(c)
Remove the outboard bearing cap (15) and the bearing retention key (14) by removing two bolts (17).
NOTE:____The bearing remains on the trunnion. Note the position of the cap to facilitate its reinstallation.
CAUTION: A LIMITED CLEARANCE EXISTS BETWEEN THE GEAR COMPONENTS AND
_______ THE AIRPLANE STRUCTURE. VIOLATION OF THE CLEARANCE CAN CAUSE DAMAGE TO THE COMPONENTS AND STRUCTURE.
(d)
Slowly jack the airplane away from the body gear, watching the clearance between the gear and the airplane structure.
(e)
Remove the upper bushing half (4) from the inboard bearing when the trunnion (5) clears the support fitting.
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CAUTION: CLEARANCES ARE MINIMAL; OBSERVE CAREFULLY ALL AREAS TO
_______ AVOID STRIKING AIRPLANE WHILE YOU REMOVE GEAR. DAMAGE TO THE AIRPLANE OR TO THE GEAR CAN OCCUR WHEN YOU REMOVE GEAR.
(f)
Continue to jack the airplane until it clears the gear.
(g)
Roll the gear from under airplane using an automotive type jack under the forward end of the truck for steering.
TASK 32-13-01-404-022
3. Body Landing Gear Installation
______________________________
A. Special Tools and Equipment
(1)
G32005-8 - Gage Equipment - Vertical Support Fitting, Inboard Trunnion, Body Landing Gear
(a)
G32005-9 - Clamp up Gage
(b)
G32005-11 Rotation Gage
(2)
2MIT65B08802-1 - Bungee Restraining Tool, Body Gear
(3)
6MIT65B00163 - Torque Equipment, Body Landing Gear Inboard Trunnion
(4)
2MIT65B01203 - Torque Adapter, Body Landing Gear Trunnion Retaining Nut
(5)
G32028-134 - Vertical Stabilizer, Body Gear Shock Strut
(6)
8ME65B01202-3 - Retention Tool, Body Gear Shock Strut
B.
Standard Tools and Equipment
(1)
3-Ton Automotive Type Jack
C.
Consumable Materials
(1)
A00247 - Sealant, BMS 5-95, Type 1, Class B
(2)
B00316 - Cleaning Solvent, TT-N-95, Type I
(3)
D00633 Grease - BMS 3-33 (preferred)
(4)
D00013 Grease - MIL-G-23827 (optional)
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D. Parts ~.............................................................................. | AMM | | AIPC | ................. ...........................| | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ...............................................................................| | 402 | 2 | Nut | 32-13-01 | 10 | 240 | | | 3 | Washer | | | 235 | | | 4 | Bushing, Upper | | | 260 | | | 6 | Bearing Retention Key | | | 220 | | | 7 | Cap, Bearing | | | 250 | | | 8 | Washer | | | 230 | | | 9 | Bolt | | | 225 | | | 10 | Bushing, Lower | | | 265 | | | 12 | Nut | | | 75 | | | 13 | Washer | | | 70 | | | 14 | Bearing Retention Key | 32-13-01 | 01 | 120 | | | 15 | Cap, Bearing | 32-13-01 | 10 | 80 | | | 16 | Washer | | | 65 | | | 17 | Bolt | | | 60 | | | 18 | Nut | 32-13-01 | 01 | 60 | | | 19 | Washer | 32-21-04 | 05 | 65 | | | 21 | Seal Backup Ring | 32-13-03 | 02 | 84A | | | 22 | Spiral Seal | | | 84B | | | 23 | Seal Retainer | | | 84 | | | 24 | Body Landing Gear (LH) | 32-13-01 | 05 | 1 | | | 24 | Body Landing Gear (RH) | | | 10 | 2......…........…...................................…...........….....…........1
E. References
(1)
AMM 07-11-01/201, Jacking Airplane
(2)
AMM 09-11-00/201, Towing
(3)
AMM 12-15-04/301, Body Landing Gear Shock Strut
(4)
AMM 12-21-01/301, Landing Gear
(5)
AMM 24-22-00/201, Manual Control
(6)
AMM 29-11-00/201, Main Hydraulic Supply System
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本文鏈接地址：747-400 AMM 飛機維護手冊 起落架 LANDING GEAR 2(127)
