASH INSPECTION WORKCARDS

USAF MODEL (ALL 135 AIRCRAFT)

DSS, LLC.

FA8124-21-F-0018

PREPARED BY AFLCMC/WLTMA KC-135 WEAPON SYSTEM PROGRAM OFFICE

THIS TO SUPERSEDES TO 1C-135-6WC-3, DATED 1 MAY 2021, AND ANY CHANGES INCLUDING SUPPLEMENTS

DISCLOSURE NOTICE - This information is furnished upon the condition that it will not be released to another nation without the specific authority of the department of the air force of the united states, that it will be used for military purposes only, that individual or corporate rights originating in the information, whether patented or not, will be respected, that the recipient will report promptly to the united states any known or suspected compromise, and that the information will be provided substantially the same degree of security afforded it by the department of defense of the united states. Also, regardless of any other markings on the document, it will not be downgraded or declassified without written approval of the originating united states agency.

DISTRIBUTION STATEMENT D - Distribution authorized to the Department of Defense and U.S. DoD Contractors only, Administrative or Operational Use, 15 March 2019.

Other requests shall be referred to AFLCMC/WLTMA, Tinker AFB, OK 73145-3019.

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, as amended (Title 50, U.S.C. App. 2401 et. seq.). Violations of these export-control laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25.

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15 JULY 2021

Published under authority of the Secretary of the Air Force.

LIST OF EFFECTIVE CARDS INSERT LATEST CHANGE CARD. DESTROY SUPERSEDED CARDS.

NOTE The portions of the text affected by the changes are indicated by a vertical line in the outer margin of the card. Changes to illustrations are indicated by shaded or screened areas, or by miniature pointing hands.

Dates of issue for original and changed cards are:

Original . . . . . . . . . . 0 ......................................... 15 July 2021

The total number of cards in this publication is 87, consisting of the following:

Card *Change Card *Change Card *Change No. No. No. No. No. No.

Title A 1 - 5 1-001 2-001 - 2-001 3-001 - 3-001 4-001 - 4-006 5-001 - 5-041 6-001 - 6-008 7-001 - 7-005

* Zero in this column indicates an original card.

USAF A

PUBLICATION NUMBER

INSPECTION REQUIREMENTS

INTRODUCTION

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NOTE

FOR THE PURPOSE OF THIS TECHNICAL ORDER, THE PHRASES “DEPLOYED AREA” AND “DEPLOYING” HAVE THE

SAME MEANINGS AS “TDY LOCATION” AND “GOING TDY”.

A. THESE CARDS PROVIDE MANDATORY WASH, CLEAR WATER RINSE, LUBRICATION, AND MINOR AND MAJOR CRITICAL CORROSION INSPECTION (CCI) REQUIREMENTS APPLICABLE TO ALL -135 AIRCRAFT. THESE WORKCARD REQUIREMENTS

ARE DIVIDED INTO SEVEN PARTS AS FOLLOWS:

(1) PART I - SAFETY PRECAUTIONS

(2) PART II - GENERAL INSTRUCTIONS

(3) PART III - PREPARATION

(4) PART IV - WASH PROCEDURES

(5) PART V - POST WASH REQUIREMENTS

(6) PART VI - CRITICAL CORROSION INSPECTION REQUIREMENTS

(7) PART VII - CLEAR WATER RINSE REQUIREMENTS AND PROCEDURES

B. DUE TO THE CRITICAL LIFE LIMITING IMPACT OF CORROSION, THE AIRCRAFT WILL BE WASHED ON SCHEDULE OR EAR-

LIER.

(1) AIRCRAFT WASH SCHEDULING WILL BE DETERMINED BY THE AIRCRAFT’S HOME STATION CORROSION ZONE PER TO 1-1-691.

(2) AIRCRAFT WILL BE WASHED USING PROCEDURES PER TO 1-1-691.

(3) AN AIRCRAFT WASH AND LUBRICATION MUST ALWAYS BE PERFORMED PRIOR TO, AND IN CONJUNCTION WITH, A

PERIODIC INSPECTION PER TO 1C-135-6WC-2.

INSPECTION REQUIREMENTS

INTRODUCTION

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C. FOR FLEXIBILITY DUE TO UNFORSEEN CIRCUMSTANCES, AIRCRAFT ARE PERMITTED TO OVERFLY THE WASH DUE DATE

BY 8 DAYS IN ALL CORROSION ZONES.

(1) EXTENSION OF THE WASH FOR PERIODS GREATER THAN 8 DAYS WILL REQUIRE MAJCOM APPROVAL.

(2) EXTENDING THE AIRCRAFT WASH PAST THE WASH DUE DATE SHALL ONLY BE ALLOWED IF CIRCUMSTANCES ARE BEYOND THE UNIT’S CONTROL. WHEN CIRCUMSTANCES REQUIRING EXTENSION OF THE WASH ARE RESOLVED, THE

AIRCRAFT SHALL BE WASHED AS SOON AS OPERATIONALLY AND LOGISTICALLY POSSIBLE.

D. AIRCRAFT FORMS DOCUMENTATION REQUIREMENTS:

(1) WHEN A WASH BECOMES DUE AND IS NOT ACCOMPLISHED, A RED DASH (-) WILL BE ENTERED IN THE AFTO FORM

781A (DO NOT DEFER TO THE 781K) TO SHOW THE WASH IS OVERDUE.

(2) WHEN THE WASH BECOMES OVERDUE (BEYOND 8 DAYS) PAST THE WASH DUE DATE OR BEYOND THE MAJCOM APPROVED WASH DUE DATE, A RED X SHALL BE ENTERED IN THE AFTO FORM 781A TO SHOW THE AIRCRAFT IS

GROUNDED UNTIL THE WASH IS ACCOMPLISHED.

E. AIRCRAFT WILL BE CLEAR WATER RINSED PER THE DIRECTIONS LISTED IN PART VII.

F. AIRCRAFT SHOULD NOT ASSUME ALERT WITH LESS THAN 30 DAYS REMAINING UNTIL WASH DUE DATE. IF THE WASH BECOMES DUE WHILE THE AIRCRAFT IS ON ALERT IT MAY BE EXTENDED TO COINCIDE WITH THE ALERT CYCLE AND

MUST BE WASHED WITHIN 8 DAYS AFTER ALERT.

G. IF THE AIRCRAFT EXCEEDS THE WASH DUE DATE BY MORE THAN 8 DAYS, ENTER A RED X IN FORM 781 AND GROUND THE AIRCRAFT UNTIL WASHED. MAJCOMS MAY WAIVE THE GROUNDING REQUIREMENT DURING CONTINGENCY, WAR-

TIME SITUATIONS OR SPECIAL CIRCUMSTANCES.

H. (F108) AIRCRAFT STATIONED AT LOCATIONS IDENTIFIED AS A SEVERE CORROSION ZONE PER TO 1-1-691, WASH ENGINES

PER TO 2J-F108-2-1 EVERY 90 DAYS.

INSPECTION REQUIREMENTS

INTRODUCTION

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I. AIRCRAFT DEPLOYING TO A LOCATION IN A DIFFERENT WASH INTERVAL/CORROSION ZONE THAN THE HOME STATION WILL BE WASHED WITHIN 5 DAYS PRIOR TO DEPARTURE, THEN WILL FALL INTO THE WASH INTERVALS OF THE DEPLOYED

LOCATION. AIRCRAFT NOT WASHED WITHIN THE 5 DAY PRE-DEPLOYMENT WINDOW WILL:

(1) SHORTER TO LONGER INTERVAL - REMAIN ON THE HOME STATION WASH CYCLE UNTIL WASH IS DUE.

(2) LONGER TO SHORTER INTERVAL - WILL ASSUME THE DEPLOYED LOCATION WASH CYCLE AFTER 20 DAYS.

J. THE MINOR CRITICAL CORROSION INSPECTION WILL BE ACCOMPLISHED EVERY 180 DAYS IN CONJUNCTION WITH AN AIRCRAFT WASH. FOR FLEXIBILITY DUE TO UNFORSEEN CIRCUMSTANCES, AIRCRAFT ARE PERMITTED TO OVERFLY THE

MINOR CCI DUE DATE 8 DAYS TO STAY ALIGNED WITH THE WASH REQUIREMENT.

K. THE MAJOR CRITICAL CORROSION INSPECTION WILL BE ACCOMPLISHED IN CONJUNCTION WITH THE PERIODIC INSPEC-

TION.

(1) TC-135 AIRCRAFT WILL COMPLETE A MAJOR CRITICAL CORROSION INSPECTION EVERY 12 MONTHS.

