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

CAN BECOME DISCONNECTED AND CAUSE DAMAGE TO THE ELEVATOR AND
STABILIZER.
(e) Tighten the new nuts [47] to 70 - 80 pound-inches (7.9 - 9.0 newton-meters).
GUN ALL
(f) Install the screws [48] to attach the pin retainers [49] to the elevator tab control mechanism
[32].
(g) Install the bushings [27], bolts [28], washers [26] and new nuts [25] to connect the tab
pushrods [29] to the elevator tab [22].
NOTE: The inboard bolt is installed with the head inboard and the outboard bolt is
installed with the head outboard.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-34
Page 419
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
GUN 156, 201-204, 206 PRE SB 737-55A1080
CAUTION: IF THE NEW NUTS [25] ARE NOT TIGHTENED CORRECTLY, THEN THE PUSHRODS
CAN BECOME DISCONNECTED AND CAUSE DAMAGE TO THE ELEVATOR AND
STABILIZER.
(h) Tighten the new nuts [25] to 30 - 50 pound-inches (3.4 - 5.7 newton-meters) and install new
pins [53].
NOTE: Make sure the new nuts [25] stay tightened to 30 - 50 pound-inches (3.4 - 5.7
newton-meters) after alignment of the nut [25] and cotter pin hole in the bolt [28].
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080
CAUTION: IF THE NEW NUTS [25] ARE NOT TIGHTENED CORRECTLY, THEN THE PUSHRODS
CAN BECOME DISCONNECTED AND CAUSE DAMAGE TO THE ELEVATOR AND
STABILIZER.
(i) Tighten the new nuts [25] to 70 - 80 pound-inches (7.9 - 9.0 newton-meters) and install new
pins [53] in the anti-rotation boss at the head of the bolt [28].
GUN ALL
SUBTASK 27-31-34-080-003
(3) Remove rig pin E-5 of the rig pin kit, SPL-1585 from the aft control quadrant (Figure 401).
SUBTASK 27-31-34-820-002
(4) Adjust the tab pushrods until you get the same tab position that you measured before you
removed the elevator tab pushrods. To adjust them, do this task: Elevator Tab Pushrods -
Adjustment, TASK 27-31-00-820-805.
SUBTASK 27-31-34-420-005
(5) Install the bolts [24] to attach the access panel [23] to the elevator [21].
SUBTASK 27-31-34-730-009
(6) Do this task: Elevator Travel Limit - Test, TASK 27-31-00-700-804.
SUBTASK 27-31-34-730-010
(7) Do this task: Elevator Tab Linkage - Test, TASK 27-31-00-700-806.
SUBTASK 27-31-34-730-011
(8) Do this task: Control Column Power Force - Test, TASK 27-31-00-700-809.
F. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-34-410-008
(1) For the left elevator, install this access panel:
Number Name/Location
333BB Horizontal Stabilizer, Access Panel, Trailing Edge
SUBTASK 27-31-34-410-009
(2) For the right elevator, install this access panel:
Number Name/Location
343BB Horizontal Stabilizer, Access Panel - T.E. Area
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-34
Page 420
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-31-34-410-012
(3) Close this access panel:
Number Name/Location
318BR Tailcone Access Door
SUBTASK 27-31-34-730-012
(4) Do this task: Elevator Power-Off Flight - Test, TASK 27-31-00-710-803.
------------------------- END OF TASK ---------------------------
TASK 27-31-34-000-804
6. Elevator Tab Lock Actuator - Removal
(Figure 401, Figure 409)
GUN 156, 201-204, 206 PRE SB 737-55A1080; AIRPLANES WITH FOUR ELEVATOR TAB HINGES
NOTE: Also see Figure 402, Figure 404 and Figure 407.
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080; AIRPLANES
WITH THE SIX HINGE ELEVATOR TAB WITH RECTANGULAR HEAD BOLTS
NOTE: Also see Figure 403, Figure 405 and Figure 408.
GUN ALL
A. References
Reference Title
27-31-00-710-803 Elevator Power-Off Flight - Test (P/B 501)
27-31-00-800-802 Remove Pressure from the Elevator Hydraulic Systems A and B
(P/B 201)
27-31-00-820-805 Elevator Tab Pushrods - Adjustment (P/B 501)
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
SPL-1585 Kit - Rigging Pins, All Systems
(Part #: F70207-109, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
C. Location Zones
Zone Area
318 Tail Cone Compartment - Right
333 Left Horizontal Stabilizer - Rear Spar to Trailing Edge
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飛機維護手冊3(60)