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Boeing Tooling
| Produkt Nr. | Beschreibung | Flugzeugtyp | |
|---|---|---|---|
| 14R02-32T | SLEEVE | #NV | |
| 2ME65B00002 | WRENCH | #NV | |
| 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 | |
| 2MIT65B08802-1 | HOLDING FIXTURE | #NV | |
| 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 | |
| 6TE65B00114 | TEST FIXTURE | #NV | |
| A07001-11 | JACK ADAPTER | B767 | |
| A07003-1 | JACK ADAPTER | B767 | |
| 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 | |
| A10002-7 | REMOVAL/INSTALLATION TOOL | B767 | |
| 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 | |
| A20001-83 | HOIST ARM ASSY. | B767 | |
| A20001-97 | ADJUSTING RING | B767 | |
| A21010-203 | VACUUM TANK - PRESSURE RELIEF VALVE TEST USED TO TEST PRESSURE RELIEF VALVES. |
727, 737, 747, 757, 767, 777, 787 | |
| A21015-8 | DISPATCH EQPT.-BLANK-OFF PLATE, TRIM AIR | B767 | |
| A27003-23 | SECURING CLAMP | B767 | |
| 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 | |
| A27102-7 | SOCKET WRENCH | B767 | |
| A27107-1 | BRACE, SET | B767 | |
| 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 | |
| A28008-8 | DRAIN HOSE | B767 | |
| A28012-1 | SOCKET WRENCH | B767 | |
| A32012-13 | WRENCH - WHEEL RETAINING NUT, M.L.G. USED TO TORQUE MLG WHEEL RETAINING NUT. |
767 | |
| A32014-1 | SAFETY PIN | B767 | |
| A32014-2 | SAFETY PIN | B767 | |
| 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 | |
| A32045-88 | SOCKET WRENCH ADAPTER | B767 | |
| A32045-92 | SOCKET WRENCH ADAPTER | B767 | |
| A32069-7 | WRENCH ADAPTER - RETAINER NUT, ANTI-SKID TRANSDUCER USED TO REMOVE AND INSTALL THE ANTI-SKID TRANSDUCER RETAINER NUT. |
737, 757, 767 | |
| A32075-10 | DRIVE SHAFT | B767 | |
| 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 | |
| A34016-182 | BREAKOUT BOX EQPT | B767 | |
| 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 | |
| A38003-20 | BLOCKAGE REMOVER- VACUUM TOILET | B767 | |
| 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 | |
| A49001-17 | BALLAST WEIGHT | B767 | |
| A49002-1 | EYEBOLT | B767 | |
| 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 | |
| A71015-157 | LIFT FIXTURE | B767 | |
| 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 | |
| B27055-1 | RETAINING TOOL | B757 | |
| 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 | |
| B28001-2 | SOCKET WRENCH | B757 | |
| B28002-2 | INTERMEDIATE PIECE | B757 | |
| B28003-1 | EXTRACTOR | B757 | |
| B32001-4 | LOCKING MECHANISM | B757 | |
| B32013-17 | LOCKING MECHANISM | B757 | |
| B32069-8 | LOCKING BOLT | B757 | |
| B52003-15 | PROTECTIVE EQUIPMENT | B757 | |
| 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 | |
| B78001-2 | LOCKING BOLT | B757 | |
| 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 | |
| B78001-3 | BOLT | B757 | |
| B78001-43 | LOCKING MECHANISM, SET | B757 | |
| BOT710001 | COVER SET | B757 | |
| 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 | |
| C07004-4 | JACK ADAPTER | B737 NG | |
| 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 | |
| C10008-29 | MOORING EQPT NLG | B737 NG | |
| C12002-7 | DRAIN HOSE | B737 NG | |
| C12006-1 | LOCK EQPT.-AILERON FULL-UP LUBRICATION | B737 NG | |
| 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 | |
| C21009-1 | DISPATCH EQUIPMENT | B737 NG | |
| 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 | |
| C25002-1 | REM/INSTL TOOL | B737 NG | |
