Airframe & Engine Tools

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Boeing Tooling

Product Nr. Description Applicability  
2MIT65B04011-41 SAFETY RIG & TOW PIN, NOSE GEAR
USED TO HOLD THE NOSE GEAR
STEERING METERING VALVE IN THE
NEUTRAL POSITION & ALLOW FLUID
BYPASS FROM ONE STEERING CYLINDER
TO THE OTHER WHEN TOWING THE
AIRCRAFT.
747  
4MIT65B80307-1 PROTRACTOR ASSY - CONTROL COLUMN
USED TO MEASURE ANGULAR MOVEMENT
OF CONTROL COLUMN, CONTROL WHEELS
AND VARIOUS CONTROLS DURING
INSTALLATION. USED IN CONJUNCTION
WITH MIT65B00115-1,
MIT69B81601-1, MIT65B0985-9,
MIT65B80326-6 & 3MIT65B80307-1.
QUIVALENT
707, 727, 737, 747, 757, 767  
A09003-2 USED TO LOCK THE NOSE LANDING GEAR STEERING BYPASS VALVE (TOWING LEVER) IN THE HYDRAULIC BYPASS POSITION FOR AIRPLANE TOWING. 737, 757, 777, 787  
A12001-14 FUEL SAMPLING EQUIPMENT USED FOR
CHECKING FUEL TANK SUMPS FOR
WATER OR FOR COLLECTING FUEL
SAMPLES.
747  
A12001-15 FUEL SAMPLING EQUIPMENT USED FOR
CHECKING FUEL TANK SUMPS FOR
WATER OR FOR COLLECTING FUEL
SAMPLES.
777, 787  
A20001-185 BOOM HOIST EQPT - GENERAL (400 LB
CAPACITY). IN CONJUNCTION WITH
APPROPRIATE ADAPTERS OR WITH
SHORT OR LONG HOIST ARM ASSYS
WILL BE USED TO INSTALL/REMOVE
VARIOUS AIRPLANE COMPONENTS.
737, 757, 767, 777, 787  
A21010-203 VACUUM TANK - PRESSURE RELIEF
VALVE TEST USED TO TEST PRESSURE
RELIEF VALVES.
727, 737, 747, 757, 767, 777, 787  
A27007-19 GROUND LOCK - LEADING EDGE SLATS
USED TO LOCK THE INBOARD OR
OUTBOARD LEADING EDGE SLATS
DURING MAINTENANCE OPERATIONS.
TWO LOCK ASSEMBLIES ARE REQUIRED
TO SIMULTANEOUSLY LOCK BOTH
INBOARD AND OUTBOARD SLATS.
767  
A27092-132 ACTUATOR/DEACTUATOR SET -
PROXIMITY SENSORS USED TO ACTUATE
OR DEACTUATE SENSORS DURING
SENSOR TEST PROCEDURES.
767, 787  
A27092-139 ACTUATOR/DEACTUATOR SET -
PROXIMITY SENSORS USED TO ACTUATE
OR DEACTUATE SENSORS DURING
SENSOR TEST PROCEDURES.
737, 747, 757, 767  
A27124-36 FORCE EQPT - RUDDER FREEPLAY
CHECK USED TO APPLY A CONSTANT
FORCE TO THE RUDDER IN ORDER TO
MEASURE THE FREEPLAY OF THE
RUDDER ACTUATORS.
747, 757, 767, 777, 787  
A28005-82 TEST EQPT - LEAK & PRESSURE, APU
FUEL LINE SHROUD USED TO CHECK
PRESSURE AND LEAKAGE OF APU FUEL
LINE SHROUD.
737-NG, 737-MAX, 757, 767, 777  
A32012-13 WRENCH - WHEEL RETAINING NUT,
M.L.G. USED TO TORQUE MLG WHEEL
RETAINING NUT.
767  
A32015-9 INSTL./REM. TOOL - DOWN LOCK, MLG
& NLG TO ALLOW INSERTION AND
REMOVAL OF THE MAIN GEAR AND NOSE
GEAR GROUND LOCK PINS FROM GROUND
LEVEL.
757, 767, 777, 787  
A32045-114 WRENCHES - SPANNER CONTAINS
VARIOUS LANDING GEAR WRENCHES.
777  
A32069-7 WRENCH ADAPTER - RETAINER NUT,
ANTI-SKID TRANSDUCER USED TO
REMOVE AND INSTALL THE ANTI-SKID
TRANSDUCER RETAINER NUT.
737, 757, 767  
A32080-1 BRAKE DISCONNECT - FLIGHT
DISPATCH USED TO ALLOW EITHER A
747-400, -400F, -8, 757 OR 767
AIRPLANE TO DISPATCH WITH ANY ONE
OF THE BRAKES INOPERATIVE.
747, 757, 767  
A32101-1 WRENCH ADAPTER - AXLE NUT, NLG
USED TO INSTALL AND REMOVE THE
WHEEL RETAINING NUT OF THE NOSE
LANDING GEAR.
767  
A34001-4 WARNING EQUIP - ATC, DME, VHF
ANTENNA AND DRAIN MAST USED TO
PREVENT INJURY TO THE ANTENNA,
DRAIN MASTS OR PERSONNEL.
WARNING STREAMERS WILL HANG NEXT
TO THE ATC, DME, AND VHF
ANTENNAS, OR DRAIN MASTS.
767, 777, 787  
A38001-22 VACUUM TEST EQPT - VACUUM WASTE
SYSTEM USED TO PLUG WASTE SYSTEM
AND PROVIDE LEAK DETECTING
EQUIPMENT.
737, 747, 757, 767, 777  
A38001-68 VACUUM TEST EQPT - VACUUM WASTE
SYSTEM USED TO PLUG WASTE SYSTEM
AND PROVIDE LEAK DETECTING
EQUIPMENT.
737, 747, 757, 767, 777, 787  
A38003-30 BLOCKAGE REMOVER - VACUUM TOILET.
USED FOR REMOVING AN OBSTRUCTION
BETWEEN TOILET BOWL AND DIAPHRAGM
VALVE.
737, 747, 757, 767, 777, 787  
A38007-9 PLUG, VACUUM WASTE SYSTEM USED TO
PLUG VACUUM WASTE LINE DURING
WASTE SYSTEM OPERATION, WHEN A
TOILET IS REMOVED FOR REPAIRS.
737, 747, 757, 767, 777, 787  
A38012-40 PUMP EQPT - VACUUM LAV SYSTEM
USED FOR REMOVAL OF BUILD-UP ON
THE INNER SURFACES OF THE WASTE
LINE.
737, 747, 757, 767, 777  
A49002-2 LIFTING EYE - GENERATORS AND
STARTERS USED TO PROVIDE A LIFT
POINT FOR REM/INSTL OF GENERATORS
OR STARTERS.
737, 757, 767, 777, 787  
A71015-108 LIFT FIXTURE - ENGINE ACCESSORY
USED TO SUPPORT ENGINE
ACCESSORIES IN CONJUNCTION WITH
THE APPROPRIATE ADAPTER FOR EACH
ENGINE ACCESSORY.
737, 747, 757, 767, 787  
A78019-29 HAND PUMP - OPENING SYSTEM,
THRUST REVERSER. USED TO SUPPLY
HYDRAULIC PRESSURE TO THE
ACTUATOR & PDOS SYSTEMS FOR THE
OPENING OF THE FAN COWLS (777 &
787)AND THE THRUST REVERSERS
(737,747,757,767,777,787)FOR
ENGINE MAINTENANCE.
737, 747, 757, 767, 777, 787  
B20004-42 COMPONENT - RECEPTACLE - FUEL SAMPLING USED
FOR COLLECTING FUEL SAMPLES AND/
OR DRAINING SUMPS OF WING AND
CENTER SECTION TANKS.
757  
B28001-18 ADAPTER - SUMP DRAIN VALVE, REM/
INSTL USED FOR REM/INSTL OF THE
PRIMARY SUMP DRAIN VALVES FROM
THE FUEL TANKS.
757, 767, 777  
B52004-1 INSTALLATION TOOL - DOOR SEAL
USED TO INSTALL DOOR SEALS.
707, 727, 737, 747, 757, 767, 777  
B54001-53 HYDRAULIC PUMP - ENGINE `C` DUCT
USED TO OPEN THE `C` DUCT FOR
ENGINE MAINTENANCE.
737, 747, 757, 767  
B71040-66 SLING EQPT - INLET COWL. USED TO
REMOVE/INSTALL THE INLET COWL ON
RB211, CFM56-7 AND CFM LEAP-1B
ENGINES.
737, 747, 757, 767  
B71044-28 ADAPTER EQUIPMENT - LOAD TEST,
PRESSURE RELIEF DOOR LATCH. USED
TO APPLY A TEST LOAD WITH THE USE
OF A TORQUE WRENCH ON THE
PRESSURE RELIEF DOOR LATCH.
737, 747, 757, 767, 777  
B78001-24 LOCK - THRUST REVERSER ISOLATION
VALVE (GROUND,FLYAWAY &
DISPATCH), -2, -5, & -24 ARE
USED TO PREVENT T/R OPERATION IN
FLIGHT. -1, -8, -14 & -24 ARE
USED TO PREVENT T/R OPERATION ON
GROUND DURING MAINTENANCE &
ALLOWS MANUAL OPERATION OF THRUST
REVERSER. -43 USED ON 747-8 TO
HOLD T/R ACTUATOR & TRACK LOCK,
IN UNLOCK POSITION ON GROUND
DURING MAINTENANCE.
747, 777  
C07002-1 FITTING - WING JACKING USED TO
PROVIDE JACKING POINT ON EACH
WING.
737-NG, 737-MAX  
C07004-1 PAD - AIRCRAFT JACKING, AFT BODY
USED TO INSERT INTO THE JACK PAD
FITTING TO PERMIT JACKING OF
AIRPLANE.
737-NG, 737-MAX  
C07007-19 JACK FITTING - FWD BODY STA 294.5
USED FOR JACKING/LEVELING THE
NOSE OF THE AIRPLANE. PROVIDES A
JACKING POINT AT STA 294.5, LBL
47.2, WL 170.5.
737-NG, 737-MAX  
C10004-1 PROTECTIVE COVER - VANE SENSOR,
AOA USED TO PROTECT THE ANGLE OF
ATTACK SENSOR WHILE THE AIRPLANE
IS PARKED AND DURING AIRPLANE
WASHING.
737-NG, 737-MAX, 747, 757, 767, 777, 787  
C10005-1 PROTECTIVE COVER EQPT - ENGINE
INLET, CFM LEAP-1B. USED TO
PREVENT FOREIGN OBJECT DEBRIS
(FOD) FROM ENTERING THE ENGINE
INLET WHILE THE AIRPLANE IS
PARKED.
737-MAX  
C10006-1 PLUG EQPT - ENGINE EXHAUST, CFM
LEAP-1B USED TO COVER AND SEAL
THE ENGINE EXHAUST OPENING WHILE
THE AIRPLANE IS PARKED.
