32-00-01
ALL ú ú 01 Page 804 ú Jun 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
(3)
IPC 32-13-11 Fig. 1
B.
Access
(1)
Location Zone
755 Body Landing Gear, LH
765 Body Landing Gear, RH
C.
Procedure
S 028-023
(1)
Remove the truck pivot pin (Ref 32-13-11/401).
S 228-006
(2)
Do a check of the parts (Ref 32-13-11/601).
S 328-007
(3)
Make shims if it is necessary (Fig. 801).
S 428-008
(4)
Install the truck pivot pin with shims between the bushing flanges (Fig. 801) (Ref 32-13-11/401).
TASK 32-00-01-308-009
4. Clearance Correction for the Torsion Link Pin of the Wing Landing Gear
______________________________________________________________________
A. References
(1)
32-11-14/401, Wing Gear Torsion Links
(2)
32-11-14/601, Wing Gear Torsion Links
(3)
IPC 32-11-14 Fig. 2
B.
Access
(1)
Location Zone
735 Wing Landing Gear, LH
745 Wing Landing Gear, RH
C.
Procedure
S 028-022
(1)
Remove the torsion link pin (Ref 32-11-14/401).
S 228-010
(2)
Do a check of the parts (Ref 32-11-14/601).
S 328-011
(3)
Make shims if it is necessary (Fig. 801).
S 428-012
(4)
Install the torsion link with shims between the bushing flanges (Fig. 801) (Ref 32-11-14/401).
TASK 32-00-01-308-013
5. Clearance Correction for the Torsion Link Pin of the Body Landing Gear
______________________________________________________________________
A. References
(1) 32-13-14/201, Body Gear Lower Torsion Link
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-00-01
ALL ú ú 01 Page 805 ú Oct 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
(2)
IPC 32-13-14 Fig. 1
B.
Access
(1)
Location Zone
755 Body Landing Gear, LH
765 Body Landing Gear, RH
C.
Procedure
S 028-024
(1)
Remove the torsion link pin (Ref 32-13-11/401).
S 228-014
(2)
Do a check of the parts (Ref 32-13-14/201).
S 328-015
(3)
Make shims if it is necessary (Fig. 801).
S 428-016
(4)
Install the torsion link with shims between the bushing flanges (Fig. 801) (Ref 32-13-14/201).
TASK 32-00-01-308-017
6. Clearance Correction for the Steering Link of the Body Landing Gear
___________________________________________________________________
A. References
(1)
32-53-11/401, Body Gear Steering Actuator and Yoke
(2)
32-53-11/601, Body Gear Steering Actuator and Yoke
(3)
IPC 32-53-11 Fig. 1
B.
Access
(1)
Location Zone
755 Body Landing Gear, LH
765 Body Landing Gear, RH
C.
Procedure
S 028-025
(1)
Remove the steering link (Ref 32-53-11/401).
(2)
Do a check of the parts (Ref 32-53-11/601).
(3)
Make shims if it is necessary (Fig. 801).
S 428-020
(4)
Install the steering link with shims between the bushing flanges (Fig. 801) (Ref 32-53-11/401).
S 228-018
S 328-019
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-00-01
ALL ú ú 01 Page 806 ú Oct 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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本文链接地址：747-400 AMM 飞机维护手册 起落架 LANDING GEAR 1(19)