(2) AIRCRAFT ASSIGNED TO SEVERE CORROSION ZONES WILL COMPLETE A MAJOR CRITICAL CORROSION INSPECTION

EVERY 12 MONTHS.

L. AIRCRAFT RETURNING FROM A DEPLOYMENT WILL CONVERT TO THE HOME STATION WASH INTERVAL IMMEDIATELY UPON ARRIVAL AT THE HOME STATION. AIRCRAFTS NEW WASH DUE DATE WILL EITHER BE OLD DEPLOYED OR NEW

HOME STATION WASH DUE DATE, WHICHEVER WOULD OCCUR FIRST.

M. AIRCRAFT DEPLOYED TO A SOUTHWEST ASIA ENVIRONMENT FOR 20 DAYS OR MORE WILL PERFORM POST DEPLOY-

MENT TASK NLT 30 DAYS AFTER RETURN TO HOME STATION IAW TO 1-1-691 CHAPTER 9.

N. THE WORK CARDS CONTAIN REQUIREMENTS APPLICABLE TO EQUIPMENT THAT MAY NOT BE INSTALLED ON EVERY MODEL OF C/KC-135 AIRCRAFT. WHEN THIS SITUATION IS ENCOUNTERED, THOSE REQUIREMENTS WHICH DO NOT APPLY

SHOULD BE DISREGARDED.

INSPECTION REQUIREMENTS

INTRODUCTION

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A. AGING AIRCRAFT CONCERNS PREVENT ADDITIONS OR DELETIONS TO THESE REQUIREMENTS BY LOCAL OPERATING

ACTIVITIES. ALL REQUESTS FOR CHANGES WILL BE MADE THROUGH COMMAND CHANNELS.

B. THE LUBRICATION CARDS CONTAINED WITHIN THIS DECK MUST BE ACCOMPLISHED EVERY WASH, INCLUDING WASHES DONE IN CONJUNCTION WITH THE AIRCRAFT PERIODIC (PE) INSPECTION WORKCARDS, TO ENSURE LUBRICATION RE-

QUIREMENTS ARE MET AFTER A COMPLETE WASH HAS BEEN ACCOMPLISHED.

(1) UNLESS OTHERWISE NOTED, GREASE ALL LUBRICATION FITTINGS UNTIL GREASE EXTRUDES FROM FITTINGS AND

JOINTS (EXCESS LUBE WILL BE CLEANED OFF).

(2) N/A

C. IF MAJCOM OR WKDA WASH WAIVERS HAVE BEEN ISSUED DUE TO CONTINGENCY OPERATIONS, THE POST WASH LUBRI- CATION WORKCARDS SHALL BE ACCOMPLISHED EVERY 60 DAYS UNTIL THE AIRCRAFT IS BACK ON ITS HOME STATION

SCHEDULED WASH CYCLE.

D. THE USE OF THE NORDIC DINO 11 OR 777 MECHANICAL CLEANING DEVICE IS AUTHORIZED PROVIDED THE BRUSHES ARE CYLINDRICAL 25 CM LONG, 1.0 MM THICK CORDS MADE OF POLYETHYLENE FIBERS TYPE PEX 1.0. EACH CORD MUST BE CRUSHED AT ITS EXTREMES SO THE INDIVIDUAL FIBERS ARE FREE. ANY OTHER MECHANICAL DEVICE MUST BE AP-

PROVED BY WKDA.

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PART I

GENERAL SAFETY PRECAUTIONS

1. PERSONNEL SHALL BECOME THOROUGHLY FAMILIAR WITH GENERAL SAFETY PRECAUTIONS,

EMERGENCY AND MAINTENANCE MEASURES PER TO 1-1-691 AND TO 1C-135-3-1.

2. PROTECTIVE CLOTHING AND EQUIPMENT, SUCH AS RUBBER GLOVES, FACE AND EYE

SHIELDS, RESPIRATORY EQUIPMENT, APRONS, BOOTS, ETC., MUST BE USED TO PROVIDE

ADEQUATE SAFETY PROTECTION FOR PERSONNEL.

3. INSTALL ALL NECESSARY GROUND SAFETY LOCKS AND PINS PER 2-2 SERIES TECHNICAL

ORDERS TO PREVENT ACCIDENTAL MOVEMENT OF VARIOUS COMPONENTS DURING GROUND

MAINTENANCE.

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PART II

GENERAL INSTRUCTIONS

1. DETERMINE EXTERIOR AND INTERIOR FINISHES, THE LOCATION OF HONEYCOMB AND GLASS

FABRIC PANELS, AND SKIN MATERIALS OF AREAS TO BE WASHED OR CLEANED FROM TO

1C-135-3-1.

DO NOT EXPERIMENT WITH OR USE NON-QUALIFIED PRODUCTS. SEVERE COR-

ROSION OR HYDROGEN EMBRITTLEMENT MAY RESULT.

2. SELECT APPROPRIATE CLEANING MATERIALS AND PROCEDURES FROM TO 1-1-691 OR TO

1C-135-3-1. USE ONLY CLEANERS LISTED IN THESE TECHNICAL ORDERS.

A. IN LOCATIONS WHERE USE OF STANDARD ALKALINE CLEANERS HAS BEEN PROHIBITED,

USE OF MIL-C-87937 QUALIFIED PRODUCTS IS AUTHORIZED.

3. USE OF LIVE STEAM FOR CLEANING -135 AIRCRAFT IS NOT ALLOWED. USE OF LIVE STEAM

WILL DAMAGE OR REMOVE MOST ORGANIC FINISHES AND IN CERTAIN INSTANCES WILL

CAUSE DAMAGE TO GLASS FABRIC LAMINATES, RUBBER COMPOUNDS, AND PLASTICS.

A. USE OF HEATED ALKALINE CLEANERS PER TO 1-1-691 IS RECOMMENDED FOR REMOVING

HEAVY SOILS ON METAL SURFACES.

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4. PRIOR TO THE PE WHEN THE LANDING GEAR IS WASHED, IT WILL BE HAND WASHED AND

RINSED FIRST BEFORE PROCEEDING WITH THE AIRCRAFT WASH.

A. DO NOT USE CLEANERS ON CARBON BRAKES OR WHEELS. CLEANERS CONTACTING

CARBON DISKS WILL ABSORB INTO BRAKE DISC CAUSING DISK AND BRAKE MALFUNC-

TION.

B. RINSE LANDING GEAR WITH LOW PRESSURE WATER ONLY. LOW PRESSURE WATER IS

DEFINED AS THE UNRESTRICTED PRESSURE OF WATER THAT COMES OUT OF A NORMAL

GARDEN HOSE.

C. LOW PRESSURE WATER AND A CLEAN RAG WILL BE USED TO WIPE WHEELS AFTER LAND-

ING GEAR WASH IS COMPLETE.

D. ONCE LANDING GEAR WASH IS COMPLETE, INSTALL NOSE AND MAIN LANDING GEAR

WHEEL COVERS. LEFT AND RIGHT MAIN LANDING GEAR COVERS SHALL REMAIN IN-

STALLED UNTIL AIRCRAFT IS DRIP-DRY, AND FLAPS HAVE BEEN RAISED AND COMPLETELY

DRAINED OF WATER.

5. DURING WASHING AND/OR HAND CLEANING:

A. DIRECT SPRAY NOZZLE OF PRESSURIZED SPRAY EQUIPMENT AT AN ANGLE OF 45 DE-

GREES TO THE SURFACE BEING WASHED.

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• DO NOT DIRECT SPRAY FROM HIGH PRESSURE EQUIPMENT ON GLASS FABRIC

PATCHES ON HONEYCOMB PANELS, OR INTO OPENINGS SUCH AS RAM AIR-

SCOOPS, LANDING GEAR OR ON ELECTRONIC EQUIPMENT, ETC.

• DO NOT USE SPRAY WASH EQUIPMENT WITH PRESSURE HIGHER THAN ALLOWED

BY TO 1-1-691. PRESSURE HIGHER THAN 175 PSI CAN DAMAGE THIN FUSELAGE

SKINS AND SPOTWELDED STRUCTURE. HIGHER PRESSURE ALSO REMOVES PRO-

TECTIVE LUBRICANTS AND FINISHES.

• DO NOT WASH AFT EXTERIOR FUSELAGE ON OC-135B AIRCRAFT WITH CAMERA

WINDOW COVERS REMOVED FROM OPTICAL GLASS.

• IF HIGH PRESSURE HOT WATER WASH EQUIPMENT IS USED, DO NOT EXCEED

PRESSURE OR TEMPERATURE LISTED IN TO 1-1-691.