737-MAX  
C10007-1 PLUG EQUIPMENT - FAN REVERSER,
CFM LEAP-1B USED TO COVER AND
SEAL THE ENGINE FAN REVERSER
OPENING WHILE THE AIRPLANE IS
PARKED.
737-MAX  
C21003-135 BACKFLUSH EQPT - A/C PACK HEAT
EXCHANGER USED WITH CUSTOMER
SUPPLIED AIR (EITHER APU OR
GROUND CART)AND WATER TO
BACKFLUSH AND CLEAN THE HEAT
EXCHANGERS OF THE AIR
CONDITIONING PACK.
737-NG, 737-MAX  
C21003-155 BACKFLUSH EQPT - A/C PACK HEAT
EXCHANGER USED WITH CUSTOMER
SUPPLIED AIR (EITHER APU OR
GROUND CART)AND WATER TO
BACKFLUSH AND CLEAN THE HEAT
EXCHANGERS OF THE AIR
CONDITIONING PACK.
737-NG, 737-MAX  
C21006-7 DEACTIVATION TOOL - CHECK VALVE USED TO HOLD OPEN CHECK VALVES M913-1 & 4663-8 DURING HEAT EXCHANGER & PLENUM/DIFFUSER ASSEMBLY CLEANING. USED IN CONJUNCTION W/ C21002 & C21003. 737  
C21010-1 CLEANING WAND EQPT - HEAT EXCHANGER. USED FOR CLEANING AIR CONDITIONING PACK HEAT EXCHANGERS. 737-NG, 737-MAX  
C24002-78 JACK ADAPTER - VSCF & IDG USED
FOR REMOVING/INSTALLING VSCF
(VARIABLE SPEED CONSTANT
FREQUENCY) GENERATOR/CONVERTER OR
IDG (INTEGRATED DRIVE GENERATOR).
USED IN CONJUNCTION WITH CUSTOMER
FURNISHED JACK.
737-NG, 737-MAX  
C24003-1 TRAY ASSY - BATTERY, RMVL & INSTL
USED TO REMOVE/INSTALL THE MAIN
BATTERY (AND AUXILIARY IF
EQUIPPED) IN THE E/E BAY.
737-NG, 737-MAX  
C26004-83 TEST EQPT - ENGINE FIRE
EXTINGUISHING SYSTEM USED TO
PRESSURIZE THE ENGINE FIRE
EXTINGUISHING SYSTEM FOR TUBING
LEAKAGE TEST.
737-NG, 737-MAX  
C26004-84 TEST EQPT - ENGINE FIRE
EXTINGUISHING SYSTEM USED TO
PRESSURIZE THE ENGINE FIRE
EXTINGUISHING SYSTEM FOR TUBING
LEAKAGE TEST.
737  
C26006-70 TEST BOX - CARGO FIRE
EXTINGUISHING SYSTEM USED TO TEST
THE AIRPLANE ELECTRICAL WIRING TO
THE SQUIBS ON THE FIRE
EXINGUISHING BOTTLES LOCATED IN
OR NEAR THE AIR CONDITIONING
DISTRIBUTION BAY IN THE LOWER
LOBE.
737  
C26011-1 ALIGNMENT EQPT - FIRE SUPPRESSION
BOTTLE NOZZLE USED FOR THE
ALIGNMENT AND TORQUEING OF THE
FIRE EXTINGUISHER BOTTLE NOZZLES.
THE TOOL ORIENTS AFT EXTINGUISHER
BOTTLE(34000055-2) NOZZLES 180°
TO ALIGN WITH FWD EXTINGUISHER
BOTTLE (34000055-2) NOZZLES.
737-NG, 737-MAX  
C27001-51 GROUND LOCK SET - OUTBOARD
SPOILER ACTUATORS. C27001-16
GROUND LOCK SET IS USED TO LOCK
THE OUTBOARD GROUND SPOILER
NUMBERS 1 & 8 IN THE 40° FULLY
EXTENDED POSITION. C27001-41
GROUND LOCK SET IS USED TO LOCK
THE OUTBOARD GROUND SPOILER
NUMBERS 0, 1, 8 & 9 IN THE 60°
FULLY EXTENDED POSITION.
C27001-42 OR -51 GROUND LOCK SET
IS USED TO LOCK THE OUTBOARD
GROUND SPOILER NUMBERS 1 & 12 IN
THE 60° FULLY EXTENDED POSITION.
NOTES: IN CONJUNCTION WITH GROUND
LOCK C27001-16 USE F80017 OR
C27047 FOR SPOILER NUMBERS 2, 3,
6 & 7 AND F80040 FOR SPOILER
NUMBERS 4 & 5 WITH DOUBLE
ACTUATORS. IN CONJUNCTION WITH
GROUND LOCK C27001-41 USE F80017
FOR SPOILER NUMBERS 2, 3, 6 & 7
AND F80040 FOR SPOILER NUMBERS 4
& 5 WITH DOUBLE ACTUATORS. FOR
737-600, -700, -800, -900: IN
CONJUNCTION WITH GROUND LOCK
C27001-42 OR C27001-51 USE C27047
FOR FLIGHT SPOILER NUMBERS 2-5 &
NUMBERS 8-11 AND C27046 FOR INBD
GROUND SPOILER NUMBERS 6 & 7.
FOR 737-7, -8, -8200, -9, -10: IN
CONJUNCTION WITH GROUND LOCK
C27001-51 USE C27107 FOR FLIGHT
SPOILER NUMBERS 2-5 & NUMBERS
8-11 AND C27046 FOR INBD GROUND
SPOILER NUMBERS 6 & 7.
737-NG, 737-MAX  
C27022-1 CLAMP SET - TRAILING EDGE FLAP
TORQUE TUBE USED TO PREVENT THE
TRAILING EDGE FLAP DRIVE SYSTEM
FROM ROTATING WHEN THE TORQUE
TUBES ARE DISCONNECTED OR REMOVED
FOR MAINTENANCE.
737-NG, 737-MAX  
C27034-31 SLING EQPT - ELEVATOR REMOVAL/INSTALLATION. USED FOR REMOVAL AND INSTALLATION OF THE RIGHT AND LEFT ELEVATORS. 737-MAX  
C27038-6 LOCKOUT PIN, L.E. CRUISE
DEPRESSURIZATION VALVE USED TO
LOCK THE MANUAL OVERRIDE HANDLE
OF THE CRUISE DEPRESSURIZATION
VALVE IN THE OFF POSITION,
LOCATED IN THE MAIN WHEEL WELL.
737-NG, 737-MAX  
C27046-13 LOCK SET - INBOARD GROUND SPOILER
ACTUATOR. USED TO HOLD THE
INBOARD GROUND SPOILERS IN THE
DEPLOYED POSITION DURING GROUND
MAINTENANCE. THIS LOCK HAS BEEN
DESIGNED TO WITHSTAND FULL SYSTEM
PRESSURE. USED IN CONJUNCTION
WITH C27001 FOR THE OUTBOARD
GROUND SPOILERS AND C27047 FOR
THE FLIGHT SPOILERS.
737-NG, 737-MAX  
C27047-41 LOCK SET - FLIGHT SPOILER
ACTUATOR USED TO HOLD FLIGHT
SPOILERS IN DEPLOYED POSITION
DURING GROUND MAINTENANCE. LOCK
HAS BEEN DESIGNED TO WITHSTAND
FULL SYSTEM PRESSURE. USED IN
CONJUNCTION W/ C27001 FOR OUTBD
GROUND SPOILERS AND C27046
(737-600 THRU -900) OR F80040
(737-100 THRU -500)FOR THE
737-NG  
C27047-43 LOCK SET - FLIGHT SPOILER
ACTUATOR USED TO HOLD FLIGHT
SPOILERS IN DEPLOYED POSITION
DURING GROUND MAINTENANCE. LOCK
HAS BEEN DESIGNED TO WITHSTAND
FULL SYSTEM PRESSURE. USED IN
CONJUNCTION W/ C27001 FOR OUTBD
GROUND SPOILERS AND C27046
(737-600 THRU -900) OR F80040
(737-100 THRU -500)FOR THE
737-NG  
C27050-82 HANDLING EQUIPMENT - REM/INSTAL,
STAB JACKSCREW USED FOR REMOVAL &
INSTALLATION OF HORIZONTAL
STABILIZER JACKSCREW. USED IN
CONJUCTION W/ CUSTOMER FURNISHED
FISHPOLE HOIST OR CHAIN HOIST
(200 LB MIN CAPACITY) & F80027
STABILIZER LOCK ASSY.
737-NG, 737-MAX  
C27051-29 LOCK SET - LE SLAT AND KRUEGER
FLAP ACTUATORS USED TO LOCK
LEADING EDGE SLAT AND KRUEGER
FLAP ACTUATORS IN THE EXTENDED
POSITION. LOCKS ARE DESIGNED TO
WITHSTAND FULL HYDRAULIC SYSTEM
PRESSURE.
737-NG, 737-MAX  
C27052-39 SLING EQPT - TRAILING EDGE FLAPS
USED TO AID IN THE REMOVAL AND
INSTALLATION OF THE TRAILING EDGE
FLAPS.
737-NG, 737-MAX  
C27060-1 ADAPTER EQPT - CONTROL WHEEL USED
TO MEASURE CONTROL WHEEL ANGLE
AND TORQUE, AND CONTROL COLUMN
ANGLE AND FORCE.
737  
C27066-1 LOCK EQPT - AILERON/ELEVATOR PCU
INPUT ROD(POGO) USED TO LOCK THE
AILERON & ELEVATOR PCU ACTUATOR
IN PLACE DURING TESTING.
737-NG, 737-MAX  
C27083-1 RIGGING BAR - ELEVATOR TAB. USED
TO ALIGN THE ELEVATOR TAB
737-NG  
C27083-18 RIGGING BAR - ELEVATOR TAB. USED
TO ALIGN THE ELEVATOR TAB
737-MAX  
C27084-1 TEST EQUIPMENT - OUTBD T.E. FLAP
TRANSMISSION, NO-BACK BRAKE
OPERATIONAL TEST USED TO CREATE
COMPRESSION LOAD ON THE OUTBD TE
FLAP BALLSCREW POSITION 1,2,7 AND
8 TO MAKE THE RATCHET SOUND
AUDIBLE DURING NO-BACK BRAKE
OPERATIONAL TEST.
737-NG, 737-MAX  
C27095-1 RIGGING LOCK - FOUR DEGREE,
SPEEDBRAKE LEVER USED TO HOLD
SPEEDBRAKE LEVER AT 4 DEGREES.
737-MAX  
C27096-1 AILERON RIGGING TOOL USED TO
VERIFY THE AILERON DOWN RIG
DIMENSION BETWEEN THE AILERON AND
THE FIXED TRAILING EDGE ON THE
LEFT HAND AND RIGHT HAND WING.