| C26004-101 | TEST EQUIPMENT | B737 NG | |
| 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 | |
| C26007-78 | TEST EQPT.-CMPT OVERHEAT DETECTION (M237 | B737 NG | |
| C26008-148 | REMOVAL/INSTALLATION EQPT - CARGO FIREX | B737 NG | |
| C26010-1 | COVER-WARNING HORN | B737 NG | |
| 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 | |
| C27001-6 | KNURLED NUT | B737 NG | |
| 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 | |
| C27030-94 | TEST TOOL | B737 NG | |
| 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 | |
| C27042-1 | SOCKET WRENCH ADAPTER | B737 NG | |
| 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 | |
| C27050-89 | HALF SHELL | B737 NG | |
| 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 | |
| C27065-20 | TEST TOOL | B737 NG | |
| 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 | |
| C27069-20 | SETTING TOOL | B737 NG | |
| C27075-1 | SOCKET WRENCH ADAPTER | B737 NG | |
| 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 | |
| C27086-27 | SPRING REM/INSTAL EQPT | B737 NG | |
| C27092-1 | RIGGING BEAM | B737 NG | |
| 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 | |
| C29005-1 | TEST TOOL | B737 NG | |
| C29006-27 | ADAPTER EQUIPMENT - GROUND SERVICE CONNECTION, HYDRAULIC POWER USED TO CONNECT A HYDRAULIC GROUND CART TO THE AIRPLANE HYDRAULIC SYSTEM - SKYDROL SYSTEM. |
737 | |
| C32011-7 | SOCKET WRENCH | B737 NG | |
| 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 | |
| C32022-21 | PROTECTIVE SLEEVE | B737 NG | |
| 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 | |
| C32025-7 | SOCKET WRENCH ADAPTER | B737 NG | |
| C32026-1 | DOWNLOCK EQPT.-NLG & MLG | B737 NG | |
| 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 | |
| C32034-339 | RMVL/INSTL EQUIPMENT | B737 NG | |
| C32040-6 | SOCKET WRENCH | B737 NG | |
| C32041-67 | EXTENSION EQPT. | B737 NG | |
| 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 | |
| C32055-18 | CLAMP ASSY - STEERING CABLES, NLG | B737 NG | |
| C33001-58 | TEST CABLING-B737 BSI LIGHT | B737 NG | |
| C35003-10 | RETRACTION EQUIPMENT - FIRING PIN, OXYGEN SYSTEM USED TO DISARM OXYGEN GENERATORS DURING REMOVAL & INSTALLATION. |
737, 747, 757, 767, 777 | |
| C35003-13 | SAFETY PIN | B737 NG | |
| C35004-1 | PRY BAR EQUIPMENT | B737 NG | |
| C36001-63-KIT | TEST EQUIPMENT- LESS GAUGES | B737 NG | |
| C36001-64 | TEST EQUIPMENT - ENGINE BLEED AIR SYSTEMS USED TO PERFORM OPERATIONAL OR FUNCTIONAL TEST OF THE ENGINE BLEED AIR SYSTEM COMPONENTS. |
737-CL | |
| C36001-64-KIT | TEST EQUIPMENT- LESS GAUGES | B737 NG | |
| 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 | |
| C36006-1-KIT | TEST EQUIPMENT -- LESS GAUGE | B737 NG | |
| C36007-12 | BLANKING PLATE | B737 NG | |
| C36008-1 | BLANKING PLATE | B737 NG | |
| 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 | |
| C44001-55 | REMOVAL/INSTALLATION EQPT -LIFTING STRAP | B737 NG | |
| C49004-40 | HOISTING DEVICE | B737 NG | |
| C49004-41 | FITTING, SET | B737 NG | |
| 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 | |
| C49010-20 | CONE BOLT | B737 NG | |
| 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 | |
| C52008-1 | SOCKET WRENCH SET | B737 NG | |
| C54016-1 | SLING EQPT | B737 NG | |
| C54017-1 | REMOVAL AND INSTALLATION EQPT | B737 NG | |
| 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 | |
| C55009-1 | ALIGNMENT TOOL | B737 NG | |