B. N/A

6. REMOVE LOOSE DIRT AND FOREIGN MATERIALS FROM INTERIOR COMPARTMENTS, FLAP

WELLS, WING TRAILING EDGE SHELF, WHEEL WELLS, ETC. WITH VACUUM CLEANER BRUSH,

OR OIL-FREE CLOTH PRIOR TO STARTING WASHING OR HAND-CLEANING PROCEDURE.

7. AFTER WASHING AND/OR HAND CLEANING:

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A. REMOVE ALL CLEANING COMPOUNDS AND MATERIALS FROM AIRCRAFT AND EQUIPMENT.

FAILURE TO REMOVE SUCH RESIDUAL MATERIALS WILL CREATE ADDITIONAL CORRO-

SION PROBLEMS.

B. AFTER COMPLETION OF CLEANING AND RINSING CHECK THAT ALL CONFINED AREAS

THAT WILL NOT DRAIN SUCH AS CREVICES, JOINTS, AREAS UNDER AFT FUSELAGE WALK-

WAYS ETC ARE DRY AND FREE OF RINSING MATERIALS. SUCH AREAS CONTAINING RINSE

MATERIALS SHALL BE SPONGED OR WIPED DRY. CARE SHALL BE EXERCISED TO ENSURE

THAT MOISTURE SENSITIVE EQUIPMENT SUCH AS EXPOSED ELECTRICAL OR ELEC-

TRONIC COMPONENTS ARE DRY PRIOR TO APPLICATION OF POWER TO THE AFFECTED

SYSTEM. WARM AIR MAY BE USED TO DRY AREAS THAT ARE DIFFICULT TO REACH.

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• WASH AIRCRAFT WHEN SKIN SURFACE IS COOL. A HOT SURFACE WILL EVAPO-

RATE THE CLEANER AND LEAVE A CORROSIVE RESIDUE BEFORE RINSING CAN BE

ACCOMPLISHED.

• DURING NEAR FREEZING AND BELOW TEMPERATURES, ENSURE AIRCRAFT SKIN

IS ALLOWED SUFFICIENT TIME TO WARM PRIOR TO APPLYING WATER OR CLEANER

TO AIRCRAFT. IN EXTREME CASES, WINGS MAY REQUIRE AN EXCESS OF 12 HOURS

TO WARM.

NOTE

USE OF HIGH PRESSURE HOT WATER WASH (HPHWW) EQUIPMENT IAW TO 1-1-

691 IS RECOMMENDED. WHEN HPHWW IS USED, THE AIRCRAFT MUST STILL BE

SCRUBBED TO ADEQUATELY REMOVE CORROSIVE CONTAMINANTS.

8. ALKALINE WATERBASE CLEANER: CLEANERS SPECIFIED IN THIS PROCEDURE MAY BE USED

SAFELY ON ALL AIRCRAFT SURFACES IF THEY ARE NOT ALLOWED TO DRY ON PLASTICS,

PLATEGLASS, OR PAINTED SURFACES. PLASTIC SURFACES ARE NOT DAMAGED BY LIMITED

CONTACT WITH THE CLEANING SOLUTIONS; HOWEVER, MASKING OF ALL PLASTIC AREAS

PRIOR TO CLEANING GREATLY REDUCES THE POSSIBILITY OF DAMAGE. CLEANING SOLU-

TION MAY BE APPLIED BY BRUSH OR SPRAY. IF SPRAY EQUIPMENT IS AVAILABLE, SPRAY THE

SOLUTION ON THE AIRCRAFT THROUGH PETROLEUM-RESISTANT LINES AT APPROXIMATELY

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70 PSI. A COARSE SPRAY IS DESIRED SINCE HIGH ATOMIZATION REDUCES EFFECTIVENESS,

INCREASES HEALTH HAZARDS, AND WASTES MATERIAL.

9. PREPARE CLEANING SOLUTION IAW TO 1-1-691.

10. TO WASH AIRCRAFT FOLLOW PROCEDURES AS OUTLINED IN PART IV.

11. APPLY CLEANING MIXTURE UNTIL AREA TO BE CLEANED IS COMPLETELY COVERED. BEGIN

CLEANING AT THE LOWEST SURFACE ON AIRCRAFT. IF SOIL DEPOSITS ARE HEAVY, AGITATE

THE COMPOUND WITH A NON-METALLIC BRUSH.

NOTE

DO NOT ALLOW CLEANER TO DRY BEFORE RINSING. THROUGHLY FLUSH ALL AIR-

FRAME AREAS CONTACTED BY THE CLEANER. FOR SMALL AREAS REMOVE

CLEANING COMPOUND WITH WATER OR WET RAGS.

12. AFTER A 15-MINUTE SOAK PERIOD (LESS IF SCRUBBING IS USED), PRESSURE-RINSE USING

WARM (50 DEGREES C - 120 DEGREES F MAXIMUM) WATER IF AVAILABLE.

13. REPEAT STEPS 4 AND 5 UNTIL AIRCRAFT IS CLEAN.

A. DO NOT PERMIT CLEANING COMPOUNDS OR SOLVENTS TO CONTACT CONTROL CABLES,

SEALED BEARINGS, EXPOSED ELECTRICAL COMPONENTS AND CONNECTORS, OR TO

ENTER CONFINED AREAS WHICH CANNOT BE DRAINED.

B. DO NOT PERMIT HYDROCARBON SOLVENTS OR CLEANING COMPOUNDS TO CONTACT

THE AILERON, RUDDER OR ELEVATOR BALANCE SEALS.

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PART III

PREPARATION

1. AFTO FORM 781 SERIES FORMS CHECKED.

2. FIRE EXTINGUSHER PROVIDED.

3. ENSURE WHEELS ARE CHOCKED.

4. ENSURE AIRCRAFT IS STATICALLY GROUNDED PER 2-2 SERIES TECHNICAL ORDERS.

5. ENSURE REFUELING VALVE IS POSITIONED TO REFUEL.

6. ENSURE MANIFOLD VALVES SWITCH IS IN WING REFUEL POSITION.

A. ON ARR/IFR PANEL PLACE MASTER REFUEL SWITCH TO ON.

B. PLACE MANIFOLD VALVE/MANF VALVES TO WING REFUEL/REFUEL.

C. ON ARR/IFR PANEL PLACE MASTER REFUEL SWITCH TO OFF.

@ 7. APPLY EXTERNAL POWER AND ACCOMPLISH THE FOLLOWING:

A. LOWER WING FLAPS PER 2-2 SERIES TECHNICAL ORDERS.

B. POSITION HORIZONTAL STABILIZER TO ″2.5 UNITS AIRPLANE NOSE DOWN″.

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C. LOWER BOOM AND INSTALL BOOM SLING PER 2-6 SERIES TECHNICAL ORDERS.

D. ENSURE MLG WHEEL WELL DOORS ARE CLOSED. DOORS WILL REMAIN CLOSED UNTIL

MLG HAS BEEN WASHED AND PROTECTIVE COVERS HAVE BEEN INSTALLED.

8. DISCONNECT EXTERNAL POWER.

9. DISCONNECT MAIN BATTERY PER 2-10 SERIES TECHNICAL ORDERS.

10. FOR KC-135R/T AND WC-135R AIRCRAFT, DISCONNECT APU BATTERY PER 2-16 SERIES TECH-

NICAL ORDERS.

11. FOR RC/TC-135 AIRCRAFT, DISCONNECT JFS BATTERY PER 2-10 SERIES TECHNICAL ORDERS.

12. FOR NC/WC-135W AIRCRAFT, DISCONNECT THE AUXILIARY BATTERY PER 2-10 SERIES TECH-

NICAL ORDERS.

13. FOR NC/RC/TC-135 AIRCRAFT, DISCONNECT THE INS BATTERY PER DMM-BS135.

14. REMOVE OR OPEN ALL GALLEY EQUIPMENT (DRAWERS, COFFEE MAKERS, OVENS, WATER

BOTTLES, ETC) AS APPLICABLE.

15. LOWER COVE LIP DOORS.

16. RAISE ALL SPOILERS, AND INSTALL LOCKS.

17. ENSURE ALL FUSELAGE WATER DRAIN SCREWS ARE CLOSED.

18. OPEN NOSE WHEEL WELL DOORS AND DISCONNECT LINKAGE.

19. INSTALL PROTECTIVE PLUGS, COVERS, AND SHIELDS IN LOUVERS, AIRSCOOPS, AND EN-

GINES PER 2-2 SERIES TECHNICAL ORDERS.