737-MAX  
C27107-1 LOCK SET - FLIGHT SPOILER
ACTUATOR USED TO HOLD THE FLIGHT
SPOILERS IN THE DEPLOYED POSITION
DURINGGROUND MAINTENANCE. LOCKS
ARE DESIGNED TO WITHSTAND FULL
HYDRAULIC SYSTEM PRESSURE.
737-MAX  
C29004-1 DRAIN HOSE - HYDRAULIC RESERVOIR USED TO DRAIN THE STAND BY HYDRAULIC SYSTEM RESERVOIR. 737  
C29006-27 ADAPTER EQUIPMENT - GROUND
SERVICE CONNECTION, HYDRAULIC
POWER USED TO CONNECT A HYDRAULIC
GROUND CART TO THE AIRPLANE
HYDRAULIC SYSTEM - SKYDROL SYSTEM.
737  
C32012-12 REVL/INSTL EQPT - WHEEL RETENTION
NUT, MLG AND NLG USED FOR REMOVAL
AND INSTALLATION OF THE NOSE OR
MAIN LANDING GEAR WHEEL RETENTION
NUT.
737-NG, 737-MAX  
C32015-18 PULLER EQPT - FUSE PIN, MLG FORWARD TRUNNION SUPPORT USED TO REMOVE AND INSTALL FUSE PINS FOR MLG FORWARD TRUNNION SUPPORT. 737-NG, 737-MAX  
C32016-46 RMVL/INSTL EQPT - NLG LOWER SEALS
USED TO REMOVE AND INSTALL THE
NOSE GEAR LOWER SEALS.
737-NG, 737-MAX  
C32017-53 REPLACEMENT EQPT - LWR BEARING
SEALS, MAIN LANDING GEAR. USED TO
REMOVE/INSTALL THE MAIN LANDING
GEAR GLAND SEAL ASSEMBLIES.
737-NG, 737-MAX  
C32021-1 WRENCH SET - RETAINER NUT, REM/
INSTL, ANTI-SKID, TRANSDUCER, MLG
USED TO REMOVE/INSTALL THE ANTISKID
RETAINER NUT.
737-NG, 737-MAX  
C32022-20 THREAD PROTECTOR EQPT - MLG/NLG
AXLE. USED TO PROTECT NOSE
LANDING GEAR AND MAIN LANDING
GEAR AXLE THREADS AND MAIN GEAR
ANTI-SKID TRANSDUCER ASSEMBLY
DURING WHEEL AND BRAKE
INSTALLATION AND REMOVAL.
737-NG, 737-MAX  
C32022-38 THREAD PROTECTOR EQPT - MLG/NLG
AXLE. USED TO PROTECT NOSE
LANDING GEAR AND MAIN LANDING
GEAR AXLE THREADS AND MAIN GEAR
ANTI-SKID TRANSDUCER ASSEMBLY
DURING WHEEL AND BRAKE
INSTALLATION AND REMOVAL.
737-NG, 737-MAX  
C32022-39 THREAD PROTECTOR EQPT - MLG/NLG
AXLE. USED TO PROTECT NOSE
LANDING GEAR AND MAIN LANDING
GEAR AXLE THREADS AND MAIN GEAR
ANTI-SKID TRANSDUCER ASSEMBLY
DURING WHEEL AND BRAKE
INSTALLATION AND REMOVAL.
737-NG, 737-MAX  
C32026-15 DOWNLOCK EQPT - NLG AND MLG USED
TO PREVENT THE RETRACTION OF THE
NOSE AND MAIN LANDING GEAR.
737-NG, 737-MAX  
C32029-45 PIN INSTL/RMVL KIT - MAIN LANDING
GEAR. USED TO REMOVE/INSTALL
VARIOUS MAIN LANDING GEAR PINS
DURING ASSEMBLY/DISASSEMBLY OF
LANDING GEAR.
737-NG, 737-MAX  
C32031-22 REMOVAL/INSTL EQPT - AFT TRUNNION
PIN, MLG. USED TO REMOVE AND
INSTALL THE MAIN LANDING GEAR AFT
TRUNNION PIN.
737-NG, 737-MAX  
C32049-1 OUTRIGGER ASSY - RMVL AND INSTL/
GROUND HANDLING, NLG USED TO AID
IN THE REMOVAL AND INSTALLATION
OF THE 737 NOSE LANDING GEAR AND
IS ALSO USED FOR SHOP AND GENERAL
GROUND HANDLING.
737-NG, 737-MAX  
C32054-1 RMVL/INSTL EQPT - TRUNNION PIN,
NLG USED TO REMOVE AND INSTALL
THE NOSE LANDING GEAR TRUNNION
PINS AND UPPER DRAG STRUT
TRUNNION PINS.
737-MAX  
C35003-10 RETRACTION EQUIPMENT - FIRING
PIN, OXYGEN SYSTEM USED TO DISARM
OXYGEN GENERATORS DURING REMOVAL
& INSTALLATION.
737, 747, 757, 767, 777  
C36001-64 TEST EQUIPMENT - ENGINE BLEED AIR
SYSTEMS USED TO PERFORM
OPERATIONAL OR FUNCTIONAL TEST OF
THE ENGINE BLEED AIR SYSTEM
COMPONENTS.
737-CL  
C36003-23 PRECOOLER RMVL/INSTL EQPT - CFM
LEAP-1B ENGINE REMOVED. USED WITH
A20001 AND J20002 TO REMOVE AND
INSTALL THE PRECOOLER WHEN THE
ENGINE IS REMOVED.
737-MAX  
C36004-1 PRECOOLER REMOVAL AND INSTALLATION EQPT - ENGINE ON. USED TO REMOVE OR INSTALL THE PRECOOLER WITH ENGINE INSTALLED. 737-MAX  
C36005-37 SLING - PRECOOLER. USED TO LIFT
THE PRECOOLER FROM SHIPPING
CONTAINER TO PRECOOLER REMOVAL
AND INSTALLATION EQPT.
737-MAX  
C36006-1 TEST EQUIPMENT - AIR SUPPLY
CONTROL SYSTEM USED TO PERFORM
OPERATIONAL OR FUNCTIONAL TEST OF
THE ENGINE BLEED AIR SYSTEM
COMPONENTS.
737-MAX  
C38001-29 DRAIN MAST PLUG - WASTE WATER
USED TO PLUG THE WASTE WATER
DRAIN MAST (FORWARD AND AFT)
DURING GRAY WATER CLEANING
PROCEDURES.
737, 757, 767, 777  
C38003-1 INSTALLATION ASSY - SLEEVE, WASTE
TANK USED TO PUSH THE SLEEVE OVER
THE WASTE TANK JOINT TO REDUCE
THE RISK OF DAMAGING THE SLEEVE.
737-NG, 737-MAX  
C49006-1 THREAD PROTECTOR EQPT - APU MOUNT
BOLTS USED DURING INSTALLATION
AND REMOVAL OF APU. THE ALIGNMENT
PIN ASSY PREVENTS MISALIGNMENT OF
THE FAILSAFE STRUT SO THAT THE
STRUT CARRIES NO LOAD DURING
INSTALLATION OF THE APU.
737-NG, 737-MAX  
C49007-42 HOIST EQPT - AUXILIARY POWER UNIT USED TO INSTALL AND/OR REMOVAL
THE APU USING CHAIN OR CABLE FISHPOLE HOISTS.
737-NG, 737-MAX  
C49010-50 CRADLE ASSY - AE131-9B APU USED
TO SUPPORT AND TRANSPORT THE
AE131-9B APU DURING MAINTENANCE,
OVERHAUL AND STORAGE IN
CONJUNCTION WITH THE F72950
TRANSPORTATION CART.
737-NG, 737-MAX  
C54018-1 ALIGNMENT EQPT - ECCENTRIC
BUSHING, ENGINE STRUT SLIDE LINK
USED TO DETERMINE AND FIX THE
CENTER-TO-CENTER DISTANCE BETWEEN
THE ENGINE STRUT SIDE LINK
SPHERICAL BEARINGS; TRANSFER THIS
DISTANCE TO THE SIDE LINK
FITTINGS; LOCATE AND INSTALL AN
ECCENTRIC BUSHING IN THE SIDE
LINK FITTINGS.
737-MAX  
C54019-1 SLING EQPT - FUSE PIN R/I, CFM
LEAP-1B, ENGINE ON USED TO UNLOAD
THE UPPER LINK, MID SPAR AND
DIAGONAL BRACE FUSE PINS FOR
REMOVAL AND/OR INSTALLATION
WITHOUT REMOVING THE ENGINE.
737-MAX  
C54021-1 SLING EQPT - FUSE PIN R/I, CFM
LEAP-1B, ENGINE OFF USED TO
UNLOAD AND PRELOAD STRUT WITHOUT
ENGINE DURING DIAGONAL BRACE PIN
AND UPPER LINK REMOVAL AND
INSTALLATION.
737-MAX  
C54022-1 RMVL/INSTL KIT - FUSE PIN USED
FOR REMOVAL OR INSTALLATION OF
FUSE PINS ON CFM LEAP-1B ENGINES
737-MAX  
C55005-19 PIN REMOVAL EQPT - HORIZONTAL
STABILIZER USED TO REMOVE
HORIZONTAL STABILIZER ATTACH
BOLTS.
737  
C57002-15 SLING EQPT - REMOVAL/
INSTALLATION, WINGLET USED FOR
INSTALLATION AND REMOVAL OF
WINGLET. SLING EQPT FOR THE 737
MAX AIRPLANE HAS A LONG AND A
SHORT SLING ASSY. THE LONG SLING
ASSY IS FOR REMOVAL/INSTALLATION
OF THE UPPER AND LOWER BLADES AS
AN ASSEMBLY. THE SHORT SLING ASSY
IS USED FOR REMOVAL/INSTALLATION
OF THE LOWER BLADE ONLY.
737-NG  
C57002-22 SLING EQPT - REMOVAL/INSTALLATION, WINGLET USED FOR INSTALLATION AND REMOVAL OF WINGLET. SLING EQPT FOR THE 737 MAX AIRPLANE HAS A LONG AND A SHORT SLING ASSY. THE LONG SLING ASSY IS FOR REMOVAL/INSTALLATION OF THE UPPER AND LOWER BLADES AS AN ASSEMBLY. THE SHORT SLING ASSY IS USED FOR REMOVAL/INSTALLATION OF THE LOWER BLADE ONLY. 737-MAX  
C57006-1 HOLDING FIXTURE - WINGLET USED TO
SUPPORT WINGLET WHEN REMOVED FROM
THE AIRPLANE.
737-MAX  
C71020-105 BOOTSTRAP EQPT - CFM56-7 ENGINE
USED FOR REMOVAL AND INSTALLATION
OF THE CFM56-7 ENGINE IN
CONJUCTION WITH THE ENGINE CRADLE.
737-NG  
C71022-6 TORQUE WRENCH - ENGINE MOUNT
BOLTS USED FOR THE FINAL TORQUE
OF THE FORWARD AND AFT MOUNT
BOLTS ON THE CFM56-7 ENGINE.