| C55014-1 | SLING EQPT - HORIZONTAL STAB RMVL/INSTL | B737 NG | |
| C57002-13 | FITTING | B737 NG | |
| 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 | |
| C57007-25 | COVER EQPT *** NO LONGER A TOOL*** | B737 NG | |
| C71004-1 | HOISTING DEVICE | B737 NG | |
| 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 | |
| C71020-105UK91 | UPGRADE KIT FOR C71020-91 TO -105 | B737 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 | |
| C71030-1 | PROOF LOAD FIXTURE - BOOTSTRAP | B737 NG | |
| C71031-1 | SLING EQPT - FAN COWL,CFM LEAP-1B ENGINE. USED TO REMOVE AND INSTALL THE FAN COWL PANELS. |
737-MAX | |
| C71032-1 | SAFETY SCREEN-PERSONNEL BARRIER, CFM LEA | B737 NG | |
| 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 | |
| C78006-1 | SECURING COLLAR | B737 NG | |
| 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 | |
| C78018-30 | PIN | B737 NG | |
| 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 | |
| C78021-13 | GROOVED BOLT | B737 NG | |
| C78021-2 | HOLD OPEN ARM, 65° | B737 NG | |
| C78021-5 | PROTECTIVE CONE | B737 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 | |
| C78025-21 | REM/INSTL TOOL-ACTUATOR | B737 NG | |
| C78025-30 | ACTUATOR INSTALLATION/REMOVAL TOOL USED TO REMOVAL AND/OR INSTALL THRUST REVERSER ACTUATORS FROM THRUST REVERSER ASSEMBLY. |
737-MAX | |
| C78026-259 | REMOVAL/INSTALLATION DEVICE | B737 NG | |
| C78030-10 | GAP MEASURING GAUGE-TRAS LOCKING ACTUATO | B737 NG | |
| 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 | |
| C78033-40 | HOLD OPEN EQPT - THRUST REVERSER | B737 NG | |
| 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 | |
| C78039-1 | REMOVAL/INSTL KIT | B737 NG | |
| C78040-1 | DRIVE SOCKET | B737 NG | |
| C78042-17 | GAUGE | B737 NG | |
| F70199-14 | SEAL | B737 calssic | |
| F70199-15 | PROTECTIVE COVER | B737 calssic | |
| F70199-25 | TIRE INFLATION GAUGE | B737 calssic | |
| 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 | |
| F70207-139 | LOCKING BOLT, SET | B737 calssic | |
| F70207-151 | KIT - RIGGING PIN USED TO RIG SYSTEMS AS DEFINED BY THE AIRPLANE MAINTENANCE MANUALS. |
737-MAX | |
| F70230-1 | INSTALLATION TOOL | B737 calssic | |
| 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 | |
| F70308-15 | PROOF LOAD TAG | B737 calssic | |
| F70308-18 | CABLE ID TAG | B737 calssic | |
| F70308-20 | CABLE ID TAG | B737 calssic | |
| F70308-23 | MAINTENANCE TAG | B737 calssic | |
| F70308-24 | IDENTIFICATION TAG | B737 calssic | |
| F70336-1 | SOCKET WRENCH | B737 calssic | |
| 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 | |
| F72735-1 | KNURLED BOLT | B737 calssic | |
| 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 | |
| F72913-11 | PROTECTIVE COVER | B737 calssic | |
| F72913-8 | PROTECTIVE SLEEVE | B737 calssic | |
| 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 | |
| F72959-31 | SOCKET WRENCH ADAPTER | B737 calssic | |
| F72959-32 | SOCKET WRENCH ADAPTER | B737 calssic | |
| F72959-33 | SOCKET WRENCH ADAPTER | B737 calssic | |
| F72959-35 | SOCKET WRENCH ADAPTER | B737 calssic | |
| F72959-40 | SPANNER WRENCH AN STANDARD TYPE USED FOR NUMEROUS TORQUING OPERATIONS. |
707, 727, 737, 747, 757, 767, 777 | |
| F72959-41 | SOCKET WRENCH ADAPTER | B737 calssic | |
| F80000-7 | JACK ADAPTER | B737 calssic | |
| 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 | |
| F80060-6 | JACK ADAPTER | B737 calssic | |
