曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
SUBTASK 27-31-00-010-004
(4) Remove this access panel:
Number Name/Location
318BR Tailcone Access Door
SUBTASK 27-31-00-860-032
(5) Use the bar, SPL-1677 to set the "B" dimension at 4 units of trim (39.89 +/- 0.01 inches or 1013.2
+/- 0.3 mm) (Figure 502).
SUBTASK 27-31-00-480-004
(6) Install the rig pin E-5 from the rig pin kit, SPL-1585 to the elevator aft quadrant (Figure 507).
H. Input Rods of the Elevator Neutral Shift Mechanism and Output Rod of the Elevator Feel and
Centering Unit
SUBTASK 27-31-00-220-001
(1) Measure the distance "Z" between the centerline of the left neutral shift crank bolt [82] and the
aft side of the vertical bulkhead.
(a) Make sure the distance is 1.25 +/- 0.03 inches (31.8 +/- 0.8 mm).
SUBTASK 27-31-00-820-003
(2) If the distance is not 1.25 +/- 0.03 inches (31.8 +/- 0.8 millimeters), adjust the neutral shift input
rods [84] of the elevator neutral shift mechanism [87] (Figure 507):
(a) Remove the nut [79], washer [78], washer [77], and bolt [76] to disconnect the output rod of
the elevator feel and centering unit [71] from the input crank [75].
(b) Loosen the checknuts on the neutral shift input rods [84].
(c) Remove the nuts [85], washers [86], washers [83], washers [81], and bolts [82] to
disconnect the neutral shift input rods [84] from the neutral shift mechanism crank [87].
(d) Adjust the input rods [84] until you get a "Z" dimension of 1.25 +/- 0.03 inches (31.8 +/- 0.8
mm) at the left input rod [84].
(e) Install the bolts [82], washers [81], washers [83], washers [86], and nuts [85] to connect the
stabilizer position sensor input rods [80] and neutral shift input rods [84] to the neutral shift
mechanism crank [87].
1) Install the lockwire, G01912.
SUBTASK 27-31-00-820-004
(3) Adjust the output rod of the elevator feel and centering unit (Figure 507):
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 537
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(a) If it is not disconnected, remove the nut [79], washer [78], washer [77], and bolt [76] to
disconnect the output rod [74] of the elevator feel and centering unit from the input crank
[75].
(b) Measure the distance between the bolt hole in the output rod [74] and the bolt hole in the
input crank [75]:
(c) If the distance is greater than 0.06 inch (1.5 millimeters), then do these steps:
1) Turn the output rod end half turn relative to the sleeve [73], and the sleeve [73] and the
output rod [74] end together half turn.
2) Make sure the distance of the two bolt holes is less than 0.06 inch (1.5 mm).
3) Keep the number of threads that you can see in the two parts approximately the same.
(d) If the distance is less than 0.06 inch (1.5 mm), then do these steps:
1) Turn the sleeve [73] until you can install the bolt [76] easily.
NOTE: You must always turn the output rod end and sleeve [73] in the same direction.
2) Keep the number of threads that you can see in the two parts are approximately same.
CAUTION: DO NOT TRY TO TIGHTEN THE OUTER BOLT OF THE BOLT [76] AGAIN
AFTER YOU TIGHTEN THE NUT [79]. YOU CAN CAUSE DAMAGE TO THE
EQUIPMENT.
3) Install the bolt [76], washer [77], washer [78], and nut [79] to connect the output rod [74]
to the input crank [75].
a) Tighten the outer bolt of the bolt [76] to 75 - 85 pound-inches (8.5 - 9.6 newtonmeters).
b) Tighten the nut [79] to 15 - 20 pound-inches (1.7 - 2.3 newton-meters).
SUBTASK 27-31-00-820-005
(4) If it is necessary, do this task: Elevator Neutral Shift Sensor Adjustment,
TASK 22-11-14-820-801.
SUBTASK 27-31-00-820-006
(5) If it is necessary, do this task: Stabilizer Position Sensor Adjustment, TASK 22-11-31-820-801.
I. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-00-080-004
(1) Remove the rig pin E-5 from the elevator aft quadrant.
SUBTASK 27-31-00-410-004
(2) Install this access panel:
Number Name/Location
318BR Tailcone Access Door
SUBTASK 27-31-00-940-005
(3) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-31-00-860-033
(4) Do this task: Put the Elevator Systems A and B Back to the Condition Before the Pressure
Removal, TASK 27-31-00-840-802.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 538
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
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册2(142)