737-NG  
C71029-1 BOOTSTRAP EQPT - CFM LEAP-1B
ENGINE. USED FOR REMOVAL AND
INSTALLATION OF THE CFM LEAP-1B
ENGINE.
737-MAX  
C71031-1 SLING EQPT - FAN COWL,CFM LEAP-1B
ENGINE. USED TO REMOVE AND
INSTALL THE FAN COWL PANELS.
737-MAX  
C71033-1 REMOVAL/INSTALLATION FRAME EQPT -
INLET COWL,CFM LEAP-1B ENGINE.
USED IN CONJUNCTION WITH THE
C20002 BOOM HOIST - GROUND BASED
REMOVAL/INSTALLATION TOOL FOR THE
REMOVAL AND INSTALLATION OF THE
INLET COWL FOR CFM LEAP-1B
ENGINES.
737-MAX  
C71035-1 SAFETY LANYARD - PERSONNEL,
ENGINE MAINTENANCE. USED WITH
CUSTOMER FURNISHED BODY HARNESS
TO PREVENT PERSONNEL FROM BEING
INGESTED INTO FAN INLET DURING
ENGINE RUN-UP AND MAINTENANCE.
737-MAX  
C71036-1 STABILIZER - ENGINE MOUNT, CFM
LEAP-1B USED ON THE CFM LEAP-1B
ENGINE TO RESTRAIN THE FORWARD
AND THE AFT MOUNTS DURING ENGINE
TRANSPORT.
737-MAX  
C71037-1 SUPPORT - ENGINE ANTI-ICE DUCT,
CFM LEAP-1B. USED TO SUPPORT THE
ENGINE ANTI-ICE DUCT DURING
SHIPPING AND STORAGE FOR CFM
LEAP-1B ENGINES.
737-MAX  
C71038-1 REMOVAL/INSTALLATION EQPT -
THRUST LINK, CFM LEAP-1B ENGINE.
USED TO REMOVE AND INSTALL THE
CFM LEAP-1B ENGINE THRUST LINKS.
737-MAX  
C71039-1 ENGINE SLING EQPT - OVERHEAD SHOP HANDLING. USED FOR SHOP HANDLING OF THE CFM LEAP-1B ENGINE OR ENGINE WITH EITHER INLET OR EXHAUST OR BOTH REMOVED. 737-MAX  
C71040-30 TORQUE EQPT - ENGINE MOUNT BOLTS,
CFM LEAP-1B. USED TO TORQUE
ENGINE MOUNT BOLTS ON THE CFM
LEAP-1B ENGINE
737-MAX  
C71041-1 UNLOCK POLE - FAN COWL HOLD OPEN
RODS. USED TO UNLOCK THE LOCKS ON
THE HOLD OPEN RODS AND SPRING
DOOR OPENING SYSTEM.
737-MAX  
C78004-1 LOCKPIN EQPT - THRUST REVERSER
TRANSLATING SLEEVE, CFM56-3
ENGINE USED TO PREVENT THE THRUST
REVERSER TRANSLATING SLEEVE FROM
ACTUATING.
737  
C78005-53 HAND PUMP - OPENING SYSTEM,
THRUST REVERSER USED TO OPEN THE
THRUST REVERSERS AND 787 FAN
COWLS FOR ENGINE MAINTENANCE.
737, 747, 757, 767, 787  
C78009-72 REMOVE/INSTALL TOOL - PRIMARY
EXHAUST ASSYS USED TO REMOVE/
INSTALL THE EXHAUST SLEEVE,
PRIMARY NOZZLE AND PRIMARY PLUG
ASSYS OF THE CFM56-3, CFM56-7 AND
CFM LEAP-1B ENGINES.
737  
C78018-50 SLING EQPT - THRUST REVERSER,
CFM56-7 USED FOR REMOVAL/
INSTALLATION OF THE CFM56-7
THRUST REVERSERS.
737-NG  
C78019-15 HOLD OPEN EQPT - T/R COWL, CFM56-7 ENGINE USED TO HOLD OPEN THRUST REVERSER COWL AT 45 DEGREES DURING ENGINE CHANGE. 737-NG  
C78020-14 LATCHING TOOL - THRUST REVERSER CDUCT
HALVES USED TO HELP CLOSE
THE THRUST REVERSER COWLINGS.
737-NG  
C78023-1 LOCK EQPT - THRUST REVERSER
ACTUATOR, CFM56-7 USED TO HOLD
THRUST REVERSER ACTUATOR ROD IN
THE EXTENDED POSITION TO PREVENT
ACCIDENTAL CLOSING OF THE THRUST
REVERSER COWL.
737-NG  
C78025-30 ACTUATOR INSTALLATION/REMOVAL
TOOL USED TO REMOVAL AND/OR
INSTALL THRUST REVERSER ACTUATORS
FROM THRUST REVERSER ASSEMBLY.
737-MAX  
C78031-1 SLING EQPT - THRUST REVERSER
OPENING,CFM LEAP-1B ENGINE USED
TO MANUALLY OPEN THRUST REVERSER
WITH A FAILED MDOS.
737-NG  
C78032-1 SLING EQPT - THRUST REVERSER, CFM
LEAP-1B ENGINE. USED FOR REMOVAL/
INSTALLATION OF CFM LEAP-1B
THRUST REVERSERS.
737-MAX  
C78033-1 HOLD OPEN EQPT - THRUST REVERSER,
CFM LEAP-1B ENGINE USED TO
SUPPORT THE CFM LEAP-1B THRUST
REVERSERS IN THE OPEN POSITION
DURING ENGINE REMOVAL /
INSTALLATION.
737-MAX  
C78034-1 HOIST EQPT - THRUST REVERSER SLEEVE, CFM LEAP-1B ENGINE USED FOR REMOVAL/INSTALLATION OF CFM LEAP-1B THRUST REVERSER SLEEVES. 737-MAX  
C78035-1 LOCK EQPT - THRUST REVERSER
OPENING ACTUATORS,CFM LEAP-1B
ENGINE USED DURING MAINTENANCE TO
LOCK THE THRUST REVERSER OPENING
ACTUATORS IN THE EXTENDED
POSITION TO PREVENT ACCIDENTAL
CLOSING OF THE THRUST REVERSERS.
THE 15 DEGREE LOCK EQPT IS USED
DURING REMOVAL AND INSTALLATION
OF THE T/R TRANSLATING SLEEVE
ACTUATORS.
737-MAX  
C78035-14 LOCK EQPT - THRUST REVERSER
OPENING ACTUATORS,CFM LEAP-1B
ENGINE USED DURING MAINTENANCE TO
LOCK THE THRUST REVERSER OPENING
ACTUATORS IN THE EXTENDED
POSITION TO PREVENT ACCIDENTAL
CLOSING OF THE THRUST REVERSERS.
THE 15 DEGREE LOCK EQPT IS USED
DURING REMOVAL AND INSTALLATION
OF THE T/R TRANSLATING SLEEVE
ACTUATORS.
737-MAX  
F70199-52 INFLATION TOOL - TIRE USED TO
INFLATE LANDING GEAR TIRES AND TO
CONTROL TIRE PRESSURE. THE TIRE
PRESSURE GAUGE IS USED TO MEASURE
TIRE PRESSURE.
707, 727, 737, 747, 757, 767, 777, 787  
F70200-35 INFLATION TOOL - STRUT USED TO
INFLATE THE LANDING GEAR STRUTS.
707, 727, 737, 747, 757, 767, 777, 787  
F70207-109 KIT - RIGGING PIN USED TO RIG
SYSTEMS AS DEFINED BY THE
AIRPLANE MAINTENANCE MANUALS.
737-NG  
F70207-151 KIT - RIGGING PIN USED TO RIG
SYSTEMS AS DEFINED BY THE
AIRPLANE MAINTENANCE MANUALS.
737-MAX  
F70284-1 WEAR GAGE SET - GROUND POWER PLUG
AND RECEPTACLE USED TO CHECK FOR
EXCESS WEAR ON THE A/P RECEPTACLE
PINS AS NO-GO GAGES. IF THE GAGE
SLIDES ON THE APPLICABLE PIN.
THEN THAT PIN HAS EXCESS WEAR.
THESE GAGES CAN ALSO BE USED TO
CHECK FOR EXCESS WEAR ON T
707, 727, 737, 747, 757, 767, 777, 787  
F71329 LEAKAGE TRACING DEVICE - INTEGRAL
TANK LEAKAGE TEST. USED TO APPLY
A LEAKAGE TRACING MEDIUM UNDER
PRESSURE TO THE EXTERIOR SURFACE
OF THE INTEGRAL TANK AT THE LEAK.
707, 727, 737, 747, 757, 767, 777, 787  
F71336-501 LOCK ASSY - STABILIZER TRIM USED
TO HOLD THE WHEEL ASSY STABILIZER
CONTROL IN A FIXED POSITION TO
PREVENT INJURY FROM STABILIZER,
WHILE WORK IS BEING DONE THROUGH
ACCESS DOOR ON FUSELAGE.
707, 727, 737  
F72735-13 GROUND LOCK ASSY USED AS A SAFETY
LOCK TO PREVENT ACCIDENTAL RETRACTION OF THE LANDING GEAR
DURING GROUND OPERATIONS. GROUND LOCK ASSY USED AS A SAFETY LOCK TO PREVENT ACCIDENTAL RETRACTION OF THE LANDING GEAR DURING GROUND OPERATIONS.
737-CL  
F72790 PROTRACTOR MOUNT ASSY - PILOTS &
COPILOTS CONTROL WHEEL USED IN
CONJUNCTION WITH BUBBLE
PROTRACTOR TO MEASURE ROTATIONAL
MOVEMENT OF THE PILOTS AND
COPILOTS CONTROL WHEEL.
707, 727, 737  
F72928-58 AIR PRESSURE REGULATOR - ELEVATOR
FEEL COMPUTER USED TO PROVIDE AIR
PRESSURE REGULATOR TO SUPPLY
REGULATED AIR & TO MONITOR
PRESSURE AT THE ELEVATOR FEEL
COMPUTER DURING ELEVATOR SYSTEM
FUNCTIONAL TEST.
737-NG, 737-MAX  
F72950-158 AUXILIARY POWER UNIT TRANSPORTATION EQUIP. USED WITH THE APPLICABLE ADAPTER STAND OR THE C49010 CRADLE ASSY TO HOLD THE AUXILIARY POWER UNIT FOR TRANSPORTATION, OVERHAUL & STORAGE. 737  
F72951-1 WATER MANOMETER - TEST EQUIPMENT
USED TO PROVIDE PRESSURE AND
VACUUM RELIEF PROTECTION DURING
HYDROSTATIC TESTING OF CERTAIN
PRESSURE RETAINING COMPONENTS,
STRUCTURES AND SYSTEMS.
707, 727, 737, 747, 757, 767, 777, 787  
F72959-40 SPANNER WRENCH AN STANDARD TYPE
USED FOR NUMEROUS TORQUING
OPERATIONS.
