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 ~.............................................................................. | AMM | | AIPC | ................. ...........................| | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ...............................................................................| | 402 | 1 | Spherical Bearing | 32-11-02 | 02 | 69 | | | 2 | Outer Bearing Race | | | 68 | | | 3 | Bearing Retainer Bolt | 57-15-01 | 02 | 95 | | | 4 | Lockwasher | 32-11-02 | 02 | 66 | | | 5 | Trunnion Bearing Locknut | | | 67 | | | 6 | Bolt | 32-11-02 | 02 | 60 | | | 7 | Washer | | | 65 | | | 8 | Retaining Nut Lockplate | | | 55 | | | 9 | Bearing Retainer Bolt | 57-15-01 | 02 | 115 | | | 10 | Bearing Retainer | | | 135 | | | 11 | Bearing Adjusting Ring | 32-11-02 | 02 | 69 | | | 12 | Trunnion Outer Sleeve | | | 110 | | | 13 | Key | 32-11-02 | 02 | 50 | 2......…........…...................................…...........….....…........1
 E. References
 (1)  
AMM 07-11-01/201, Jacking Airplane

 (2)  
AMM 12-15-03/301, Wing Landing Gear Shock Strut

 (3)  
AMM 12-21-01/301, Landing Gear - Servicing Lubrication

 (4)  
AMM 24-22-00/201, Manual Control

 (5)  
AMM 29-11-00/201, Main Hydraulic Supply System

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-11-01
 ALL  ú ú 02 Page 414 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 (6)  
AMM 32-09-03/501, Proximity Switch Electronics Unit

 (7)  
AMM 32-11-03/401, Wing Gear Drag Brace

 (8)  
AMM 32-11-15/401, Wing Gear Actuator Walking Beam

 (9)  
AMM 32-11-19/401, Wing Gear Trunnion Fork

 (10)
 AMM 32-11-20/401, Wing Gear Truck Positioning Actuator

 (11)
 AMM 32-11-27/401, Wing Gear Side Strut Component Assembly

 (12)
 AMM 32-12-06/401, Wing Gear Shock Strut Inboard Door

 (13)
 AMM 32-12-07/401, Wing Gear Shock Strut Outboard Door

 (14)
 AMM 32-11-23/501, Wing Gear Truck Mechanical Lock Adjustment/Test.

 (15)
 AMM 32-32-00/501, Wing Gear and Door Extension and Retraction

 (16)
 AMM 32-32-01/401, Wing Gear Actuator

 (17)
 AMM 32-41-00/201, Hydraulic Brake System

 (18)
 AMM 32-41-00/501, Hydraulic Brake System

 (19)
 AMM 32-42-00/501, Brake Control System

 (20)
 AMM 32-46-00/501, Brake Temperature Monitoring System

 (21)
 WDM 32-48-12, WDM 32-48-13, WDM 32-48-14, WDM 32-48-15

 F.
Access

 (1)  
Location Zone
 735 Wing Landing Gear, LH
 745 Wing Landing Gear, RH

 G.
Prepare for the Installation

 S 494-047
 WARNING: YOU MUST CAREFULLY INSTALL THE GROUND LOCKS IN ALL LANDING
_______ GEAR. AN ACCIDENTAL RETRACTION OF THE LANDING GEAR CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (1) Install the ground locks in all landing gear (AMM 09-11-00/201).
 S 494-048
 WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASKS BELOW TO INSTALL
_______ THE DOOR LOCKS ON THE LANDING GEAR DOORS. THE DOORS CAN CLOSE QUICKLY IF YOU DO NOT INSTALL THE DOOR LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (2)  
Do this task: "Installation of the Door Locks on the Wing Landing Gear" (AMM 32-00-30/201).

 S 494-049

 (3)  
Do this task: "Installation of the Door Locks on the Body Landing Gear" (AMM 32-00-30/201).

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 ALL  ú ú 04 Page 415 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 H. Prepare to Install the Wing Landing Gear (Fig. 402 and 403).
 S 214-080
 (1)  
Make sure corrosion preventive compound (MIL-C-11796) is on the aft trunnion (Fig. 403).

 (a)  
If the corrosion preventive compound is damaged, worn, has cracks or is too thin, apply compound as necessary (Fig. 403).
　
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