737-300 400 500 AMM 飞机维护手册 起落架 LANDING GEAR 2(127)

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_______ STEERING ACTUATORS ON THE NOSE GEAR WHILE THE GEAR EXTENDS AND RETRACTS. THIS CAN OCCUR IF THE DOORS ARE NOT ADJUSTED CORRECTLY AND CAN CAUSE DAMAGE TO THE DOORS.
 (2)  
Extend and retract the gear and verify the door for correct
 operation (AMM 32-33-00/501).

 (3)  
Extend the gear.

 S 865-017
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A 737-300/400/500MAINTENANCE MANUAL
 (4)  S 495-018Install the ground locks on the nose landing gear (AMM 32-00-01/201).
 (5)  S 095-021Remove the jacks from the airplane.

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A
737-300/400/500MAINTENANCE MANUAL
 NOSE LANDING GEAR WHEEL WELL DOOR LINKAGE - INSPECTION/CHECK
____________________________________________________________
 1.  General_______
 A.  This procedure only has illustration and a wear limits table which shows the data for wear limits. There are no procedures for the access, the removal, or the installation of the parts. Refer to the Nose Landing Gear Wheel Well Door Linkage - Removal/Installation for procedures to do these tasks.
 TASK 32-33-61-206-001
 2.  Wear Limits for the Door Linkage on the Wheel Well of the Nose Landing Gear___________________________________________________________________________ (Fig./601)
 A.  Wear Limits for the Door Linkage on the Wheel Well of the Nose Landing Gear
 S 226-002
 (1)  Refer to Fig. 601 for the inspection points and the wear limits table.
SEE A
Nose Gear Door Linkage Wear Limits
Figure 601 (Sheet 1)

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A 737-300/400/500MAINTENANCE MANUAL

C-C
Nose Gear Door Linkage Wear Limits Figure 601 (Sheet 2)
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A 737-300/400/500MAINTENANCE MANUAL

NOT USED REFER TO THE OVERHAUL MANUAL FOR REPAIR INSTRUCTIONS REPLACE WORN BUSHINGS THE TOTAL DIAMETRAL CLEARANCE BETWEEN THE BEARING RACE, BEARING BALL, AND BOLT MUST NOT BE GREATER
THAN THE SPECIFIED MAX. DIA CLEARANCE.
Nose Gear Door Linkage Wear Limits
Figure 601 (Sheet 3)

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C98797
A
737-300/400/500MAINTENANCE MANUAL
 NOSE GEAR RETRACT PRESSURE FUSE - REMOVAL/INSTALLATION
______________________________________________________
 TASK 32-33-71-004-001
 1.  Nose Gear Retract Fuse Removal (Fig. 401)_________________________________________
 A. Equipment
 (1)  
Ground Lock Assemblies (Ref 32-00-01).

 B.
Prepare for the removal.

 S 864-002
 (1)  
Make sure that you install the ground lock assemblies for the landing gears (Ref 32-00-01).

 (a)  
　
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