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• AIRCRAFT WITH AN/AS1-141(V) INTEGRATED DUAL FLIGHT DIRECTOR SYSTEM (RO-

TATION-GO-AROUND) SHALL HAVE BOTH ANGLE-OF-ATTACK PROBES MASKED

FROM TIP TO FUSELAGE SURFACE TO PREVENT CLEANING AGENTS FROM ENTER-

ING AND DAMAGING THE ELECTRO-MECHANICAL PARTS.

• MAKE SURE THAT STATIC VENT/OPENINGS/PORTS ARE NOT FOULED BY TAPE AD-

HESIVE TRANSFER. COVER STATIC VENT/OPENINGS/PORTS BY CUTTING BARRIER

MATERIAL (MIL-PRF-131, CLASS 1) TO THE SAME SIZE AS THE VENT/OPENING/

PORTS, AND HOLD IN PLACE WITH PRESERVATION TAPE (AMS-T-22085, TYPE II) OR

MASKING TAPE (AMS-T-21595, TYPE III).

20. SEAL PITOT STATIC OPENINGS, ANGLE-OF ATTACK PROBES, AND PITOT TUBES.

NOTE

ONCE LANDING GEAR WASH IS COMPLETE INSTALL NOSE WHEEL COVERS, AND

MAIN WHEEL COVERS OR ONE-PIECE LANDING GEAR COVERS. COVERS SHALL

REMAIN INSTALLED UNTIL AIRCRAFT IS DRIP-DRY, AND FLAPS HAVE BEEN RAISED

AND COMPLETELY DRAINED.

21. IF AIRCRAFT IS BEING WASHED FOR PERIODIC (PE) INSPECTION, DO NOT INSTALL LANDING

GEAR WHEEL COVERS OR ONE-PIECE COVERS AT THIS TIME. LANDING GEAR COVERS WILL

BE INSTALLED AFTER LANDING GEAR IS WASHED.

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• WATER INFILTRATION INTO LANDING GEAR TRUCKS, WHEELS, AND BEARINGS

WASHES AWAY PROTECTIVE GREASES AND LUBRICANTS AND CAN ACCELERATE

CORROSION. FAILURE OF LANDING GEAR MAY RESULT IN CATASTROPHIC DAM-

AGE.

• DO NOT USE PRESSURIZED CLEANERS TO WASH THE NOSE OR MAIN LANDING

GEAR ASSEMBLIES.

WATER INFILTRATION INTO LANDING GEAR CARBON BRAKES CAN CAUSE WATER

SATURATION OF THE BRAKE ASSEMBLY HEAT-SINK. WET BRAKES CAN FREEZE

TOGETHER WHEN SUBJECTED TO FREEZING TEMPERATURES.

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NOTE

• THE ONE-PIECE LANDING GEAR COVER (PN 39261D0311005-1) MAY BE USED IN

LIEU OF INDIVIDUAL WHEEL COVERS (PN 39261D0311003-1).

• AIRCRAFT WASHES THAT ARE PREPARATORY FOR PERIODIC (PE) INSPECTION

WILL HAVE PROTECTIVE WHEEL COVERS INSTALLED AFTER LANDING GEAR IS

HAND WASHED.

22. FOR WASHES NOT PREPARATORY FOR PERIODIC (PE) INSPECTION, INSTALL PROTECTIVE

COVERS ON NOSE WHEELS (PN 39261D0311001-1) AND ON MAIN WHEELS (PN 39261D0311003-

1), AND MASKING (AS NEEDED) ON LANDING GEAR TRUCKS.

• DO NOT USE ABRASIVE PADS TO WASH RADOMES.

• WASH RADOMES WITH MILD SOAP AND SOFT SPONGES/TOWELS ONLY.

23. MASK NOSE RADOME (BS 178) AND RADOME LOWER FUSELAGE (RC-135) (BS 1200 - 1400) TO

PREVENT WASHING SOLUTION INTRUSION INTO RADOME.

24. TAPE APU INLET AND EXHAUST DOORS LOCATED ON EXTERNAL FUSELAGE SKIN.

CARD NO.

3-001

WORK AREA TYPE MECH RQR

APG

MECH NO. CARD TIME PUBLICATION NUMBER

WORK

AREA

WORK UNIT CODE PREPARATION INSPECTION

REQUIREMENTS

ELECTRICAL POWER

ON/OFF

SERVICE FIGURE CARD NO.

3-001 SYS SUB

25. MASK THE EXTRUDING PANEL IN EACH CHEEK FAIRING TO PREVENT WASHING SOLUTION

FROM CONTACTING THE PANEL (AS APPLICABLE).

26. TAPE CARGO DOOR, OVERWING HATCHES, AND AFT HATCH TO PREVENT WATER INTRUSION.

27. OPEN F108 ENGINE COWLING.

RC-135

28. COVER ITEMS IDENTIFIED IN DMM-BS135 USING TAPE (AMS-T-22085 TYPE II PRESERVATION

TAPE FOR MASKING) AND BARRIER MATERIAL (MIL-PRF-131, CLASS 1).

WC-135

29. COVER INTAKE AND EXHAUST ON BOTH, LH/RH PSA (PARTICULATE SAMPLER ASSEMBLY)

AIRFOIL.

KC-135

FAILURE TO REMOVE THE POD AND POD ADAPTER PLATE MAY RESULT IN SIGNIFI-

CANT DAMAGE TO THE SYSTEM.

30. (AFTER TCTO 1898) ENSURE LAIRCM GEN 3 POD AND POD ADAPTER PLATE HAVE BEEN RE-

MOVED AND AIRCRAFT INTERFACE CLOSEOUT COVER IS INSTALLED PRIOR TO WASH.

4-001

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WORK UNIT CODE WA H PROCEDURES INSPECTION

REQUIREMENTS

ELECTRICAL POWER SERVICE FIGURE CARD NO.

4-001 SYS SUB

PART IV

WASH PROCEDURES

LANDING GEAR (STEP 1)

• CLEANERS CANNOT BE USED ON CARBON BRAKES. CLEANERS CONTACTING

CARBON DISKS WILL ABSORB INTO DISK CAUSING DAMAGE TO THE DISK MATE-

RIAL AND THE BRAKE TO MALFUNCTION IN SERVICE.

• DO NOT SPRAY CLEANING SOLUTIONS DIRECTLY ON LANDING GEAR. USE LOW

PRESSURE WATER ONLY TO RINSE LANDING GEAR. LOW PRESSURE WATER IS

DEFINED AS THE UNRESTRICTED PRESSURE OF WATER WHICH COMES OUT OF A

NORMAL GARDEN WATER HOSE.

• LANDING GEAR WILL BE HAND-WASH ONLY.

• PROTECTIVE COVERS PREVENT MOISTURE SATURATION OF CARBON BRAKE AS-

SEMBLIES. SATURATED CARBON BRAKE ASSEMBLIES EXPOSED TO FREEZING

TEMPERATURES MAY BECOME FROZEN AND CAN RESULT IN TIRE FAILURE DUR-

ING AIRCRAFT LANDING.

NOTE

CARD NO.

4-001

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WORK UNIT CODE WASH PROCEDURES INSPECTION

REQUIREMENTS

ELECTRICAL POWER SERVICE FIGURE CARD NO.

4-001 SYS SUB

• IF AIRCRAFT WASH IS NOT PREPARATORY TO PERIODIC (PE) INSPECTION, REMOVE

AND REINSTALL MAIN AND NOSE WHEEL PROTECTIVE COVERS AS LANDING GEAR

WASH PROGRESSES.

• IF AIRCRAFT WASH IS PREPARATORY FOR PERIODIC (PE) INSPECTION, INSTALL

MAIN AND NOSE WHEEL PROTECTIVE COVERS AFTER LANDING GEAR IS WASHED.

1. USING HAND-WASH METHOD, REMOVE ACCUMULATION OF DIRT, GREASE, AND HYDRAULIC

FLUID FROM THE MAIN AND NOSE LANDING GEAR.

2. USING LOW PRESSURE WATER AND A RAG, RINSE AND WIPE WHEELS AFTER WASH IS COM-

PLETE.

NOTE

THE ONE-PIECE LANDING GEAR COVER (PN 39261D0311005-1) MAY BE USED IN

LIEU OF INDIVIDUAL WHEEL COVERS (PN 39261D0311003-1).

3. INSTALL PROTECTIVE COVERS ON NOSE WHEELS (PN 39261D0311001-1) AND ON MAIN

WHEELS (PN 39261D0311003-1), AND MASKING (AS NEEDED) ON LANDING GEAR TRUCKS.