| F80063-501 | SUPPORT STAY | B737 calssic | |
| F80167-13 | LUBRICATION TOOL SET | B737 calssic | |
| F80197-6 | OPEN-ENDED WRENCH | B737 calssic | |
| F80197-7 | BOX WRENCH | B737 calssic | |
| 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 | |
| F80241-17 | RESTRAINT | B737 calssic | |
| FTC102 | TOTAL AIR TEMPERATURE COVER | B737 calssic | |
| G07005-1 | JACK ADAPTER | B747 | |
| 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 | |
| G28018-2 | INTERMEDIATE PIECE ASSY. | B747 | |
| G28018-61 | TEST EQUIPMENT | B747 | |
| G28018-7 | INTERMEDIATE PIECE ASSY. | B747 | |
| G29015-1 | TEST EQUIPMENT | B747 | |
| G32005-8 | GAUGE, SET | B747 | |
| G32039-4 | SOCKET WRENCH | B747 | |
| G32048-41 | LOCK EQPT | B747 | |
| G32051-1 | LOCKING MECHANISM | B747 | |
| 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 | |
| G34002-1 | ANGLE MEASURING EQUIPMENT | B747 | |
| G34002-20 | CYLINDER PIN | B747 | |
| G34002-21 | PIN, DIAMOND | B747 | |
| G35002-2 | CLAMPING PIECE | B747 | |
| 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 | |
| G36035-39 | REDUCING COUPLING | B747 | |
| G36035-77 | TEST EQPT- PNEUMATIC SYSTEM HEALTH CHECK | B747 | |
| G38004-12 | PLUG | B747 | |
| 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 | |
| G71038-17 | UNLOCK POLE EQPT | B747 | |
| G71045-1 | 6 TON HOIST ASSY (HARRINGTON HOIST ONLY) | B747 | |
| G71045-2 | 3 TON HOIST ASSY (HARRINGTON HOIST ONLY) | B747 | |
| G71045-3 | 6 TON HOIST ASSY (HARRINGTON HOIST ONLY) | B747 | |
| 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 | |
| G78005-10 | INTERMEDIATE PIECE | B747 | |
| G78009-1 | GAUGE | B747 | |
| 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 | |
| J07003-1 | JACK ADAPTER | B777 | |
| J07016-1 | FITTING EQPT | B777 | |
| J07017-1 | FITTING EQPT - JACK OUTER WING (G & H) | B777 | |
| J10001-1 | BLANKING PLATE, SET | B777 | |
| J10001-25 | BLANKING PLATE, SET | B777 | |
| J10008-1 | PLUG SET | B777 | |
| 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 | |
| J20009-88 | LIFTING ADAPTER | B777 | |
| J20011-1 | INTERFACE ADAPTER ASSY | B777 | |
| J21001-133 | HOISTING EQUIPMENT | B777 | |
| J21003-1 | MAINTENANCE PLATFORM | B777 | |
| J23001-26 | HOIST ADAPTER | B777 | |
| J24001-50 | HOIST ADAPTER | B777 | |
| 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 | |
| J24018-1 | HOIST ADAPTER - IDG | B777 | |
| J24019-1 | HOIST ADAPTERS - BACKUP GENERATOR | B777 | |
| J25001-5 | LEVER | B777 | |
| J26004-24 | TEST EQPT - SQUIB FIRE EXTINGUISHING SYSTEM USED TO VERIFY THE REQUIRED VOLTAGE AT THE APPROPRIATE SQUIB CONNECTOR UPON DISCHARGE. |
777, 777X, 787 | |
| J26006-1 | TEST DEVICE | B777 | |
| J27005-48 | LOCK EQPT - INBD/OUTBD, SPOILER ACTUATOR USED TO HOLD THE INBOARD AND OUTBOARD SPOILERS IN THE DEPLOYED POSITION. |
777 | |
| J27007-15 | HOIST EQPT | B777 | |
| 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 | |
| J27012-1 | HOISTING SLING | B777 | |
| 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 | |
| J27028-20 | SECURING CLAMP | B777 | |
| J27028-21 | SECURING CLAMP | B777 | |
| J27079-38 | ELEVATOR FREEPLAY USED TO PERFORM THE FREEPLAY INSPECTION OF THE POWER CONTROL UNITS FOR THE ELEVATOR. |
747, 767, 777, 777X, 787 | |
| J27087-1 | EQPT LOCK SPOILER PWR CNTL | B777 | |
| J27088-1 | GAGE ASSY | B777 | |
| J27108-1 | DRIVE ADAPTER | B777 | |
| J27108-13 | DRIVE ADAPTER | B777 | |
| J27157-1 | FLAP LEVER LOCKOUT | B777 | |
