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the off position.
GUN ALL
I. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-00-080-003
(1) Remove the rig pin E-5 from the elevator aft quadrant.
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EFFECTIVITY
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SUBTASK 27-31-00-410-003
(2) Install this access panel:
Number Name/Location
318BR Tailcone Access Door
SUBTASK 27-31-00-940-004
(3) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-31-00-860-029
(4) Do this task: Put the Elevator Hydraulic systems A and B Back to the Condition Before the
Pressurization, TASK 27-31-00-840-801.
------------------------- END OF TASK ---------------------------
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EFFECTIVITY
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Elevator PCU Input Rods Adjustment
Figure 506 (Sheet 1 of 3)/27-31-00-990-808
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EFFECTIVITY
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Elevator PCU Input Rods Adjustment
Figure 506 (Sheet 2 of 3)/27-31-00-990-808
737-600/700/800/900
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EFFECTIVITY
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Elevator PCU Input Rods Adjustment
Figure 506 (Sheet 3 of 3)/27-31-00-990-808
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EFFECTIVITY
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TASK 27-31-00-820-804
9. Input Rods of the Elevator Neutral Shift Mechanism and Output Rod of the Feel and Centering Unit -
Adjustment
(Figure 502, Figure 507)
A. General
(1) Use this test to adjust the input rods which connect the elevator neutral shift mechanism to the
stabilizer. This test also includes steps to adjust the output rod which connects the elevator feel
and centering unit to the input torque tube.
B. References
Reference Title
22-11-14-820-801 Elevator Neutral Shift Sensor Adjustment (P/B 501)
22-11-31-820-801 Stabilizer Position Sensor Adjustment (P/B 501)
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-1585 Kit - Rigging Pins, All Systems
(Part #: F70207-109, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
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)
D. Consumable Materials
Reference Description Specification
G01912 Lockwire - Monel (0.032 In. Dia.) NASM20995N~
C32
(QQ-N-281)
E. Location Zones
Zone Area
311 Area Aft of Pressure Bulkhead - Left
312 Area Aft of Pressure Bulkhead - Right
317 Tail Cone Compartment - Left
318 Tail Cone Compartment - Right
F. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
318BR Tailcone Access Door
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G. Prepare for the Adjustment
SUBTASK 27-31-00-860-030
(1) Do this task: Remove Pressure from the Elevator Hydraulic Systems A and B,
TASK 27-31-00-800-802.
SUBTASK 27-31-00-860-031
(2) Do this task: Null Procedure - Mach Trim Actuator, TASK 27-31-00-700-801.
SUBTASK 27-31-00-010-035
(3) Open this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
　
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本文鏈接地址：737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飛機維護手冊2(141)