4. WASH EXTERIOR OF MAIN LANDING GEAR DOORS. WHEN DOOR WASH IS COMPLETE, OPEN

MAIN WHEEL WELL DOORS AND INSTALL LOCKS PER -2-2 SERIES TECHNICAL ORDERS.

4-002

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REQUIREMENTS

ELECTRICAL POWER SERVICE FIGURE CARD NO.

4-002 SYS SUB

PART IV

WASH PROCEDURES

ENGINES (STEP 2)

NOTE

• PROTECT ENGINE AND ACCESSORIES FROM ENTRY OF WATER OR CLEANING SO-

LUTION BY PLUGGING OR MASKING AIR INTAKE, EXHAUST TAIL PIPES, VENT HOLES,

BLEED AIR VALVES AND OTHER OPENINGS.

• TF-33 COWLING SHALL REMAIN INSTALLED DURING EXTERNAL WASHING OPERA-

TIONS.

1. SEAL DISCONNECTED ELECTRICAL CONNECTORS AND COMPONENTS AS REQUIRED TO

KEEP CLEANING SOLUTION OUT OF THOSE AREAS.

2. LUBRICATED PARTS SHALL BE PROTECTED.

CARD NO.

4-002

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REQUIREMENTS

4-002 SYS SUB

• BEFORE APPLYING CLEANING SOLUTION, THE ENGINES AND ACCESSORIES SHALL

BE AT AMBIENT TEMPERATURE TO PREVENT EXCESSIVE TEMPERATURE CHANGES

ON ENGINE COMPONENTS AND CONSEQUENT DAMAGE.

• WET THE AREAS TO BE CLEANED WITH WATER, ESPECIALLY AT SEAMS AND LAP

JOINTS BEFORE APPLYING CLEANING SOLUTION. THIS WILL REDUCE THE POSSI-

BILITY OF CLEANING SOLUTION GETTING UNDER SKIN AREAS DUE TO CAPILLARY

ACTION.

• CLEANING SOLUTION SHALL NOT BE APPLIED TO AREAS WHERE AGENTS MAY BE

ENTRAPPED. CARE WILL BE EXERCISED WHEN CLEANING AROUND ELECTRICAL

COMPONENTS.

NOTE

CLEANING SOLUTION MAY BE APPLIED BY SPRAYING, SWABBING, BRUSHING OR

MOPPING.

3. PREPARE CLEANING SOLUTION PER TO 1-1-691.

A. FOR STARTER EXHAUST AREA: ONE PART CLEANING COMPOUND DILUTED WITH THREE

PARTS WATER. ONE PART CLEANER WITH ONE PART WATER FOR HEAVILY SOILED AREA.

B. FOR MODERATELY OR LIGHTLY SOILED AREAS, PAINTED OR UNPAINTED SURFACES: ONE

PART CLEANING COMPOUND WITH TEN TO FIFTEEN PARTS WATER.

4-002

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WORK UNIT CODE WA H PROCEDURES INSPECTION

REQUIREMENTS

ELECTRICAL POWER SERVICE FIGURE CARD NO.

4-002 SYS SUB

4. APPLY PROPERLY MIXED SOLUTION TO THE STARTER EXHAUST AREA. BRUSHING WITH A

NON-METALLIC BRUSH, MIL-B-5612, MAY BE REQUIRED TO GET AREA AS CLEAN AS POS-

SIBLE. RINSE THOROUGHLY WITH CLEAN WATER.

5. APPLY PROPERLY MIXED SOLUTION TO OTHER AREAS TO BE CLEANED. BEGIN AT THE LOW-

EST SURFACE AND WORK UP UNTIL ALL AREAS TO BE CLEANED ARE COMPLETELY COV-

ERED. AGITATE WITH A NON-METALLIC BRUSH IN EXTREMELY SOILED AREAS. DEPENDING

ON THE WEATHER CONDITION, ALLOW APPROXIMATELY 5 TO 10 MINUTES FROM APPLICA-

TION TO RINSING.

NOTE

DO NOT ALLOW MIXTURE TO DRY BEFORE RINSING.

6. THOROUGHLY RINSE SOLUTION FROM THE AREAS BEING CLEANED USING LARGE AMOUNTS

OF WATER. MAKE CERTAIN ALL SEAMS AND LAP JOINTS ARE THOROUGHLY RINSED. HEATED

WATER (120 DEGREES MAXIMUM) WILL GIVE THE BEST RESULTS, HOWEVER COOL TAP WA-

TER MAY BE USED.

7. OPEN AND HAND WASH INSIDE F108 ENGINE COWLING AND RINSE WITH LOW PRESSURE

WATER AVOIDING UNNECESSARY WATER SPRAY ONTO ENGINE.

8. REMOVE TF-33 ENGINE COWLINGS AND WASH SEPARATELY FROM AIRCRAFT.

9. THRUST REVERSER (P-5, PW-102 ONLY).

A. MOVE AFT REVERSER SLEEVE TO REVERSE THRUST POSITION.

CARD NO.

4-002

WORK AREA TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

WORK

AREA

WORK UNIT CODE WASH PROCEDURES INSPECTION

REQUIREMENTS

ELECTRICAL POWER SERVICE FIGURE CARD NO.

4-002 SYS SUB

B. USE CLEANING SOLUTION P-D-680, TYPE III, OR MIL-C-85570, OR MIL-C-87937 AS AN AL-

TERNATE CLEANING COMPOUND TO CLEAN THE THRUST REVERSER TRACKS.

C. SPRAY AND THOROUGHLY FLUSH ALL TRACES OF EXHAUST RESIDUE FROM TRACKS,

HINGE BEARINGS, ROD END BEARINGS, TRUCKS AND OTHER MOVABLE COMPONENTS.

DO NOT LUBRICATE ANY OF THE AFT REVERSER COMPONENTS WITH ANYTHING

EXCEPT SPRAY-ON SOLID FILM LUBRICANTS SUCH AS: DRY-SLIDE PN 00903, DRY-

SLIDE INC., INDUSTRIAL PARK, FREEMONT, MI 49412.

10. THRUST REVERSER SLEEVE (P-5, PW-102 ONLY).

A. APPLY CLEANER, MIL-C-87937 (REF. TO 1-1-691, TABLE E-2) TO SOILED SURFACES.

B. AGITATE CLEANER WITH BRUSH FOR FIVE TO TEN MINUTES.

C. THOROUGHLY FLUSH OFF WITH WATER.

D. REPEAT PROCESS AS NECESSARY TO COMPLETELY REMOVE RESIDUE.

INSPECTION REQUIREMENTS

WASH PROCEDURES

FIGURE

DWG

CHANGE NO. CARD NO.

4-003

INSPECTION REQUIREMENTS

WASH PROCEDURES

FIGURE

DWG

4-003

4-004

WORK AREA TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

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MIN

WORK

AREA

WORK UNIT CODE WASH PROCEDURES INSPECTION

REQUIREMENTS

ELECTRICAL POWER SERVICE FIGURE CARD NO.

4-004 SYS SUB

PART IV

UPPER WINGS AND CENTER OF FUSELAGE (STEP 5)

SAFETY CABLES WILL BE INSTALLED AND SAFETY HARNESS WORN WHEN WASH-

ING UPPER EXTERIOR OF AIRCRAFT.

1. INSTALL SAFETY CABLES AND DON SAFETY HARNESS.

CARD NO.

4-004

WORK AREA TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

WASH PROCEDURES

FIGURE

DWG

4-004

4-005

WORK AREA TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE WASH PROCEDURES INSPECTION

REQUIREMENTS

ELECTRICAL POWER SERVICE FIGURE CARD NO.

4-005 SYS SUB

PART IV

UPPER SURFACE OF FUSELAGE (STEP 6)

SAFETY CABLES WILL BE INSTALLED AND SAFETY HARNESS WORN WHEN WASH-

ING UPPER EXTERIOR OF AIRCRAFT.

1. INSTALL SAFETY CABLES AND DON HARNESS.

CARD NO.

4-005

WORK AREA TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

WASH PROCEDURES

FIGURE

DWG

4-005

4-006

WORK AREA TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE WA H PROCEDURES INSPECTION

REQUIREMENTS

ELECTRICAL POWER SERVICE FIGURE CARD NO.

4-006 SYS SUB

PART IV

WASH PROCEDURES

INTERIOR CLEANING (STEP 7)

1. RELIEF FACILITIES AND COMPONENTS:

DO NOT USE SUCH LARGE QUANTITIES OF CLEANING SOLUTION, DEODORIZING

SOLUTION OR RINSE WATER THAT THEY RUN BENEATH THE FLOOR TO AIRPLANE

STRUCTURE.