| J28013-1 | FUEL DRAIN SUMP. USED TO DRAIN FUEL FROM MAIN TANK SUMPS. |
737, 767, 777 | |
| J29003-93 | HOIST ADAPTER | B777 | |
| J29007-1 | HOIST ADAPTER - ENGINE DRIVEN PUMP | B777 | |
| 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 | |
| J32004-23 | EXTRACTOR, SET | B777 | |
| 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 | |
| J32008-74 | REMOVAL EQUIPMENT | B777 | |
| 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 | |
| J32036-56 | EXTRACTOR WITH SLIDE HAMMER | B777 | |
| J32043-178 | LUG LIFT EQPT | B777 | |
| 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 | |
| J32065-1 | ALIGNMENT PIN | B777 | |
| 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 | |
| J46002-11 | TEST DEVICE | B777 | |
| J46002-16 | FIBER OPTIC BREAKOUT BOX | B777 | |
| 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 | |
| J52013-1 | ADJUSTMENT DEVICE | B777 | |
| 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 | |
| J57014-1 | LOCKOUT TOOL | B777 | |
| 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 | |
| J71002-60 | RATCHET | B777 | |
| 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 | |
| J71048-1 | SLING EQPT - INLET | B777 | |
| J71049-1 | HOIST EQUIPMENT | B777 | |
| J71056-1 | TRANSPORTATION EQPT | B777 | |
| J78004-111 | LATCH BEAM ATT FTG | B777 | |
| 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 | |
| J78015-96 | ARM ASSY. | B777 | |
| 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 | |
| K07003-15 | JACK ADAPTER | B787 | |
| K07004-1 | JACK ADAPTER | B787 | |
| K10002-1 | BLANKING PLUG | B787 | |
| K10007-1 | PROTECTIVE COVER | B787 | |
| 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 | |
| K20003-92 | PERSONNEL PROTECTIVE EQUIPMENT | B787 | |
| 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 | |
| K21001-1 | REMOVAL/INSTALLATION DEVICE | B787 | |
| K21001-79 | INSTALL/REMOVE/TRANSPORT CART | B787 | |
| 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 | |
| K21004-72 | ADAPTER | B787 | |
| 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 | |
| K21012-1 | HOLDING FIXTURE | B787 | |
| K21014-1 | JACK ADAPTER | B787 | |
| 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 | |
| K21016-136 | ADAPTER, SET | B787 | |
| 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 | |
| K24001-119 | ADAPTER | B787 | |
| 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 | |
| K27003-1 | ADAPTER | B787 | |
| 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 | |
| K27007-1 | DRIVE ADAPTER | B787 | |
| K27008-67 | REMOVAL/INSTALLATION DEVICE | B787 | |
| K27010-104 | REMOVAL/INSTALLATION DEVICE | B787 | |
| 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 | |
| K27015-24 | LOCK - AILERON POWER CONTROL UNIT | B787 | |
| K27017-22 | SECURING COLLAR | B787 | |
| K27017-36 | SECURING COLLAR | B787 | |
| 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 | |
| K27022-39 | SETTING TOOL | B787 | |
| K27025-28 | HOISTING SLING | B787 | |
| K27035-1 | SUPPORT ROD | B787 | |
| K27036-1 | TOOL KIT | B787 | |
| K27037-76 | RIGGING EQPT-L.E. SLAT INSTALLATION | B787 | |
| 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 | |
| K27039-15 | RIGGING EQPT | B787 | |
| K27039-16 | RIGGING EQPT | B787 | |
| 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 | |
| K27044-1 | SUPPORT TOOL | B787 | |
| 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 | |
