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时间:2011-04-02 16:46来源:蓝天飞行翻译 作者:航空
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 (10)
 Lubricate the landing gear (AMM 12-21-11/301).

 (11)
 Lift the airplane for gear retraction (AMM 07-11-11/201).


 S 424-023
 S 644-024
 S 584-025
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 32-11-71
 ALL  ú ú 03 Page 407 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 084-026
 (12)
 Remove the ground lockpins (AMM 32-00-01/201).

 S 784-031

 (13)
 Pressurize the hydraulic system (AMM 29-15-00/201).

 S 724-027

 (14)
 Retract and extend the gear.

 S 494-028

 (15)
 Install the ground lockpins (AMM 32-00-01/201).

 S 214-029

 (16)
 Examine the reaction link and other related parts, and make sure they operate correctly.

 (17)
 Lower the airplane and remove the jacks.


 S 584-030
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 ALL  ú ú 02 Page 408 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 MAIN LANDING GEAR REACTION LINK - 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 Main Landing Gear Reaction Link - Removal/Installation for procedures to do these tasks.
 TASK 32-11-71-206-001
 2.  Wear Limits for the Reaction Link of the Main Landing Gear (Fig. 601)
__________________________________________________________
 A.  Wear Limits for the Reaction Link
 S 226-002
 (1)  Refer to Fig. 601 for the inspection points and the wear limits table.

C  D 
D  A  B 
FWD  INBD  REACTION LINK  B  A UPLOCK ASSEMBLY 
Main Landing Gear Reaction Link Wear Limits Figure 601 (Sheet 1) 

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 32-11-71
 ALL  ú ú 01 Page 601 ú Jul 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
2. BUSHING/BOLT

UPPER DOWNLOCK  UPPER DOWNLOCK
5. BUSHING/BOLT
LINK ASSEMBLY  LINK ASSEMBLY
(2 LOCATIONS)
C-C  D-D
Main Landing Gear Reaction Link Wear Limits
Figure 601 (Sheet 2)

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 ALL  ú ú 01 Page 602 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
INDEX NO.  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  REPLACE PART WORN  REPAIR WORN PART  REPAIR INSTR. 
DIAMETER  MAX WEAR DIM.  MAX DIAM CLEAR-ANCE
MIN  MAX 
110  BUSHING  ID  1.375  1.376  1.378  0.005  X 
BOLT  OD  1.373  1.374  1.372  X  1 
1 11  BUSHING  ID  1.250  1.251  1.253  0.005  X 
BOLT  OD  1.248  1.249  1.247  X  1 
2 10 BUSHING  ID  1.437  1.438  1.439  0.005  X 
BOLT  OD  1.435  1.436  1.434  X  1 
2 11  BUSHING  ID  1.375  1.376  1.377  0.005  X 
 
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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 1(103)