A. REMOVE THE LATRINE TANKS AND CANS AND DISCHARGE THE WASTES INTO SANITARY

SEWER SYSTEM, AS APPLICABLE. CLEAN, SANITIZE, AND DEODORIZE TANKS, CANS, AND

LATRINE PER -2-2 SERIES TECHNICAL ORDERS. FOR RC/TC135 AIRCRAFT USE ETM-RC/

TC135 LAVATORY MM.

2. CLEAN BATTERY COMPARTMENTS/TRAYS.

3. CLEAN THE FOLLOWING GALLEY EQUIPMENT (IF APPLICABLE):

A. FOOD PREPARATION AREA.

B. STORAGE COMPARTMENT.

CARD NO.

4-006

WORK AREA TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

WORK

AREA

WORK UNIT CODE WASH PROCEDURES INSPECTION

REQUIREMENTS

ELECTRICAL POWER SERVICE FIGURE CARD NO.

4-006 SYS SUB

C. OVEN(S) AND MICROWAVES.

D. HOT CUP(S).

E. BEVERAGE CONTAINER(S).

F. REFRIGERATOR.

G. HOOD AND EXHAUST FILTER SYSTEM.

H. REFUSE BIN(S).

5-001

WORK AREA TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

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CHANGE NO.

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WORK

AREA

WORK UNIT CODE POS T WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER SERVICE FIGURE CARD NO.

5-001 SYS SUB

PART V

POST WASH REQUIREMENTS

NOTE

• FOR WASHES NOT ACCOMPLISHED IN CONJUNCTION WlTH THE PERIODIC INSPEC-

TIONS, ALL POST WASH LUBRICATION REQUIREMENTS MUST BE ACCOMPLISHED

WITHIN 72 HOURS AFTER THE START OF THE WASH OR BEFORE FIRST FLIGHT,

WHICHEVER COMES FIRST.

• FOR WASHES ACCOMPLISHED PRIOR TO THE PERIODIC INSPECTIONS, ALL ITEMS

MARKED WlTH A PLUS (+) SIGN MUST BE ACCOMPLISHED WITHIN 72 HOURS AFTER

START OF THE WASH. ALL OTHER ITEMS MUST BE ACCOMPLISHED BEFORE NEXT

FLIGHT.

1. RECONNECT MAIN AIRCRAFT BATTERY PER 2-10 SERIES TECHNICAL ORDERS.

2. FOR KC-135R/T AND WC-135R AIRCRAFT, RECONNECT APU BATTERY PER 2-16 SERIES TECH-

NICAL ORDERS.

A. FOR RC/TC-135 AIRCRAFT, RECONNECT JFS BATTERY PER 2-10 SERIES TECHNICAL OR-

DERS.

B. FOR NC/WC-135W AIRCRAFT, RECONNECT AUXILIARY BATTERY PER 2-10 SERIES TECHNI-

CAL ORDERS.

3. FOR NC/RC/TC-135 AIRCRAFT, RECONNECT THE INS BATTERY PER DMM-BS135.

CARD NO.

5-001

WORK AREA TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

5-001 SYS SUB

FAILURE TO REMOVE MASKING/PROTECTIVE COVERS PRIOR TO ENGINE/AIR-

CRAFT OPERATION COULD RESULT IN DAMAGE TO EQUIPMENT.

NOTE

DO NOT REMOVE LEFT AND RIGHT MAlN LANDING GEAR WHEEL COVERS UNTIL

AIRCRAFT IS DRIP-DRY, AND FLAPS HAVE BEEN RAISED AND COMPLETELY

DRAINED OF WATER.

4. ACCOMPLISH THE FOLLOWING: REMOVE MASKING, PROTECTIVE COVERING (EXCEPT LEFT

AND RIGHT MAIN LANDING GEAR WHEEL COVERS), AND SAFETY LOCKS IF NO OTHER WORK

IS TO BE ACCOMPLISHED TO THE AREA.

TO PREVENT UNNECESSARY CORROSION ON IDG, ALL EXCESS WATER MUST BE

REMOVED FROM TOPS OF ALL IDGS AFTER COMPLETION OF WASH AND RINSE.

5. (F108) DRY ALL WATER OFF THE TOPS OF INTEGRATED DRIVE GENERATORS PRIOR TO

CLOSING COWLING.

6. OPEN ALL FUSELAGE WATER DRAIN SCREWS, ALLOW WATER TO DRAIN, THEN CLOSE

SCREWS.

5-001

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AREA

WORK UNIT CODE POS T WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER SERVICE FIGURE CARD NO.

5-001 SYS SUB

POST WASH LUBRICATION

7. LUBRICATION INFORMATION:

A. DO NOT MIX MIL-PRF-81322 AND MIL-PRF-23827.

B. WHERE MIL-PRF-23827 IS CALLED OUT USE MIL-PRF-23827, TYPE 1.

C. USE MIL-PRF-81322 ONLY WHERE SPECIFICALLY CALLED OUT.

D. USE MIL-PRF-32014 ONLY WHERE SPECIFICALLY CALLED OUT. IF MIL-PRF-32014 IS NOT

AVAILABLE, USE MIL-PRF-81322.

E. VV-L-800 HAS BEEN SUPERCEDED BY MIL-PRF-32033. SUPPLIES OF VV-L-800 MAY BE USED

UNTIL DEPLETED.

8. WITHIN 4 HOURS AFTER COMPLETION OF THE WASH ACCOMPLISH THE FOLLOWING:

A. COMPLETE ALL LUBRICATION ITEMS ON CARD 5-017.

B. RAISE WING FLAPS TO ALLOW WATER TO DRAIN. AFTER WATER HAS DRAINED, FLAPS

MAY BE LOWERED TO THE 50 DEGREE DETENT FOR FURTHER INSPECTIONS, AS RE-

QUIRED.

C. ACCOMPLISH BOOM LUBRICATION REQUIREMENTS ON CARD 5-026 AND 5-027, PRIOR TO

STOWING BOOM.

CARD NO.

5-001

WORK AREA TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

5-002

WORK AREA

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POS T WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

SERVICE FIGURE CARD NO.

5-002 SYS SUB

LUBRICATION

NOSE WHEEL WELL DOORS AND MECHANISM:

1 13 FBC 1. LOCK BUNGEE: FLUSH FITTING (2 PLACES).

1 13 FF- 2. NOSE WHEEL WELL DOOR RELEASE SUPPORT ASSEMBLY: ZERK FITTINGS (1 IN WHEEL WELL)

(1 IN LOWER NOSE COMPARTMENT).

1 13 FBL 3. DOOR OPERATOR HOUSING ASSEMBLY: FLUSH FITTING (3 PLACES).

1 13 FBN 4. SEQUENCE VALVE CONNECTING LINK: FLUSH FITTING (2 PLACES).

1 13 FB- 5. NOSE WHEEL DOOR RELEASE ARM: WIPE CLEAN AND APPLY 4 DROPS OF OIL.

1 13 FBD 6. DOOR OPERATOR ARM AND LINK: FLUSH FITTING (5 PLACES).

1 13 GAA 7. WHEEL WELL DOOR ACTUATOR: FLUSH FITTING (2 PLACES).

1 13 FBK 8. LINK: FLUSH FITTING (2 PLACES).

1 13 FB- 9. WHEEL WELL DOOR QUICK DISCONNECT (PIP) PIN: APPLY 4 DROPS TO PIN LOCKING BALL

BEARINGS AND SHAFT (2 PLACES EACH PIN) WIPE EXCESS.

13 FB- 10. WHEEL WELL DOOR OPERATOR RODS: FLUSH FITTING (4 PLACES).

CARD NO.

5-002

WORK AREA

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE

DWG

5-002

5-003

WORK AREA

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-003 SYS SUB

FB0

LUBRICATION

NOSE WHEEL WELL DOORS AND MECHANISM:

1. SHOCK STRUT DOOR HINGE: FLUSH FITTING (2 PLACES).

2. SHOCK STRUT DOOR OPERATOR ROD: FLUSH FITTING (2 PLACES).

3. NOSE GEAR EMERGENCY EXTENSION ACCESS DOOR HINGES: APPLY FOUR DROPS. WIPE

OFF EXCESS OIL (2 PLACES).

4. NOSE GEAR DOOR CONTROL VALVE CONNECTING LINKAGE: FLUSH FITTING (2 PLACES).

5. WHEEL WELL DOOR HINGES: FLUSH FITTING (2 PLACES EACH DOOR).

CARD NO.

5-003

WORK AREA

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE

DWG

5-003

5-004

WORK AREA

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POS T WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

SERVICE FIGURE CARD NO.