| K27049-90 | HOIST EQPT-ELECTRONIC MOTOR CONTROLLER, | B787 | |
| K27049-91 | HOIST EQPT-ELECTRONIC MOTOR CONTROLLER | B787 | |
| 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 | |
| K27051-1 | MEASURING TOOL | B787 | |
| 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 | |
| K27056-50 | REMOVAL/INSTALLATION DEVICE | B787 | |
| K27057-10 | BOX WRENCH | B787 | |
| 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 | |
| K27061-1 | REMOVAL EQUIPMENT | B787 | |
| K27064-1 | RIGGING TOOL FLAPERON | B787 | |
| K27068-10 | MEASURING TOOL SKEW SENSOR ANGULAR | B787 | |
| 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 | |
| K29002-78 | REMOVAL/INSTALLATION DEVICE | B787 | |
| 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 | |
| K32008-132 | WRENCH KIT,LANDING GEAR | B787 | |
| K32012-77 | HOISTING EQUIPMENT | B787 | |
| K32016-1 | TURNBUCKLE | B787 | |
| K32016-20 | TURNBUCKLE - TRUCK POSITION ACTUATOR MLG | B787 | |
| 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 | |
| K32027-106 | HAND PUMP | B787 | |
| K32028-1 | SOCKET WRENCH ADAPTER | B787 | |
| K32028-2 | SOCKET WRENCH ADAPTER | B787 | |
| K32034-1 | SOCKET WRENCH ADAPTER | B787 | |
| 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 | |
| K32046-1 | SLING EQPT SLG ACTUATOR | B787 | |
| K35001-115 | TEST EQPT | B787 | |
| 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 | |
| K38003-1 | LEAK TEST EQPT-POTABLE WATER SYSTEM | B787 | |
| 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 | |
| K49002-1 | HOISTING DEVICE | B787 | |
| K49004-1 | HOISTING EQUIPMENT | B787 | |
| K52002-133 | BARRIER - PASSENGER ENTRY DOORS. USED TO PREVENT MAINTENANCE PERSONNEL FROM ACCIDENTALLY FALLING FROM PASSENGER ENTRY DOORS DURING MAINTENANCE PROCEDURES |
787 | |
| K52009-1 | SAFETY GUARD NET | B787 | |
| K52011-1 | INSTALLATION TOOL | B787 | |
| K52016-1 | SAFETY BARRIER - CARGO DOORS USED TO PREVENT PERSONNEL FROM FALLING OVERBOARD WHEN THE CARGO DOORS ARE OPEN DURING AIRCRAFT MAINTENANCE. |
787 | |
| K52026-1 | SOCKET WRENCH | B787 | |
| 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 | |
| K53005-1 | HOOK WRENCH | B787 | |
| K54001-111 | REM/INSTL EQPT AFT STRUT FAIRING | B787 | |
| 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 | |
| K55006-125 | HOLDING FIXTURE | B787 | |
| 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 | |
| K71005-1 | TRANSPORTATION EQUIPMENT | B787 | |
| 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 | |
| K71009-47 | SLING FAN COWL GE | B787 | |
| K71009-49 | SLING - FAN COWL | B787 | |
| 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 | |
| K78005-22 | HOLD-OPEN DEVICE | B787 | |
| K78006-1 | LOCK - THRUST REVERSER ISOLATION VALVE (GROUND) USED TO PREVENT THRUST REVERSER OPERATION ON GROUND DURING MAINTENANCE AND BYPASS MODE. |
787 | |
| K78009-1 | HOLDING FIXTURE | B787 | |
| 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 | |
| ST1066RB-1 | STANDARD TOOL - RELEASE KEY | #NV | |
| ST1742F | WINDOW INSTALL & REMOVAL TOOL | #NV | |
| ST2580-418 | SOCKET WRENCH | #NV | |
| ST2584C | PLIERS | #NV | |
| ST6760A-1 | PROBE - LEAK, ULTRASONIC USED TO DETECT AIR LEAKS. USED WITH VACUUM BAG ATTACHMENTS # ST9999- VBA-201/-301, ST9999-VB & ST6760 |
ALL | |
| ST848 | INSTALLATION TOOL, SET | #NV | |
| ST8709H-X | STANDARE TOOL - GO-NO-GO GAGE | #NV |
|
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