707, 727, 737, 747, 757, 767, 777  
F80033-8 ADAPTER ASSY - WRENCH, HOOK
SPANNER. USED FOR THE REMOVAL AND
INSTALLATION OF THE MAIN LANDING
GEAR SHOCK STRUT GLAND NUT.
737-NG, 737-MAX  
F80049-65 LOCK ASSEMBLY - FLIGHT CONTROLS
USED TO PREVENT ELECTRICAL
CONNECTION AT CONTROL SURFACES
HYDRAULIC MODULE SHUTOFF VALVES
AND FLAP BY-PASS SHUT OFF VALVE.
THEREBY PRECLUDING INADVERTANT
OPERATION OF CONTROL SURFACES AND INJURY TO PERSONNEL.
737  
F80049-66 LOCK ASSEMBLY - FLIGHT CONTROLS
USED TO PREVENT ELECTRICAL
CONNECTION AT CONTROL SURFACES
HYDRAULIC MODULE SHUTOFF VALVES
AND FLAP BY-PASS SHUT OFF VALVE.
THEREBY PRECLUDING INADVERTANT
OPERATION OF CONTROL SURFACES AND INJURY TO PERSONNEL.
737  
F80055-10 TRAMMEL BAR - STABILIZER TRIM ACTUATOR USED TO MEASURE RIGGING POSITIONS ON THE STABILIZER TRIM ACTUATOR DURING FUNCTIONAL TESTING. 737  
F80201-1 DRAIN TOOL - FUEL SUMP USED FOR
COLLECTING FUEL SAMPLE AND/OR
DRAINING SUMPS OF WING AND CENTER
SECTION TANKS.
727, 737  
F80212-30 ADAPTER - RUDDER PEDAL FORCE
CHECK. USED TO CHECK THE FORCE
REQUIRED TO MOVE THE RUDDER
PEDALS.
707, 727, 737, 747, 757, 767, 777, 787  
G12001-60 KIT - RIGGING PIN USED TO RIG ANY SYSTEM COMPLETELY. 747  
G24012-1 HOIST ADAPTER - IDG USED IN CONJUNCTION WITH THE A20001 BOOM
HOIST AND J20002 LOAD POSITIONER OR A LOW-PROFILE TRANSMISSION
JACK FOR REMOVAL AND INSTALLATION  OF THE INTEGRATED DRIVE
GENERATOR(IDG).
747, 757, 767  
G28005-35 CHECK FIXTURE EQUIPMENT - PRESSURE RELIEF VALVE USED TO CHECK THE ACTUATING PRESSURE OF HORIZONTAL STABILIZER FUEL TANK PRESSURE RELIEF VALVES AND WING SURGE TANK PRESSURE RELIEF VALVES. 737, 747, 757, 767, 777  
G32075-16 TEST EQUIPMENT - BRAKE BLEED PORT
USED TO CHECK HYDRAULIC BRAKE
PRESSURE AFTER ANY MAINTENANCE TO
THE MAIN GEAR BRAKING SYSTEM
WHERE A BRAKE LINE IS OPENED OR
ANY COMPONENT IN THE BRAKING
SYSTEM IS REPLACED.
727, 737, 747, 757, 767, 777  
G36035-36 TEST EQPT - PNEUMATIC SYSTEM
HEALTH CHECK USED TO PERFORM THE
PNEUMATIC SYSTEM HEALTH CHECK ON
747-400 AND 767 AIRPLANES WITH
PRATT & WHITNEY AND GE ENGINES.
747, 767  
G38004-17 BLOCKAGE REMOVAL TOOL - VACUUM
LAV SYSTEM USED TO CLEAR
BLOCKAGES IN THE 2 INCH DIA
PLUMBING OF THE VACUUM LAVATORY
SYSTEM. NOT FOR USE ON THE
TOILETS OR THE 4 INCH DIA
LAVATORY SERVICE PLUMBING.
737, 747, 757, 767, 777, 787  
G38006-1 BLOCKAGE REMOVAL EQPT - VACUUM
WASTE SYSTEM USED TO CLEAR
BLOCKAGE BETWEEN THE SERVICE
PANEL AND THE WASTE TANK(S) IN
THE VACUUM WASTE SYSTEM.
737, 747, 757, 767, 777, 787  
G71038-13 UNLOCK POLE EQPT - FAN COWL HOLD
OPEN ROD. USED TO DISENGAGE THE
HOLD OPEN FAN COWL ROD LOCKS.
747, 777, 787  
G71048-1 THREAD PROTECTOR EQPT - ENGINE
MOUNT & THRUST LINK BOLTS USED TO
PROTECT SHOULDER BOLT THREADS AND
BEARING SURFACES DURING ENGINE
MOUNT & THRUST LINK REMOVAL &
INSTALLATION.
747  
G76002-19 PROTRACTOR - THRUST REVERSER
LEVERS, FWD & REV USED FOR FULL
TRAVEL ANGULAR MEASUREMENTS OF
THE FORWARD AND REVERSE THRUST
REVERSER LEVERS.
737, 747, 757, 767, 777  
J07001-25 JACK FITTING - FORWARD BODY. USED
FOR JACKING/LEVELING THE NOSE OF
THE AIRPLANE.
777, 777X  
J07002-1 JACK FITTING - INNER WING USED TO
PROVIDE AUXILIARY JACK POINT AT
WING REAR SPAR, RIB 21, TO
STABILIZE THE AIRPLANE AFTER IT
IS LIFTED.
777  
J20002-67 LOAD POSITIONER - ENGINE
ACCESSORIES. USED IN CONJUNCTION
WITH A BOOM HOIST OR JACK AND
OTHER LRU ADAPTERS TO PROVIDE
HORIZONTAL MOVEMENT. CAN BE USED
IN STANDARD AND INVERTED
POSITIONS.
747, 757, 767, 777, 777X, 787  
J20003-34 PIN SET - RIGGING USED FOR A
SOURCE OF RIGGING PINS FOR ALL
SYSTEMS.
777, 777X  
J20006-24 PERSONNEL EQPT - SHOCK ABSORBING
LNYD, ENGINE/STRUT USED FOR THE
ATTACHMENT OF A SAFETY HARNESS
DURING INSPECTION AND REPAIR OF
THE ENGINE AND STRUT AND IS USED
IN CONJUNCTION WITH CUSTOMER
FURNISHED FULL BODY SAFETY
HARNESS.
777, 777X  
J20009-136 JACKING EQPT - HYDRAULIC
TELESCOPING USED TO REMOVE/
INSTALL AIRPLANE COMPONENTS IN
APPLICATIONS WHERE THE ASSISTANCE
OF A HYDRAULIC JACK IS REQUIRED.
737, 747, 767, 777  
J20009-50 COMPONENT -JACKING EQPT - HYDRAULIC TELESCOPING USED TO REMOVE/ INSTALL AIRPLANE COMPONENTS IN APPLICATIONS WHERE THE ASSISTANCE OF A HYDRAULIC JACK IS REQUIRED. 737, 767, 777  
J24014-24 GFCI TESTER - HYDRAULIC, JETTISON
AND OVERRRIDE PUMPS USED TO
VERIFY CORRECT OPERATION OF
GROUND FAULT INTERRUPT CIRCUIT IN
ELMS-2 (ELECTRICAL LOAD
MANAGEMENT SYSTEM) FOR AC
HYDRAULIC, OVERRIDE AND JETTISON
PUMPS PROTECTION.
777, 777X  
J24016-1 BATTERY INSPECTION GAGE TOOL USED
TO TEST TWO DIFFERENT TYPES OF
BATTERY CONNECTOR POWER CONTACTS
BASED ON THE MANUFACTURERS DESIGN
TO MEET MS25182 REQUIREMENTS.
737, 747, 757, 767, 777, 777X, 787  
J26004-24 TEST EQPT - SQUIB FIRE
EXTINGUISHING SYSTEM USED TO
VERIFY THE REQUIRED VOLTAGE AT
THE APPROPRIATE SQUIB CONNECTOR
UPON DISCHARGE.
777, 777X, 787  
J27005-48 LOCK EQPT - INBD/OUTBD, SPOILER
ACTUATOR USED TO HOLD THE INBOARD
AND OUTBOARD SPOILERS IN THE
DEPLOYED POSITION.
777  
J27011-39 SLING EQPT - INBD T.E. FLAP. USED TO REMOVE/INSTALL INBOARD TRAILING EDGE FLAPS. A SECONDARY HOIST CAN BE USED TO ROTATE FLAP HORIZONTAL TO PREVENT DAMAGE TO TRAILING EDGE PRIOR TO REMOVAL OF SLING FITTINGS. 777  
J27019-1 PIN SET - BYPASS, ELEVATOR PCU USED FOR MANUALLY MOVING THE PCU INTERNAL MODE SELECT VALVE FROM BLOCKING POSITION TO BYPASS POSITION TO ALLOW PCU PISTON MANUAL EXTENSION OR RETRACTION WITH NO HYDRAULIC OR ELECTRIC POWER AT THE PCU. 777  
J27024-66 SLING EQPT - RUDDER, REMOVAL/INSTL USED TO REMOVE AND INSTALL THE RUDDER ASSY. USED ON RUDDERS WITH OR WITHOUT THE RUDDER TAB. RUDDER CAN BE ROTATED BETWEEN HORIZONTAL AND VERTICAL POSITIONS TO ALLOW FOR TRANSITION TO/FROM GROUND HANDLING EQUIPMENT. USED WITH J27001 RUDDER TAB CLAMP ASSY (CUSTOMER FURNISHED) WHEN RUDDER IS REMOVED OR INSTALLED WITH THE RUDDER TAB ATTACHED. 777, 787  
J27028-14 LOCK - RUDDER AND ELEVATOR POWER CONTROL UNIT USED TO HOLD THE RUDDER OR THE ELEVATOR AT FULL RIGHT POSITION DURING REMOVAL OR INSTL OF A RUDDER POWER CONTROL UNIT (PCU) OR OF AN ELEVATOR PCU. 777  
J27079-38 ELEVATOR
FREEPLAY USED TO PERFORM THE
FREEPLAY INSPECTION OF THE POWER
CONTROL UNITS FOR THE ELEVATOR.
747, 767, 777, 777X, 787  
J28013-1 FUEL DRAIN SUMP.
USED TO DRAIN FUEL FROM MAIN TANK
SUMPS.
737, 767, 777  
J32001-68 BRAKE PEDAL USED
TO MEASURE THE LOAD APPLIED AND
THE ANGLE OF TRAVEL OF THE BRAKE
PEDALS DURING SYSTEM TEST OF THE
HYDRAULIC BRAKE SYSTEM.
737, 747, 757, 767, 777, 777X, 787  
J32007-1 AXLE & THREAD,
NLG USED TO PROTECT THE THREADS
DURING NOSE LANDING GEAR WHEEL
REMOVAL AND INSTALLATION. THE
TOOL ALSO PROTECTS THE AXLE WHILE
THE WHEEL IS REMOVED.