5-004 SYS SUB

LUBRICATION

NOSE LANDING GEAR

1 13 JAA + 1. STEERING COLLAR ASSEMBLY: FLUSH FITTING (4 PLACES). USE SPECIAL FITTING DESCRIBED IN -2-2 SERIES TECHNICAL ORDERS IF AVAILABLE. IF NOT, ROTATE GEAR TO ITS FULL EXTENT

OF TRAVEL ON EITHER SIDE OF ITS CENTER LINE TO ALLOW ACCESS TO THE 2 FWD FIT-

TINGS. JACK THE NOSE OF THE AIRPLANE TO ALLOW THE GEAR TO FULLY EXTEND TO GAIN

ACCESS TO THE 2 AFT FITTINGS.

1 13 JAR + 2. STEERING CYLINDER ROD END: FLUSH FITTING (1 PLACE EACH CYLINDER).

1 13 JAA + 3. TOWING COLLAR ASSEMBLY: ZERK FITTING (4 PLACES).

1 13 JA- + 4. NOSE STEERING CABLES - APPLY A LIGHT COAT OF GREASE MIL-G-81322.

1 13 FF- + 5. DOOR TO CABLE LINK (APPLY THREE DROPS).

1 13 FCC + 6. LIGHTLY COAT EXPOSED INNER CYLINDER SHOCK STRUT AREA WITH FLUID PER MIL-PRF-

87257, WIPE OFF EXCESS.

1 13 FAB 7. TRUNNION BEARINGS LH, AND RH: ZERK FITTING (1 PLACE EACH BEARING).

1 13 FFA 8. TORSION LINKS: ZERK FITTING (3 PLACES EACH LINK).

CARD NO.

5-004

WORK AREA

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE

DWG

5-004

5-005

WORK AREA

TYPE MECH RQR

APG

MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POS T WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

SERVICE FIGURE CARD NO.

5-005 SYS SUB

LUBRICATION

1 13 FD- 1. DRAG BRACE ASSEMBLY: ZERK FITTING (2 PLACES), FLUSH FITTING (7 PLACES).

1 13 GAG 2. LOCK RETENTION ACTUATOR: FLUSH FITTING (2 PLACES).

NOTE

CARE MUST BE TAKEN TO PREVENT DIRT OR FOREIGN PARTICLES ENTERING

LOCK WHEN LUBRICATING.

1 13 FDE 3. DRAG BRACE LOCK ROLLERS:

13 FDE A. REMOVE THE TWO LUBRICATION PLUGS.

13 FDE B. USING A NEEDLE POINT GREASE GUN ADAPTER OR DRAG BRACE LUBRICATION FITTING

ADAPTER, LUBRICATE DRAG BRACE LOCK ROLLERS. IF USING DRAG BRACE LUBRICA-

TION FITTING ADAPTER, PERFORM STEPS C THRU E TO INSTALL ADAPTER.

13 FDE C. PARTIALLY UNSCREW FLUSH/ZERK FITTING ADAPTER FROM LUBRICATION FITTING

ADAPTER SO GREASE FITTING IN DRAG BRACE WILL NOT BE CONTACTED WHEN FITTING

ADAPTER IS INSTALLED IN DRAG BRACE.

13 FDE D. SCREW OUTER PLUG OF FITTING ADAPTER INTO DRAG BRACE UNTIL SNUG.

CARD NO.

5-005

WORK AREA

TYPE MECH RQR

APG

MECH NO. CARD TIME PUBLICATION NUMBER

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

SERVICE FIGURE

DWG

CARD NO.

5-005 SYS SUB

13 FDE E. SCREW FLUSH/ZERK FITTING ADAPTER WITH FINGERS UNTIL THE DRAG BRACE FITTING

IS CONTACTED, THEN TURN 1/4 TO 1/2 WITH WRENCH TO SEAT ADAPTER INTO DRAG

BRACE FLUSH FITTING.

13 FDE F. IF THERE ARE TWO LUBRICATION FITTINGS (ONE ON EACH SIDE), APPLY THREE PUMPS

OF GREASE. IF THERE IS ONLY ONE LUBRICATION FITTING, APPLY FIVE PUMPS OF

GREASE.

13 FDE G. REMOVE LUBRICATION FITTING ADAPTER IF USED. REINSTALL LUBRICATION PLUGS AND

SAFETY WIRE.

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE CHANGE NO. CARD NO.

5-005

5-006

WORK AREA

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-006 SYS SUB

GAE

GAF

FBG

LUBRICATION

1. NOSE GEAR ACTUATOR: ZERK FITTING (2 PLACES) (LIMIT QUANTITY TO 1 PUMP OF GUN).

2. LOCK ACTUATOR: FLUSH FITTING (2 PLACES).

3. DOOR CONTROL VALVE CRANK: FLUSH FITTING (1 PLACE).

CARD NO.

5-006

WORK AREA

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE

DWG

5-006

5-007

WORK AREA

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-007 SYS SUB

JB-

JA-

LUBRICATION

NOSE GEAR STEERING:

1. STEERING METERING VALVE OPERATING LINK: FLUSH FITTING (2 PLACES).

NOTE

HOUSING DRAIN HOLES ARE EXTERNAL OF MAIN ASSEMBLY.

2. STEERING SHAFT EXTENSION ASSEMBLY: INJECT OIL INTO 2 HOLES IN POSITIONING SLEEVE.

HOLES CAN BE SERVICED THROUGH THE HOUSING DRAIN HOLES.

CARD NO.

5-007

WORK AREA

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE

DWG

5-007

5-008

WORK AREA

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-008 SYS SUB

LUBRICATION

1. KEEL BEAM BAY DOOR:

A. DOOR HINGES: APPLY A LIGHT COAT OF MIL-PRF-32033.

B. DOOR LATCHES: LUBRICATE WITH MIL-PRF-32033.

C. LATCH SHAFTS AND LATCH PORTS: WIPE CLEAN, LUBRICATE WITH MIL-PRF-23827, AND

WIPE EXCESS.

CARD NO.

5-008

WORK AREA

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

5-009

WORK AREA

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-009 SYS SUB

34-

36-

1. CARGO DOOR HINGE: APPLY OIL, MIL-PRF-32033 TO FULL LENGTH OF HINGE, WIPE OFF EX-

CESS OIL.

EMERGENCY EXIT HATCHES

NOTE

(DO NOT REMOVE RIGHT OVER WING HATCH ON RC-135 AIRCRAFT IN WHICH AC-

CESS TO HATCH IS BLOCKED BY EQUIPMENT RACK).

2. EXTERIOR LATCH SLEEVE: WIPE CLEAN AND APPLY LIGHT COAT OF MIL-PRF-23827.

CARD NO.

5-009

WORK AREA

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE

DWG

5-009

5-010

WORK AREA

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

5-010 SYS SUB

97-

97-

97-

LUBRICATION

ARR DOORS AND RECEPTACLE (ARR SYSTEM ACFT ONLY):

1. FORWARD SEAL RETAINER: ZERK FITTING (1 PLACE EACH DOOR).

2. AFT SEAL RETAINER: ZERK FITTING (1 PLACE EACH DOOR).

3. GUIDE ROLLERS: LUBRICATE THROUGH ZERK FITTINGS (4 PLACES EACH SIDE).

CARD NO.

5-010

WORK AREA

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE

DWG

5-010

5-011

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-011 SYS SUB

2,3

EJD

EKC

EKD

LUBRICATION

FILLET FLAP SYSTEM

1. FILLET FLAP HINGES: FLUSH FITTING (3 PLACES).

2. TORQUE TUBE SUPPORT BEARINGS: ZERK FITTING (2 PLACES).

3. FILLET FLAP TRANSMISSION TRUNNIONS, AND BALL SCREW TRUNNIONS: FLUSH FITTING (4

PLACES).

CARD NO.

5-011

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE

DWG

5-011

5-012

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-012 SYS SUB

EL-

ELG

ELL

LUBRICATION

FLAP SYSTEM AND COVE LIP DOORS

1. CAM ROLLER: FLUSH FITTING (9 PIECES EACH WING).

2. DOOR STOP: FLUSH FITTING (9 PLACES EACH WING).

3. COVE LIP DOOR CAM TRACK: WIPE CLEAN, APPLY LIGHT COAT MIL-C-11796 (GRADE 3) (9

PLACES EACH WING).

CARD NO.

