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

Adjustment
Figure 507 (Sheet 1 of 3)/27-31-00-990-809
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 539
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Neutral Shift Mechanism Input Rods and Elevator Feel and Centering Unit Output Rod
Adjustment
Figure 507 (Sheet 2 of 3)/27-31-00-990-809
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 540
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Neutral Shift Mechanism Input Rods and Elevator Feel and Centering Unit Output Rod
Adjustment
Figure 507 (Sheet 3 of 3)/27-31-00-990-809
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 541
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-31-00-820-805
10. Elevator Tab Pushrods - Adjustment
(Figure 502, Figure 503, Figure 505, Figure 512)
NOTE: For each elevator tab, if both pushrods are adjusted, then Elevator Power-Off Flight - Test,
TASK 27-31-00-710-803 is necessary. If only one pushrod is adjusted and you can verify that
the remaining rod has not been replaced or adjusted since the last flight test, then this flight
test is not necessary. If only one pushrod is adjusted and you cannot verify that the
remaining pushrod has not been replaced or adjusted since the last flight test, then the
Elevator Power-Off Flight - Test, TASK 27-31-00-710-803 is necessary.
GUN 156, 201-204, 206 PRE SB 737-55A1080
NOTE: See Figure 508 or Figure 509.
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080
NOTE: See Figure 510.
GUN ALL
A. General
(1) Use this test to adjust the elevator tab pushrods. This task is applicable for the left and right
elevator tab pushrods.
B. References
Reference Title
27-31-00-700-801 Null Procedure - Mach Trim Actuator (P/B 201)
27-31-00-800-802 Remove Pressure from the Elevator Hydraulic Systems A and B
(P/B 201)
27-31-00-840-802 Put the Elevator Systems A and B Back to the Condition Before the
Pressure Removal (P/B 201)
C. 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-1677 Assembly - Trammel Bar, Stabilizer Trim Actuator
(Part #: F80055-1, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
SPL-1686 Fixture - Bar, Elevator Tab
(Part #: C27028-21, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
(Opt Part #: C27028-1, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
(Opt Part #: F80248-8, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500)
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 542
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
D. Location Zones
Zone Area
311 Area Aft of Pressure Bulkhead - Left
312 Area Aft of Pressure Bulkhead - Right
334 Left Horizontal Stabilizer - Elevator
344 Right Horizontal Stabilizer - Elevator
E. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
334PT Horizontal Stabilizer, Tab Control Rod Fairing
344PT Horizontal Stabilizer, Tab Control Rod Fairing, Elevator Sta 34.0
F. Prepare for the Adjustment
SUBTASK 27-31-00-860-034
(1) Do this task: Remove Pressure from the Elevator Hydraulic Systems A and B,
TASK 27-31-00-800-802.
SUBTASK 27-31-00-860-035
(2) Do this task: Null Procedure - Mach Trim Actuator, TASK 27-31-00-700-801.
SUBTASK 27-31-00-010-023
(3) Open this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-31-00-010-005
(4) For the left elevator tab pushrods, remove this access panel:
Number Name/Location
334PT Horizontal Stabilizer, Tab Control Rod Fairing
SUBTASK 27-31-00-010-024
(5) For the right elevator tab pushrods, remove this access panel:
　
中國航空網 m.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2(143)