27-31-21
ALL ú ú 01 Page 602 ú Dec 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
HOUSING
ASSEMBLY
3.
BUSHING/ OUTER SHAFT
4.
BEARING/ OUTER SHAFT
5.
SLEEVE/
BEARING
3. BUSHING/ OUTER SHAFT 10. BOND ASSEMBLY/ CAM ASSEMBLY STOP
C-C D-D
Wear Limits for the Elevator Neutral Shift and Override Mechanism
Figure 601 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-31-21
ALL ú ú 01 Page 603 ú Dec 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
INDEX NO. PART NAME DIM. DESIGN LIMITS WEAR LIMITS WORN PART REPLACE PART WORN REPAIR INSTR. REPAIR
DIAMETER ITTED PERM-DIM. WEAR MAX ANCE CLEAR-DIAM
MIN MAX
1 BEARING ID 1.3120 1.3125 1.3136 0.0016 X
SHAFT OD 1.3117 1.3120 1.3104 X
2 BEARING ID 1.3120 1.3125 TBF TBF X
OUTER SHAFT OD 1.3116 1.3120 TBF X
3 BUSHING ID 0.6245 0.6248 TBF TBF X
OUTER SHAFT OD 0.6243 0.6246 TBF X
4 BEARING ID 0.6245 0.6250 0.6260 0.0014 X
OUTER SHAFT OD 0.6243 0.6246 0.6231 X
5 SLEEVE ID 1.0620 1.0625 1.0635 0.0010 X
BEARING OD 1.0620 1.0625 1.0610 X
6 BEARING ID 0.3743 0.3750 0.3754 0.0002 X
OUTER PIN OD 0.3749 0.3752 0.3741 X
7 BUSHING ID 0.6250 0.6255 TBF TBF X
SHAFT OD 0.6245 0.6250 TBF X
8 BEARING ID 0.3743 0.3750 0.3767 0.0024 X
SHAFT OD 0.3738 0.3743 0.3719 X
9 BUSHING ID 0.3743 0.3748 TBF TBF X
SHAFT OD 0.3738 0.3743 TBF X
10 BOND ASSY ID 0.3755 0.3765 TBF TBF X
STOP OD 0.3745 0.3750 TBF X
11 BOND ASSY, STOP ID 0.1900 0.1910 TBF TBF X
BOLT OD 0.1880 0.1895 TBF X
Wear Limits for the Elevator Neutral Shift and Override Mechanism
Figure 601 (Sheet 3)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-31-21
ALL ú ú 01 Page 604 ú Dec 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
CONTROL COLUMN OVERRIDE ASSEMBLY - ADJUSTMENT/TEST
__________________________________________________
1. General_______
A. This procedure contains steps to adjust the override assembly for the control column.
TASK 27-31-23-825-001
2. Adjust the Override Assembly____________________________
A. Equipment
(1)
Force Gage - DPPH-100
Chatillon Inc.
83-30 Kew Garden Rd.
Kew Gardens, New York 11415
(2)
Control Wheel Adapter Equipment (Optional) -A27021-97 or -98
B.
References
(1)
06-41-00/201, Fuselage Access Doors and Panels
(2)
24-22-00/201, Electrical Power - Control
(3)
27-31-00/501, Elevator Control System
C.
Access
(1)
Location Zones
211/212 Control Cabin
113/114 Area Forward of NLG Wheel Well
(2)
Access Panel
113AL Forward Equipment Bay
D.
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 3(131)
