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(Part #: F80055-1, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
C. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
311 Area Aft of Pressure Bulkhead - Left
312 Area Aft of Pressure Bulkhead - Right
317 Tail Cone Compartment - Left
318 Tail Cone Compartment - Right
D. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
318BR Tailcone Access Door
737-600/700/800/900
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E. Prepare for the Removal
SUBTASK 27-31-91-860-001
(1) Do this task: Remove Pressure from the Elevator Hydraulic Systems A and B,
TASK 27-31-00-800-802.
SUBTASK 27-31-91-010-001
(2) Remove this access panel:
Number Name/Location
318BR Tailcone Access Door
SUBTASK 27-31-91-010-002
(3) Open this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-31-91-480-001
(4) Use the bar, SPL-1677 to set B dimension at 39.89 +/- 0.01 inches (1013.2 +/- 0.3 millimeters).
SUBTASK 27-31-91-860-002
(5) Open these circuit breakers and install safety tags:
CAPT Electrical System Panel, P18-1
Row Col Number Name
C 2 C00849 AFCS STABILIZER TRIM
C 4 C00456 AFCS SYS A MACH TRIM AC
D 1 C01049 AFCS SYS A WARN LIGHT (BAT)
D 2 C01045 AFCS SYS A FCC DC
D 3 C01048 AFCS SYS A ENGAGE INTLK
D 4 C00457 AFCS SYS A MACH TRIM DC
D 5 C01044 AFCS MCP DC 1
F/O Electrical System Panel, P6-2
Row Col Number Name
B 1 C00374 AFCS SYS B WARN LIGHT (BAT)
B 2 C01064 AFCS SYS B MACH TRIM DC
B 3 C01046 AFCS SYS B FCC DC
B 4 C00716 AFCS SYS B ENGAGE INTLK
B 10 C00207 FLIGHT CONTROL STAB TRIM CONT
C 1 C01037 AFCS SYS B MACH TRIM AC
C 2 C01042 AFCS SYS B SNSR EXC AC
C 3 C01047 AFCS MCP DC 2
D 10 C00840 FLIGHT CONTROL STAB TRIM ACTUATOR
SUBTASK 27-31-91-480-002
(6) Install the lock, SPL-1672 on the stabilizer trim wheel at the control stand (Figure 402):
(a) Turn the stabilizer trim wheel to put the handle at the top of the wheel.
(b) Adjust the height of the lock, SPL-1672 until the yoke is under the handle.
(c) Install the pin through the yoke.
(d) Install the safety pin.
SUBTASK 27-31-91-480-003
(7) Install the rig pin E-5 from the rig pin kit, SPL-1585 in the aft control quadrant, (Figure 401).
737-600/700/800/900
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F. Neutral Shift Mechanism Removal
(Figure 401)
SUBTASK 27-31-91-020-001
(1) Remove the neutral shift mechanism [1]:
(a) Remove the nut [8], washer [9], nut [10], washers [7], and bolt [6] to disconnect the neutral
shift mechanism [1] from the mach trim actuator.
(b) Remove the nuts [28], washers [26], washers [24], and bolts [25] to disconnect control rods
[23] and control rods [27] from the neutral shift mechanism [1].
(c) Remove the nuts [4], washers [3], and bolts [2] that attach the neutral shift mechanism [1] to
the support brackets.
(d) Remove the nuts [13], washers [12], and bolts [11] that attach the neutral shift mechanism
[1] to the support brackets.
(e) Remove the neutral shift mechanism [1] and spacers [17] from the airplane.
NOTE: Note the quantity, orientation, and location of the spacers [17] before you remove
them from the neutral shift mechanism [1].
------------------------- END OF TASK ---------------------------
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Elevator Neutral Shift Mechanism Installation
Figure 401 (Sheet 1 of 6)/27-31-91-990-801
737-600/700/800/900
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Elevator Neutral Shift Mechanism Installation
Figure 401 (Sheet 2 of 6)/27-31-91-990-801
737-600/700/800/900
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Elevator Neutral Shift Mechanism Installation
　
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本文鏈接地址：737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飛機維護手冊3(92)