777, 777X  
J32011-3 NLG & MLG USED TO
PREVENT ACCIDENTAL RETRACTION OF
MAIN & NOSE LANDING GEAR DURING
GROUND OPERATIONS. ALSO USED TO
SUPPORT DISPATCH OF A/P WITH
LANDING GEAR FIXED IN THE DOWN &
LOCKED POSITION.
777, 777X, 787  
J32011-7 NLG & MLG USED TO
PREVENT ACCIDENTAL RETRACTION OF
MAIN & NOSE LANDING GEAR DURING
GROUND OPERATIONS. ALSO USED TO
SUPPORT DISPATCH OF A/P WITH
LANDING GEAR FIXED IN THE DOWN &
LOCKED POSITION.
777, 777X, 787  
J32012-18 BRAKE, MAIN LANDING
GEAR. USED IN CONJUNCTION WITH
THE J32031 PROTECTOR EQPT TO PULL
THE MAIN LANDING GEAR BRAKES.
767, 777X, 787  
J32028-1 MLG AND NLG DOORS
USED TO LOCK THE DOOR RELEASE/
SAFETY VALVE(S), PREVENTING
ACCIDENTAL OPERATION OF THE
LANDING GEAR DOOR ACTUATOR(S).
777,777X  
J32028-2 COMPONENT 777, 777X  
J32028-3 COMPONENT 777, 777X  
J32031-12 AXLE, MAIN
LANDING GEAR USED TO PROTECT THE
LANDING GEAR AXLE, THE LANDING
GEAR AXLE EXTERNAL THREADS AND
THE TPIS SENSOR DURING THE
REMOVAL/INSTALLATION OF THE WHEEL
AND BRAKE ASSEMBLY.
767, 777, 777X, 787  
J32032-22 WHEEL RETENTION
NUT, MLG USED TO REMOVE AND
INSTALL THE MAIN LANDING GEAR
WHEEL RETENTION NUT FOR 777,767 &
787 AND NLG & MLG FOR 747.
747, 767, 777, 777X, 787  
J32052-1 EXTENSION BAR - FUNCTIONAL TEST, NLG STEERING USED TO MANUALLY TURN THE NOSE LANDING GEAR DURING STEERING FUNCTIONAL TEST. 777, 787  
J32054-92 RETAINER EQPT - MLG/NLG TORSION LINK USED TO SECURE THE UNPRESSURIZED INNER CYLINDERS OF THE MLG/NLG SHOCK STRUTS DURING HOISTING AND TRANSPORTATION. 777  
J32060-1 OLEO STRUT, MLG/NLG
USED TO HOLD THE OIL FILL VALUE
OPEN IN ORDER TO DRAIN OIL FROM
THE MAIN OR NOSE LANDING GEAR.
USE ONLY ON A COMPLETELY
DISCHARGED GEAR.
737, 757, 767, 787  
J32071-10 FWD & AFT LOCK
LINK, RETR TAIL SKID USED TO
RESTRAIN THE MOVEMENT OF THE
FORWARD AND AFT LOCK LINK ON THE
RETRACTABLE TAIL SKID.
777, 777X  
J34002-19 ANGLE OF ATTACK
USED TO ACCURATELY MEASURE AOA
SENSOR DEFLECTION AND FOR
PERIODIC ALIGNMENT.
737, 747, 757, 767, 777  
J46002-17 ARINC 600 STYLE CONNECTORS USED
TO FACILITATE TESTING &
TROUBLESHOOTING OF OPTICAL FIBER
AND TERMINI IN ARINC 600 STYLE
AIRPLANE CONNECTORS.
737, 767, 777, 777X  
J49006-67 CRADLE - APU USED IN CONJUNCTION WITH THE JACKING EQUIPMENT HYDRAULIC TELESCOPING AND A CUSTOMER FURNISHED SCISSOR LIFT TABLE FOR REMOVAL AND INSTALLATION OF THE APU. ALSO USED WITH APU TRANSPORTATION DOLLY TO TRANSPORT THE APU. 777  
J52011-1 CARGO DOORS USED
TO PREVENT PERSONNEL FROM FALLING
OVERBOARD WHEN CARGO DOORS ARE
OPEN DURING AIRCRAFT MAINTENANCE.
777, 777X  
J52020-1 BULK CARGO DOOR USED TO
PREVENT PERSONS FROM ACCIDENTALLY
FALLING FROM BULK CARGO DOOR
OPENING.
777, 777X  
J52029-57 SQUIB, OVERWING EXIT
USED TO VERIFY SQUIB FIRING
CURRENT ON ESCAPE SLIDE, EPAS
(EMERGENCY POWER ASSIST SYSTEM),
AND SARD (SPOILER AUXILIARY
RETRACT DEVICE) ON THE OVERWING
EXIT SYSTEM.
777, 777X  
J55006-114 TORQUE EQPT - VERTICAL FIN BOLTS. USED TO TORQUE LARGE TENSION BOLTS ON THE FIN TO SECTION 48 BODY JOIN. (TORQUE NOT TO EXCEED 2,500 FT-LBS). ALSO USED TO REMOVE PREVIOUSLY INSTALLED TENSION BOLTS. USED IN CONJUNCTION W/ J53001 AND J53003 MAINT PLATFORM. 777  
J71001-66 INLET COWL USED
FOR REMOVAL/INSTALLATION OF INLET
ASSY ON THE GE, P/W & RR 777
ENGINES AND GE & RR 787 ENGINES.
747, 777, 777X, 787  
J71002-95 ENGINE MOUNT BOLT,
GE90. USED TO TORQUE ENGINE BOLTS
ON GE90 THE ENGINE.
777  
J71032-15 PROTECTIVE, ENGINE INLET
GE, PW & RR USED TO PROTECT THE
INLET COWL IF PERSONNEL ARE
REQUIRED TO BE IN THIS AREA.
787  
J78004-123 GE90 FAN THRUST
REVERSER USED FOR REMOVAL/
INSTALLATION OF THE FAN THRUST
REVERSERS.
777  
J78007-85 EXH SLEEVE &
PLUG, PW/RR ENGINES CRADLE USED
IN CONJUNCTION W/A20001 BOOM
HOIST OR SIMILAR HOIST TO RMV/
INSTL PW, RR & GE ENGINE EXHAUST
SLEEVE & FORWARD PLUG ON A/P. MAY
ALSO BE USED FOR ENGINE BUILD UP.
SLING IN CONJUNCTION WITH AN
OVERHEAD LIFT, IS USED FOR REMOVE/
INSTALL OFF WING.
777, 787  
K05001-1 EXTENSION CABLE - BRAKE RELEASE,
MLG USED TO RELEASE THE FRICTION
BRAKE MECHANISM OF A STUCK BRAKE
CAUSED BY AN UNLIKELY ELECTRICAL
SYSTEM FAULT. CABLE CONNECTS
BETWEEN A FUNCTIONING BRAKES WIRE
BUNDLE PLUG CONNECTOR AND THE
STUCK BRAKES RECEPTACLE
CONNECTOR. CABLE CAN ALSO BE USED
TO ISOLATE WIRING FAULTS FROM
EBAC AND EBPSU EQUIPMENT FAILURES
787  
K10008-23 PROTECTIVE PLUG EQPT - ENGINE
EXHAUST, GE GENX USED TO PROTECT
THE GE ENGINE FROM FOREIGN
OBJECTS WHILE THE AIRPLANE IS
PARKED
787  
K10011-1 PROTECTIVE COVER - ENGINE INLET,
RR USED TO PROTECT THE RR ENGINE
FROM FOREIGN OBJECTS WHILE THE
AIRPLANE IS PARKED
787  
K10012-14 PROTECTIVE PLUG EQPT - ENGINE
EXHAUST, RR USED TO PROTECT THE
RR ENGINE FROM FOREIGN OBJECTS
WHILE THE AIRPLANE IS PARKED
787  
K10013-15 PROTECTIVE PLUG EQPT - THRUST
REVERSER EXHAUST DUCT, RR USED TO
PROTECT THE RR ENGINE FROM
FOREIGN OBJECTS WHILE THE
AIRPLANE IS PARKED
787  
K20001-64 HOIST - FWD EE BAY LRUS. IS USED
TO PROVIDE A MEANS TO LIFT THE
MAIN BATTERY, THE AUTO
TRANSFORMER AND OTHER LINE
REPLACABLE UNITS THROUGH THE
FORWARD ELECTRONIC EQUIPMENT BAY
HATCH.
787  
K20002-25 PERSONNEL EQPT - SHOCK ABSORBING
LANYARD, ENGINE/STRUT USED TO
PROVIDE FALL PROTECTION FOR
PERSONNEL WORKING IN THE ENGINE
AND STRUT AREAS OF THE AIRPLANE
787  
K20004-60 PERSONNEL EQPT - SHOCK ABSORBING
LANYARD, HORIZONTAL STABILIZER
USED TO PROVIDE FALL PROTECTION
FOR PERSONNEL WORKING ON THE
HORIZONTAL STABILIZERS OF THE
AIRPLANE.
787  
K20008-55 HOIST - AFT E/E BAY LRUS USED TO
TRANSFER THE LRUS THROUGH THE AFT
E/E BAY HATCH
787  
K20009-14 PIN SET - RIGGING USED TO RIG ALL
787 AIRPLANE SYSTEMS EXCEPT
ENGINES. USED IN FLIGHT CONTROLS
TO RIG RUDDER, ELEVATOR AND
LATERAL CONTROL SYSTEMS. USED IN
LANDING GEAR TO RIG MLG AND NLG
DOOR OPERATED PROXIMITY SENSOR
MECHANISMS AND THE NLG SHUT-OFF
VALVE
787  
K20014-1 WRENCH - BATTERY ENCLOSURE, EEBAY
USED TO HOLD THE NUTS IN
PLACE ON THE MAIN AND APU BATTERY
ENCLOSURE DOOR
787  
K21003-67 INSTALLATION/REMOVAL EQPT - PECS
COOLING PUMP USED TO REMOVE AND
INSTALL THE POWER ELECTRONICS
COOLING SYSTEM (PECS) AND
INTEGRATED COOLING SYSTEM (ICS)
PUMPS. THE PUMPS ARE LOCATED IN
THE LEFT AND RIGHT WHEEL WELLS
787  
K21006-53 JACK ADAPTER - AIR COMPRESSOR, AC
PACK USED TO SUPPORT THE REMOVAL
OF THE OUTBOARD AND INBOARD CABIN
AIR COMPRESSORS FROM THE AIR
CONDITIONING PACKAGES ON THE LEFT
AND RIGHT HAND SIDE OF THE
AIRPLANE. USE IN CONJUNCTION WITH
K21011 AND A71015.
787  
K21010-54 RAM AIR FAN, AC PACK - JACK
ADAPTER. USED AS A CRADLE THAT
SUPPORTS THE REMOVAL OF THE RAM
AIR FAN (RAF) FROM THE AIR
CONDITIONING (AC) PACKAGES ON
EACH LEFT AND RIGHT HAND SIDE OF
THE AIRPLANE. CAN BE ATTACHED TO
THE J20009 JACK OR TO A71015 JACK
WITH K21011 ADAPTER
787  
K21011-62 ADAPTER EQPT - ADJUSTABLE ANGLE,
JACK USED TO ACCOMMODATE REQUIRED
MOTIONS FOR REMOVAL OF AC PACK
COMPONENTS, MOVE LATERALLY (SIDE
TO SIDE, FORWARD AND BACK, OR ANY
COMBINATION OF THE 2). TOOL IS
USED WITH AND MUST BE SECURED TO
A71015 JACK.