5-012

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE

DWG

5-012

5-013

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-013 SYS SUB

ECG

ECK

E--

FLAP SYSTEM AND COVE LIP DOORS:

1. OUTBOARD TORQUE TUBE SUPPORT BEARING: ZERK FITTING (1 PLACE).

2. FLAP TRANSMISSION TRUNNIONS, AND BALL SCREW TRUNNIONS: ZERK FITTING (8 PLACES), FLUSH FITTING (8 PLACES).

3. FLAP CARRIAGES: FLUSH FITTINGS (10 PLACES EACH CARRIAGE).

CARD NO.

5-013

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE

DWG

5-013

5-014

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-014 SYS SUB

EDD

EDD

FLAP SYSTEM

1. BYPASS VALVES SPRING CARTRIDGE: WITHOUT DISASSEMBLING SPRING CARTRIDGE, WIPE

CLEAN AND BUTTER LUBE EXTERNAL SLIDING SURFACES WITH MIL-PRF-23827 (2 PLACES,

INBD/OTBD FLAP EMERGENCY BYPASS VALVE).

2. BYPASS VALVE SPRING PRESSURE DECK CAVITY: FROM INSIDE CARGO COMPARTMENT WIPE

CAVITY BETWEEN VALVE AND FLOOR PRESSURE WEB CLEAN AND REFILL WITH MIL-PRF-

23827(2 PLACES INBOARD AND OUTBOARD FLAP BYPASS VALVES).

CARD NO.

5-014

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE

DWG

5-014

5-015

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-015 SYS SUB

EMD

EMF

LUBRICATION

LEADING EDGE FLAP WELLS AND FLAPS

1. HINGE FITTING: FLUSH FITTING (1 PLACE EACH FITTING).

2. ACTUATOR ROD END: FLUSH FITTING (1 PLACE EACH ACTUATOR) (LIMIT QUANTITY TO 1 PUMP

OF GUN).

CARD NO.

5-015

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE

DWG

5-015

5-016

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-016 SYS SUB

A--

A--

LUBRICATION

LEFT AND RIGHT WING

1. LUBRICATE EXPOSED CONTROL CABLES IN THE FOLLOWING AREAS: APPLY A LIGHT COAT OF

GREASE, MIL-G-81322 TO CABLES.

A. FLAP WELL.

B. WHEEL WELL.

CARD NO.

5-016

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

5-017

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POS T WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

SERVICE FIGURE CARD NO.

5-017 SYS SUB

LUBRICATION

FLAP SYSTEM AND COVE LIP DOORS (LEFT AND RIGHT)

2,3 14 ELG 1. DOOR STOP ROLLERS: (9 PLACES) WIPE CLEAN, APPLY THREE DROPS OF OIL TO BEARING

AND SHAFT, WIPE EXCESS.

2,3 14 ELJ 2. LATCH STOP ASSEMBLY: APPLY OIL TO EXPOSED SHAFT AND ACTUATE LATCH TO ENSURE

INTERIOR IS LUBED.

2,3 11 AR0 3. FLAP TRACK: WIPE CLEAN AND APPLY LIGHT FILM OF COMPOUND MIL-C-11796 GRADE 3 OR

ALTERNATE MIL-C-16173 GRADE 5 FOR COLD APPLICATION (6 PLACES).

2,3 14 ELJ 4. LATCH STOP ASSEMBLY: FLUSH FITTING (9 PLACES) (PN 6-74621-4 ONLY).

2,3 14 EKE 5. WING FLAP JACKSCREWS (10 PLACES):

2,3 14 EKE A. FOR NON-CHROME PLATED FLAP JACKSCREWS, PERFORM THE FOLLOWING ACTIONS:

14 EKE (1) CLEAN BALL SCREW WITH SOLVENT, PRF-680, TYPE II OR III, AND DRY WITH LINT-

FREE CLOTH OR MOISTURE-FREE COMPRESSED AIR.

CARD NO.

5-017

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

SERVICE FIGURE CARD NO.

5-017 SYS SUB

14 EKE (2) INSPECT JACKSCREW FOR PITTING, FLAKING, GOUGING, CORROSION, SPALLING OR

BRINELLING PARTICULARLY IN THE BALL GROOVE AREA. INSPECT PER TO 16G2-3-

3-3, PARAGRAPHS 4.A.1 AND 4.A.3.

NOTE

IF DEFECTS CANNOT BE CORRECTED, REPLACE JACKSCREW ASSEMBLY.

14 EKE (3) REMOVE CORROSION WITH SCOTCH BRITE PAD AND CORRECT MINOR DEFECTS

WITH 600 OR 800 SANDPAPER OR EQUIVALENT AND RE-CLEAN AS REQUIRED.

14 EKE (4) APPLY DRY FILM LUBRICANT (MIL-PRF-46147) TO AREAS OF BARE METAL AND ALLOW

TO DRY.

14 EKE (5) APPLY LIGHT COAT OF OIL (MIL-PRF-32033) TO THE UPPER PORTION OF THE BALL

SCREW. RAISE FLAPS TO THE 30 DEGREE DETENT PER 2-2 SERIES TECHNICAL OR-

DERS AND WIPE CLEAN AND LUBRICATE THE LOWER PORTION OF THE SCREW. OP-

ERATE FLAPS THROUGH ONE COMPLETE CYCLE AND WIPE OFF EXCESS OIL.

2,3 14 EKE B. FOR CHROME PLATED FLAP JACKSCREWS, PERFORM THE FOLLOWING ACTIONS:

NOTE

DO NOT APPLY OIL TO BALL SCREW.

14 EKE (1) ENSURE JACKSCREWS ARE CLEAN.

14 EKE (2) SERVICE BALL SCREW NUT WITH GREASE, MIL-PRF-23827, UNTIL GREASE SEEPS

FROM SEALS.

5-018

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-018 SYS SUB

APD

SPOILER SYSTEM:

1. SPOILER ACTUATOR: FLUSH TYPE FITTING (2 PLACES EACH ACTUATOR) (LIMIT QUANTITY TO

1 PUMP OF GUN).

CARD NO.

5-018

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE

DWG

5-018

5-019

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-019 SYS SUB

ALJ

AP-

LUBRICATION

SPOILER SYSTEM

1. SPOILER CENTER HINGE FITTINGS: FLUSH FITTINGS (2 PLACES EACH SIDE).

2. VALVE SPRING SWIVEL: APPLY THREE DROPS OF OIL (2 PLACES EACH SIDE).

CARD NO.

5-019

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE

DWG

5-019

5-020

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-020 SYS SUB

ALH

SPOILER SYSTEM (LEFT AND RIGHT)

1. SPOILER TRAILING EDGE ROLLERS: WIPE CLEAN, APPLY THREE DROPS OF OIL TO BEARING, ROTATE BEARING, WIPE OFF EXCESS (2 PLACES EACH SPOILER).

CARD NO.

5-020

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE

DWG

5-020

5-021

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-021 SYS SUB

AHC

OUTBOARD AILERON (LEFT AND RIGHT)

1. OUTBOARD AILERON BALANCE TAB PIANO HINGE: APPLY OIL TO ENTIRE LENGTH OF HINGE, WIPE EXCESS.

CARD NO.

5-021

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE

DWG

5-021

5-022

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-022 SYS SUB

8DB

CORROSION PREVENTION

1. (F108) FOR AIRCRAFT OPERATING IN SEVERE CORROSION ZONES, ENGINE INLET LIP SKINS

ARE NOT TREATED WITH DEXTER 4002, ACCOMPLISH THE FOLLOWING:

A. WIPE-ON AND WIPE-OFF MIL-C-85054 AMLGUARD CPC ON THE UNPAINTED ENGINE INLET

LIP SKINS PER TO 1C-135-3-1.

CARD NO.

5-022

WORK AREA

2,3

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

5-023

WORK AREA

3,4

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-023 SYS SUB

1. REFUEL VALVE LINEAR ACTUATOR ATTACHMENT POINTS: APPLY THREE DROPS OF OIL (AS

APPLICABLE).

CARD NO.

5-023

WORK AREA

3,4

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

INSPECTION REQUIREMENTS

POST WASH REQUIREMENTS

FIGURE

DWG

5-023

5-024

WORK AREA

TYPE MECH RQR MECH NO. CARD TIME PUBLICATION NUMBER

TO 1C-135-6WC-3

CHANGE NO.

MAN

MIN

WORK

AREA

WORK UNIT CODE POST WASH REQUIREMENTS INSPECTION

REQUIREMENTS

ELECTRICAL POWER

OFF

5-024 SYS SUB

CGC

LEFT AND RIGHT ELEVATORS

1. ELEVATOR STABILIZER ACTUATED TAB PIANO HINGE: APPLY OIL TO FULL LENGTH OF HINGE

(1 PLACE EACH SIDE), WIPE OFF EXCESS.

CARD…