曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

GIMBAL BUSHING
I.D. 1.0000 in
25.40 mm
1.0010 in
25.43 mm
1.0030 in
25.48 mm
0.0050 in
#4 LOWER GIMBAL PIN O.D. 0.9980 in
25.35 mm
0.9990 in
25.37 mm
0.9970 in
25.32 mm
0.127 mm
#5 STRUCTURE
BUSHING
I.D. 0.7500 in
19.05 mm
0.7510 in
19.08 mm
0.7550 in
19.18 mm
0.0060 in
#5 LOWER GIMBAL PIN O.D. 0.7480 in
19.00 mm
0.7490 in
19.02 mm
0.7440 in
18.90 mm
0.152 mm
#6 INBOARD LOWER
GIMBAL BUSHING
I.D. 1.0000 in
25.40 mm
1.0010 in
25.43 mm
1.0050 in
25.53 mm
0.0060 in
#6 LOWER GIMBAL PIN O.D. 0.9980 in
25.35 mm
0.9990 in
25.37 mm
0.9940 in
25.25 mm
0.152 mm
#7 LOWER GIMBAL
BUSHING
I.D. 1.2400 in
31.50 mm
1.2410 in
31.52 mm
1.2440 in
31.60 mm
0.0050 in
#7 SLEEVE O.D. 1.2380 in
31.45 mm
1.2390 in
31.47 mm
1.2370 in
31.42 mm
0.1270 mm
SUBTASK 27-41-81-020-016
(3) Install the stabilizer ball nut and jackscrew gearbox. To install it, do this task: Stabilizer Ball Nut
and Jackscrew Gearbox Installation, TASK 27-41-81-400-801.
------------------------- END OF TASK ---------------------------
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EFFECTIVITY
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Stabilizer Ball Nut and Jackscrew Gearbox Wear Limits
Figure 603 (Sheet 1 of 6)/27-41-81-990-806
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Stabilizer Ball Nut and Jackscrew Gearbox Wear Limits
Figure 603 (Sheet 2 of 6)/27-41-81-990-806
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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D633A101-GUN
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Stabilizer Ball Nut and Jackscrew Gearbox Wear Limits
Figure 603 (Sheet 3 of 6)/27-41-81-990-806
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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D633A101-GUN
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Stabilizer Ball Nut and Jackscrew Gearbox Wear Limits
Figure 603 (Sheet 4 of 6)/27-41-81-990-806
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Stabilizer Ball Nut and Jackscrew Gearbox Wear Limits
Figure 603 (Sheet 5 of 6)/27-41-81-990-806
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Stabilizer Ball Nut and Jackscrew Gearbox Wear Limits
Figure 603 (Sheet 6 of 6)/27-41-81-990-806
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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STABILIZER CONTROL CABLE - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the stabilizer trim control cables
(2) An installation of the stabilizer trim control cables.
B. The stabilizer trim control cables are referred to as the STA and STB cables in this procedure. The
STA cable is located to the left of the STB cable.
C. The stabilizer trim control cable includes the cable with a swaged end connected to the aft cable
drum and an end with an eyelet that connects it to the forward cable drum.
TASK 27-41-82-000-801
2. Stabilizer Control Cable Removal
(Figure 401, Figure 402)
A. References
Reference Title
27-41-71-000-801 Stabilizer Trim Motor Removal (P/B 401)
B. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
COM-1557 Gauge - Force
(Part #: DG-200, Supplier: 92456, A/P Effectivity: 737-ALL)
(Part #: DPP-500G, Supplier: 92456, A/P Effectivity: 737-ALL)
　
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本文鏈接地址：737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飛機維護手冊4(14)