787  
K21016-129 KIT, ADAPTER - LIQUID COOLING
SYSTEM SERVICE USED FOR INTERFACE
BETWEEN THE POWER ELECTRONICS
COOLING SYSTEM (PECS), INTEGRATED
COOLING SYSTEM (ICS), FORWARD
CARGO AIR CONDITIONING (FCAC),
HIGH VOLTAGE DIRECT CURRENT MOTOR
CONTROLLER (HVDC MC),
SUPPLEMENTAL COOLING UNIT (SCU),
CARGO REFRIGERATION UNIT (CRU),
GALLEY COOLING UNIT (GCU) AND
INTEGRATED COOLING SYSTEM
SUPPLEMENTAL COOLING UNIT MOTOR
CONTROLLER (ICS SCU MC) AND
COOLANT TOP OFF PACK (CTOP) OR
COOLANT SERVICE CART (CSC)
787  
K21016-130 KIT, ADAPTER - LIQUID COOLING
SYSTEM SERVICE USED FOR INTERFACE
BETWEEN THE POWER ELECTRONICS
COOLING SYSTEM (PECS), INTEGRATED
COOLING SYSTEM (ICS), FORWARD
CARGO AIR CONDITIONING (FCAC),
HIGH VOLTAGE DIRECT CURRENT MOTOR
CONTROLLER (HVDC MC),
SUPPLEMENTAL COOLING UNIT (SCU),
CARGO REFRIGERATION UNIT (CRU),
GALLEY COOLING UNIT (GCU) AND
INTEGRATED COOLING SYSTEM
SUPPLEMENTAL COOLING UNIT MOTOR
CONTROLLER (ICS SCU MC) AND
COOLANT TOP OFF PACK (CTOP) OR
COOLANT SERVICE CART (CSC)
787  
K21018-1 DISPATCH EQPT - BYPASS ASSY, GCU
& SCU USED TO BYPASS, OR JUMPER,
ICS (INTEGRATED COOLING SYSTEM),
GCUS (GALLEY COOLING UNITS) AND
SCUS (SUPPLIMENTAL COOLING UNITS)
WHEN THEY LEAK. IN ADDITION, THE
EQUIPMENT IS USED TO PLUG THE
LRUS (LINE REPLACEABLE UNITS)
FROM THE PECS (POWERED ELECTRONIC
COOLING SYSTEM) CONNECTING TO THE
SCU WHEN THAT SCU LEAKS
787  
K21024-1 DISPATCH DEACTIVATION KIT - PPRV
USED TO DISABLE INOPERATIVE
POSITIVE PRESSURE RELIEF VALVE
DURING DISPATCH DEVIATION.
787  
K24001-1 HOIST ADAPTER ASSY - VFSG (GE AND
RR) AND ASG THE ADAPTER ADJUSTER
MATED WITH THE RR VFSG ADAPTERS
IS USED IN CONJUNCTION WITH A
CUSTOMER-FURNISHED LOW-PROFILE
TRANSMISSION JACK FOR ROLLS-ROYCE
TRENT 1000 VARIABLE FREQUENCY
STARTER GENERATOR (VFSG) REMOVAL/
INSTALLATION. MATED WITH THE GE
VFSG ADAPTERS, IT IS USED IN
CONJUNCTION WITH THE A20001 BOOM
HOIST AND THE J20002 LOAD
POSITIONER FOR GE GENX-1B
VARIABLE FREQUENCY STARTER
GENERATOR (VFSG) REMOVAL/
INSTALLATION. MATED WITH THE ASG
ADAPTERS, IT IS USED IN
CONJUNCTION WITH THE J20009
JACKING EQPT AND A CUSTOMERFURNISHED
SCISSOR LIFT PLATFORM
FOR APU STARTER GENERATOR
(ASG)REMOVAL/INSTALLATION
787  
K24001-114 HOIST ADAPTER ASSY - VFSG (GE AND
RR) AND ASG THE ADAPTER ADJUSTER
MATED WITH THE RR VFSG ADAPTERS
IS USED IN CONJUNCTION WITH A
CUSTOMER-FURNISHED LOW-PROFILE
TRANSMISSION JACK FOR ROLLS-ROYCE
TRENT 1000 VARIABLE FREQUENCY
STARTER GENERATOR (VFSG) REMOVAL/
INSTALLATION. MATED WITH THE GE
VFSG ADAPTERS, IT IS USED IN
CONJUNCTION WITH THE A20001 BOOM
HOIST AND THE J20002 LOAD
POSITIONER FOR GE GENX-1B
VARIABLE FREQUENCY STARTER
GENERATOR (VFSG) REMOVAL/
INSTALLATION. MATED WITH THE ASG
ADAPTERS, IT IS USED IN
CONJUNCTION WITH THE J20009
JACKING EQPT AND A CUSTOMERFURNISHED
SCISSOR LIFT PLATFORM
FOR APU STARTER GENERATOR
(ASG)REMOVAL/INSTALLATION
787  
K24001-118 HOIST ADAPTER ASSY - VFSG (GE AND
RR) AND ASG THE ADAPTER ADJUSTER
MATED WITH THE RR VFSG ADAPTERS
IS USED IN CONJUNCTION WITH A
CUSTOMER-FURNISHED LOW-PROFILE
TRANSMISSION JACK FOR ROLLS-ROYCE
TRENT 1000 VARIABLE FREQUENCY
STARTER GENERATOR (VFSG) REMOVAL/
INSTALLATION. MATED WITH THE GE
VFSG ADAPTERS, IT IS USED IN
CONJUNCTION WITH THE A20001 BOOM
HOIST AND THE J20002 LOAD
POSITIONER FOR GE GENX-1B
VARIABLE FREQUENCY STARTER
GENERATOR (VFSG) REMOVAL/
INSTALLATION. MATED WITH THE ASG
ADAPTERS, IT IS USED IN
CONJUNCTION WITH THE J20009
JACKING EQPT AND A CUSTOMERFURNISHED
SCISSOR LIFT PLATFORM
FOR APU STARTER GENERATOR
(ASG)REMOVAL/INSTALLATION
787  
K24002-1 DISPATCH EQPT - MOTOR CONTROLLERS
CONSISTS OF 4 DUMMY BOXES TO BE
INSTALLED IN PLACE OF THE A/P
MOTOR CONTROLLERS (CMSC'S, RFMC
AND FPMC)IN THE P700/P800 PANELS,
SO THAT THE AIRCRAFT CAN BE
DISPATCHED W/ THE MOTOR
CONTROLLERS REMOVED.
787  
K24002-2 DISPATCH EQPT - MOTOR CONTROLLERS
CONSISTS OF 4 DUMMY BOXES TO BE
INSTALLED IN PLACE OF THE A/P
MOTOR CONTROLLERS (CMSC'S, RFMC
AND FPMC)IN THE P700/P800 PANELS,
SO THAT THE AIRCRAFT CAN BE
DISPATCHED W/ THE MOTOR
CONTROLLERS REMOVED.
787  
K24012-1 DISPATCH KIT - APU STARTER
GENERATOR (ASG) USED TO PREPARE
FOR FLIGHT WITH ONE ASG REMOVED
787  
K25001-1 LEVER - STOWAGE BIN RELEASE USED
TO OPEN THE STOW BIN LATCHES ON
THE 787 IN CASE OF A LATCH LEVER
FAILURE
787  
K26001-23 TEST EQUIPMENT - FIRE EXT TUBING, CARGO COMPARTMENT USED TO PERFORM FLOW AND PRESSURE TESTS ON THE 787 FORWARD AND AFT CARGO COMPARTMENT FIRE EXTINGUISHING SYSTEM'S TUBING. MAXIMUM OPERATING PRESSURE IS 100 PSIG. 787  
K27002-85 ADAPTER EQPT - TE GEARED ROTARY ACTUATOR, REMOVAL/INSTALLATION USED IN CONJUNCTION WITH THE A20001 BOOM HOIST, THE J20002 LOAD POSITIONER AND A CUSTOMER FURNISHED SCISSOR LIFT(OPTIONAL) FOR REMOVAL/INSTALLATION OF THE 787 TE GEARED ROTARY ACTUATORS. 787  
K27004-156 HOIST EQUIPMENT - REMOVAL AND
INSTALLATION, RUDDER PCU. USED TO
REMOVE AND INSTALL THE THREE
RUDDER POWER CONTROL UNITS (PCU)
IN CONJUNCTION WITH A CUSTOMER
FURNISHED FISHPOLE HOIST.
787  
K27011-32 DISPATCH EQPT - HYDRAULIC SPOILER
ACTUATORS USED TO HOLD THE
INBOARD AND OUTBOARD HYDRAULIC
POWERED SPOILERS IN THE DISPATCH
DEPLOYED POSITION.
787  
K27011-33 DISPATCH EQPT - HYDRAULIC SPOILER
ACTUATORS USED TO HOLD THE
INBOARD AND OUTBOARD HYDRAULIC
POWERED SPOILERS IN THE DISPATCH
DEPLOYED POSITION.
787  
K27011-47 DISPATCH EQPT - HYDRAULIC SPOILER
ACTUATORS USED TO HOLD THE
INBOARD AND OUTBOARD HYDRAULIC
POWERED SPOILERS IN THE DISPATCH
DEPLOYED POSITION.
787  
K27013-1 ELECTRICAL COVERS - LE SLATS, TE
FLAPS, FLAPERONS COVERS
ELECTRICAL CONNECTORS TO PREVENT
INADVERTENT POWERING OF FLIGHT
CONTROL SURFACES. COVERS EQPT & A/
P WIRING CONNECTORS AFTER
DISCONNECTION. USED AT FLAP/SLAT
HYDRAULIC CONTROL MODULE, FLAP/
SLAT ELECTRIC MOTOR CONTROL UNITS
AND FLAPERON MANIFOLD MODULES.
787  
K27014-38 GAP GAGE EQPT - SPOILER TO FLAP
CLEARANCE USED TO SET THE GAP
BETWEEN SPOILERS #1 THRU 14 TO
FLAP SURFACE.
787  
K27017-46 LOCK EQUIPMENT - SPOILER
HYDRAULIC ACTUATORS USED TO HOLD
THE INBOARD AND OUTBOARD SPOILER
HYDRAULIC ACTUATORS IN THE
DEPLOYED POSITION.
