M50671
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-11-11
ALL ú ú 01 Page 407 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500
MAINTENANCE MANUAL
SEE A
OUTBD
FWD
SHOCK STRUT
1. DOWNLOCK SPRING
TRUNNION LINK 6. TRUNNION PIN
5. SPRING SUPPORT SHAFT
2. SPRING SUPPORT CAP 4. REACTION LINK
2A. WASHER FWD
1. DOWNLOCK SPRING A 3. REACTION LINK UNIVERSAL
Reaction Link Attachment to Shock Strut Figure 404
M50691
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-11-11
ALL ú ú 01 Page 408 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
SWING UPTRUNNION LINK CLEAR OFPIN REMOVED
SHOCK STRUT LUGS
REAR
ADJUST THE POSITION OF THE SHOCK
FWD IF IT IS NECESSARY
STAGE 1 STAGE 2 DISCONNECT DRAG STRUT AND REMOVE GEAR FROM REMOVE TRUNNION LINK PIN REAR TRUNNION BEARING
SUPPORT GEAR
HIGH ENOUGH TO
KEEP TORSION
UNSCREW FORWARD
LINKS CLEAR BEARING SLEEVEREAR WING
STAGE 3 STAGE 4 REMOVE GEAR FROM AIRPLANE REMOVE TRUNNION LINK
Main Landing Gear Removal Sequence
Figure 405
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-11-11
ALL ú ú 01 Page 409 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
M50731
A
737-300/400/500MAINTENANCE MANUAL
SEE A
1. ANTIROTATION BOLT
OUTBD
FWD
2. ACTUATOR WALKING BEAM ARM
4. TRUNNION PIN LOCKBOLT
3. SHOCK
9. TRUNNION PIN STRUT
8. THREAD PROTECTOR4. TRUNNION PIN
(F80115-1) LOCKBOLT
6. TRUNNION
FWD INBD 5A. SPECIAL PIN NUT
WASHER
7. TRUNNION
LINK 5. RETAINER
WASHER
A
Trunnion Link Shock Strut Attachment
Figure 406
M50735
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-11-11
ALL ú ú 01 Page 410 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(c)
Attach the drag strut (4) to the shock strut with a line, (Stage 2, Fig. 405).
(d)
Mark and keep the drag strut upper bolt (5) for subsequent installation.
NOTE: The bolt is identified by a yellow head.
____
(e)
Lift the airplane on jacks until the tires clear the ground so that the landing gear can move in the inboard direction (to retraction).
(f)
Lightly hit the end of the trunnion link with a lead hammer to move it upward to clear the shock strut lugs (Stage 2, Fig. 405).
(g)
Hold the trunnion link in position so that it does not touch the landing gear
S 024-099
(7)
Remove the Shock strut (13), (Fig. 408).
(a)
Get access to the aft trunnion bearing (12). 1) Remove the lockbolts (1) and the bearing retainer lock (2). 2) Remove the bearing retainer nut (3). 3) Remove the grease reservoir (4) and the seal ring (11). 4) Remove the lockbolt (5). 5) Loosen the fuse nut (6). 6) Remove the washer (7) and the key (8).
(b)
Use a minimum of three persons to lower the landing gear.
1) If necessary, use the applicable holding fixture to lower the landing gear. 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(62)