(2)
Jacks - Airplane
B.
References
(1)
AMM 07-11-11/201, Airplane Jacking
(2)
AMM 29-15-00/201, Hydraulic System
(3)
AMM 32-00-01/201, Ground Lockpins
(4)
AMM 32-61-31/401, Main Downlock Sensor
C.
Access
(1)
Location Zones
310 Left Main Landing Gear
410 Right Main Landing Gear
D.
Prepare to Remove Main Gear Side Strut
S 844-002
(1)
Make sure that all the landing gear ground lock pins are installed (AMM 32-00-01/201).
S 844-003
(2)
Remove the pressure from the hydraulic system (AMM 29-15-00/201).
S 584-004
(3)
Lift the airplane on jacks to remove the weight from the gear (AMM 07-11-11/201).
E.
Remove the Main Gear Side Strut
S 034-005
(1)
Disconnect the main gear downlock sensor (5) (AMM 32-61-31/401).
(a)
Release all the cable connections from the side strut.
(b)
Remove the cable through the slot in the sensor bracket.
(c)
Wind all the cables into coils.
(d)
Use tape to keep the switch clear of the side strut.
S 024-006
(2)
Hold the inboard wing door and the side strut and remove the upper attachment bolt (4) of the side strut.
(3)
Remove the lower attachment bolt (9) of the lock strut.
(4)
Remove the higher half of the side strut (3).
S 024-007
S 024-008
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-11-61
ALL ú ú 02 Page 401 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEE A SIDE STRUT SEE B
SEE D
UPLOCK LINK
1.
REACTION LINK
2.
SPECIAL SPACER
3.
UPPER SIDE
4.
UPPER ATTACHMENT
STRUT
BOLT
INBD FWD
SIDE STRUT UPPER ATTACHMENT A Main Gear Side Strut Installation Figure 401 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-11-61
ALL ú ú 01 Page 402 ú Jun 25/86
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
INBD 6. DOWNLOCK LOWER LINK DOWNLOCK SENSOR ACTUATOR FWD DOWNLOCK UPPER LINK FWD INBD
SEE C
9. LOCK STRUT LOWER ATTACHMENT BOLT STRUT UPPER SIDE 3. 7. SPACER WASHER SENSOR BRACKET 5. DOWNLOCK SENSOR ELECTRICAL CONDUIT
8. STRUT LOWER SIDE 3. STRUT UPPER SIDE
B 11. BOLT LOWER ATTACHMENT SIDE STRUT CENTER ATTACHMENT C
8. LOWER SIDE STRUT
UPPER DRAG STRUT
10. SIDE STRUT UNIVERSAL FITTING INBD FWD
LOWER DRAG STRUT
SIDE STRUT LOWER ATTACHMENT
D
Main Gear Side Strut Installation Figure 401 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-11-61
ALL ú ú 01 Page 403 ú Nov 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 024-009
(5)
Remove the lower attachment bolt (11) of the side strut.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 起落架 LANDING GEAR 1(97)