787  
K27021-1 REMOVAL/INSTALLATION EQPT -
HORIZONTAL STABILIZER TRIM
ACTUATOR USED FOR REMOVAL AND
INSTALLATION OF HORIZONTAL
STABILIZER TRIM ACTUATOR
787  
K27038-36 COMPONENT - LOCK - RUDDER PCU USED TO HOLD
THE RUDDER AT THE FULL RIGHT
POSITION DURING INSTALLATION OR
REMOVAL OF A RUDDER POWER UNIT
(PCU). LOCKS MUST BE INSTALLED ON
BOTH REMAINING RUDDER PCUS.
787  
K27040-1 CLAMP EQPT - DRIVE SHAFTS, LE SLATS & TE FLAPS USED TO PREVENT INADVERTENT MOVEMENT OF THE LEADING EDGE SLATS AND TRAILING EDGE FLAP DRIVE SYSTEMS. USED ONLY OUTBOARD OF DISCONNECTED LOCATION IF A TORQUE TUBE IS EXPOSED. 787  
K27041-69 DOLLY - HORIZONTAL STABILIZER
TRIM ACTUATOR USED TO SUPPORT
HORIZONTAL STABILIZER TRIM
ACTUATOR (HSTA) FOR STORAGE AND
TRANSPORT.
787  
K27046-42 LOCK EQPT - ELEVATOR PCU. USED TO
HOLD THE ELEVATOR IN THE FULL UP
POSITION DURING REMOVAL,
INSTALLATION OR MAINTENANCE OF AN
ELEVATOR PCU.
787  
K27046-51 LOCK EQPT - ELEVATOR PCU. USED TO
HOLD THE ELEVATOR IN THE FULL UP
POSITION DURING REMOVAL,
INSTALLATION OR MAINTENANCE OF AN
ELEVATOR PCU.
787  
K27048-1 DISPATCH EQUIPMENT - HORIZONTAL
STABILIZER TRIM ACTUATOR USED FOR
DISPATCH WHEN ONE OF THE TWO
STABILIZER TRIM SYSTEM CHANNELS
IS INOPERATIVE BEFORE FLIGHT
787  
K27050-14 RIGGING EQPT - AILERON AND
FLAPERON USED TO COMPARE THE
TRAILING EDGE OF THE AILERON TO
THE FUEL JETTISON PANEL AND
COMPARE THE TRAILING EDGE OF THE
FLAPERON TO THE INBOARD FLAP.
787  
K27051-10 MEASURING TOOL - EMA POSITION,
SPOILER USED TO MEASURE THE ROD
EXTENSION OF THE ELECTRIC MOTOR
ACTUATOR (EMA) AT THE SPOILER
LOCATIONS 4, 5, 10 AND 11.
787  
K27056-177 REMOVAL/INSTALLATION EQPT - ELEVATOR PCU USED TO REMOVE AND INSTALL THE ELEVATOR PCU. 787  
K27059-18 DISPATCH EQUIPMENT - SPOILER
ELECTRO MECHANICAL ACTUATOR USED
FOR DISPATCH OF AN AIRPLANE IN
THE EVENT OF A SPOILER ELECTRO
MECHANICAL ACTUATOR (SEMA)
INTERNAL SHEAROUT FOLLOWING A
FAILURE EVENT AND THE SEMA CANNOT
BE REPLACED.
787  
K28001-1 SPANNER WRENCH - FUEL SUMP DRAIN
VALVE. USED TO REMOVE OR INSTALL
THE MAIN FUEL TANK AND SURGE FUEL
TANK SUMP DRAIN VALVE INSERTS.
787  
K28002-15 DRAIN FITTING - FUEL SYSTEM USED
FOR DRAINING FUEL FROM THE LEFT
AND RIGHT HAND CENTER, MAIN AND
SURGE FUEL TANKS THROUGH THE SUMP
DRAIN VALVES.
787  
K32002-1 PROTECTOR EQPT - AXLE & THREAD,
NLG USED TO PROTECT THREADS
DURING NOSE LANDING GEAR WHEEL
REMOVAL AND INSTALLATION AND ALSO
PROTECTS AXLE WHILE THE WHEEL IS
REMOVED.
787  
K32021-1 DISPATCH EQPT - BRAKE / EBA
CONNECTOR COVERS USED TO PROTECT
DISCONNECTED ELECTRICAL
COONNECTORS ON ELECTRIC BRAKE AND
ELECTRIC BRAKE ACTUATORS AND WIRE
BUNDLES TO ALLOW DISPATCH OF AN
AIRPLANE WITH INOPERATIVE BRAKES
AND OR ACTUATORS, PER MMEL AND
DDG GUIDELINES.
787  
K32022-1 WRENCH - NLG WHEEL RETENTION NUT
USED TO REMOVE AND INSTALL THE
787 NLG WHEEL RETENTION NUT
787  
K32036-1 DISPATCH EQPT - AXLE RDC
CONNECTOR COVERS USED TO SECURE &
PROTECT THE PLUG CONNECTOR OF THE
AIRPLANE WIRING BUNDLE INSIDE THE
MLG/NLG AXLE WHEN THE AIRPLANE IS
DISPATCHED WITH A MISSING MLG OR
NLG AXLE RDC. THE EQUIPMENT
MOUNTS IN THE SAME PLACE AS THE
NLG AXLE RDC, THE MLG AXLE RDC,
OR THE MLG AXLE RDC S MOUNTING
ADAPTER.
787  
K32036-21 DISPATCH EQPT - AXLE RDC
CONNECTOR COVERS USED TO SECURE &
PROTECT THE PLUG CONNECTOR OF THE
AIRPLANE WIRING BUNDLE INSIDE THE
MLG/NLG AXLE WHEN THE AIRPLANE IS
DISPATCHED WITH A MISSING MLG OR
NLG AXLE RDC. THE EQUIPMENT
MOUNTS IN THE SAME PLACE AS THE
NLG AXLE RDC, THE MLG AXLE RDC,
OR THE MLG AXLE RDC S MOUNTING
ADAPTER.
787  
K32037-1 PROTECTOR EQPT - AXLE, MAIN
LANDING GEAR USED TO PROTECT THE
LANDING GEAR AXLE AND THE LANDING
GEAR AXLE EXTERNAL THREADS DURING
THE REMOVAL AND INSTALLATION OF
THE WHEEL AND BRAKE ASSEMBLY
787  
K38002-1 DISPATCH PLUG - VACUUM WASTE
TOILET BOWL USED TO PLUG THE
TOILET BOWL WHEN THE AIRPLANE IS
DISPATCHED WITH A FLUSH VALVE
STUCK IN THE OPEN POSITION.
787  
K42004-1 JUMPER CABLE - POWER, R-CCR
CABINET USED TO PROVIDE TEMPORARY
POWER TO THE RIGHT CCR WHEN THE
LEFT CCR IS INOPERABLE OR
UNAVAILABLE.
787  
K49001-7 THREAD PROTECTOR EQPT- APU
RETENTION BOLTS USED TO PROTECT
BOLT THREADS DURING INSTALLATION
AND REMOVAL OF APU
787  
K52002-133 BARRIER - PASSENGER ENTRY DOORS.
USED TO PREVENT MAINTENANCE
PERSONNEL FROM ACCIDENTALLY
FALLING FROM PASSENGER ENTRY
DOORS DURING MAINTENANCE
PROCEDURES
787  
K52016-1 SAFETY BARRIER - CARGO DOORS USED
TO PREVENT PERSONNEL FROM FALLING
OVERBOARD WHEN THE CARGO DOORS
ARE OPEN DURING AIRCRAFT
MAINTENANCE.
787  
K52030-1 ADAPTER - MANUAL DRIVE, LCD USED
TO MANUALLY OPEN THE FWD AND AFT
LARGE CARGO DOORS. THE SPLINE ON
THE ADAPTER FITS INTO THE SPLINED
HOLE OF THE LATCH CAMS
787  
K53003-51 LADDER EQUIPMENT - EMPENNAGE
ACCESS, VERTICAL FIN USED TO
PROVIDE ACCESS TO THE VERTICAL
FIN ACCESS DOOR AND THE LEFT AND
RIGHT EMCUS INSIDE THE EMPENNAGE
787  
K55002-45 LOCK ASSY - HORIZONTAL STABILIZER
THE LOCK ASSY IS USED TO LOCK THE
HORIZONTAL STABILIZER DURING
REMOVAL AND INSTALLATION OF THE
TRIM ACTUATOR. THE TEST ASSY IS
USED TO PERFORM FREEPLAY CHECK ON
THE BALLSCREW OF THE HORIZONTAL
STABILIZER.
787  
K55006-73 REACTION FIXTURE EQPT - TORQUE
TOOL USED TO HOLD THE E-RAD 2000
VTS (TORQUE WRENCH) AND LOAD
MASTER 3300 IN PLACE WHILE
MECHANICS TORQUE THE I-BOLT NUTS
THAT INSTALL/HOLD THE VERTICAL
FIN IN PLACE.
787  
K55006-75 REACTION FIXTURE EQPT - TORQUE
TOOL USED TO HOLD THE E-RAD 2000
VTS (TORQUE WRENCH) AND LOAD
MASTER 3300 IN PLACE WHILE
MECHANICS TORQUE THE I-BOLT NUTS
THAT INSTALL/HOLD THE VERTICAL
FIN IN PLACE.
787  
K55008-150 MAINTENANCE PLATFORM - VERTICAL FIN, TENSION BOLTS USED TO INSPECT AND TO REMOVE/INSTALL THE 787 VERTICAL FIN TENSION BOLTS. 787  
K71002-148 ENGINE CHANGE KIT - RR USED TO
REMOVE AND INSTALL THE ROLLS
ROYCE TRENT 1000 ENGINES.
787  
K71006-20 HOIST EQPT - ENGINE MOUNTS AND
THRUST LINKS USED TO REMOVE AND
INSTALL THE FWD AND AFT ENGINE
MOUNT ASSEMBLIES AND THE AFT
ENGINE MOUNT ASSY COMBINED WITH
THRUST LINKS.
787  
K71012-1 ADAPTER - HAND PUMP / PDOS USED
TO CONNECT A HAND PUMP TO THE FAN
COWL PDOS INTERFACE FOR MANUAL
OPENING OF THE FAN COWLS.
787  
K78006-1 LOCK - THRUST REVERSER ISOLATION
VALVE (GROUND) USED TO PREVENT
THRUST REVERSER OPERATION ON
GROUND DURING MAINTENANCE AND
BYPASS MODE.
787  
R/C-AOAC-2 A FLAME RESISTANT PROTECTIVE COVER THAT MINIMIZES POTENTIAL VANE DAMAGE ON THE ANGLE OF ATTACK (AOA) SENSOR.   737-NG, 757, 767, 777, 787  
SE27-0001 CONTROL WHEEL STRAIGHTEDGE USED
TO ALIGN BOTH CONTROL WHEELS TO A
COMMON PLANE, AND TO HOLD THEM IN A NEUTRAL POSITION.
737  
ST6760A-1 PROBE - LEAK, ULTRASONIC USED TO
DETECT AIR LEAKS. USED WITH
VACUUM BAG ATTACHMENTS # ST9999-
VBA-201/-301, ST9999-VB & ST6760
ALL  

 

 

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