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时间:2011-04-02 16:51来源:蓝天飞行翻译 作者:航空
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B2  LGVB  1  640.8  1/8 7 x 19  MS21260L4RH  BACT14A4 
A3  LGVA  1  502.1  1/8 7 x 19  MS21260L4RH  BACT14A4 
B3  LGVB  1  514.8  1/8 7 x 19  MS21260L4RH  BACT14A4 
C  LGVA  1  105.4  70.6  1/8 7 x 19  MS21260L4LH  BACT14B4  BACT14A4 
D  LGVB  1  99.6  1/8 7 x 19  MS21260L4LH  BACT14A4 

MATERIAL:  CABLE PREFERRED - CARBON STEEL PER BMS 7-265, TYPE 1, COMP A 1ST ALTERNATE - CARBON STEEL PER MIL-W-83420, TYPE 1, COMPOSITION A 2ND ALTERNATE - CARBON STEEL PER MIL-W-1511
NOTE:  DO NOT MIX TIN-ZINC (TZ) COVERED CABLES WITH OTHER TYPE CABLES ON THE SAME AIRPLANE BECAUSE TZ CABLES HAVE A DIFFERENT STRETCH RATE THAN OTHER CABLES.

737-300 AIRPLANES 737-400 AIRPLANES
737-500 AIRPLANES
Landing Gear Control Cable Installation Figure 401 (Sheet 2)
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 32-31-41
 ALL  ú ú 03 Page 404 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 (2)  S 434-011Attach the cables to the control quadrant assembly and install the cotter pins.
 (3)  S 434-012Connect the turnbuckles.
 (4)  S 824-013Adjust the control system for the landing gear (Ref 32-31-00/501).
 (5)  S 414-014Install the left inboard panel on the floor.
 (6)  S 434-016Install the passenger seats (Ref 25-22-00/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-31-41
 ALL  ú ú 02 Page 405 ú Nov 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 LANDING GEAR SELECTOR VALVE - REMOVAL/INSTALLATION
__________________________________________________
 TASK 32-31-51-024-011
 1.  Landing Gear Selector Valve Removal (Fig. 401)___________________________________
 A. References
 (1)
32-00-01/201, Ground Lock Assemblies

 B.
Access

 (1)  
Location Zone 216,217 Main Landing Gear Wheel Well

 C.
Removal


 (1)  S 494-001Install the ground lock assemblies (Ref 32-00-01/201).
 (2)  S 864-002Release the pressure in hydraulic system A and the hydraulic reservoir.
 (3)  S 034-003Disconnect the actuating link of the selector valve at the selector valve.
 (4)  S 034-004Disconnect all the hydraulic lines from the selector valve.
 NOTE:____ You must seal all the lines with a cap to prevent contamination.
 (5)  S 034-005Remove the bolts which attach the selector valve to the structure.
 (6)  S 024-006Remove the selector valve from the airplane.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-31-51
 ALL  ú ú 02 Page 401 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500
MAINTENANCE MANUAL

SELECTOR VALVE SEE A
SYSTEM A WHEEL WELLPRESSURE CEILING
SYSTEM A RETURN
VALVE SELECTOR  ACTUATING LINK 
INBD 
GEAR DOWN  GEAR UP  A  FWD 
Figure 401 Landing Gear Selector Valve Installation 

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 32-31-51
 ALL  ú ú 01 Page 402 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 034-023
 (7)  Remove the hydraulic fitting from the valve, discard the O-rings and seal the ports with a cap.
 TASK 32-31-51-424-010
 
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本文链接地址:737-300 400 500 AMM 飞机维护手册 起落架 LANDING GEAR 2(55)