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时间:2010-08-24 13:01来源:蓝天飞行翻译 作者:admin
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1) Apply grease, D00633 to the coupling sleeve [15].
2) Put the splined coupling [16] in the coupling sleeve [15].
3) Install the screws [14] to attach the torque tube to the transmission.
4) Install lockwire on the screws [14].
SUBTASK 27-51-00-820-013
(7) Move the flap drive system to the retracted position (Figure 502):
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AIRCRAFT MAINTENANCE MANUAL
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
WARNING: DO NOT RETRACT THE POWER DRIVE UNIT PAST THE RIG MARK IN THE UP
DIRECTION. YOU CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO
EQUIPMENT.
(a) Use the manual drive on the flap power drive unit [17] to retract it to the retracted position.
NOTE: The flap power drive unit is in the retracted position when the black rig mark on
the cable drum [12] extends past the white cable guard [13] a minimum of 0.03
inches (0.76 millimeters) on each side.
(b) Use an adapter, SPL-1679 on the torque tube couplings inboard of the tee-angle gearbox to
retract the left and right wings to the retracted position.
NOTE: The flap drive systems for the wings are in the retracted position when the
ballscrew nuts are 1/2 turn +/- 10 degrees from the upstop on the yoke.
1) Retract the flap drive systems until the ballscrew nuts for transmission No. 4 and
transmission No. 5 are approximately 1/2 turn from the upstop on the yokes.
2) Make sure the distance from the upstop for transmission No. 4 and transmission No. 5
are the same in the limit of 0.10 inch (2.54 millimeters).
SUBTASK 27-51-00-820-014
(8) Connect the torque tubes [18] to the flap power drive unit [17]:
NOTE: This will connect the flap drive system for the left wing to the right wing.
(a) Apply grease, D00633 to the coupling sleeves [15].
(b) Put the splined coupling [16] in the coupling sleeve [15].
(c) Install the screws [14] to attach the torque tube [18] to the power drive unit [17].
(d) Install lockwire on the screws [14].
SUBTASK 27-51-00-210-010
(9) Make sure the torque trip indicators on the transmissions are set.
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-00-420-004
(1) For the flap position transmitters on the left and the right wing, do this task: Flap Position
Transmitter Installation, TASK 27-58-01-400-801.
SUBTASK 27-51-00-440-003
(2) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
------------------------- END OF TASK ---------------------------
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Trailing Edge Flap Drive System Adjustment
Figure 503 (Sheet 1 of 6)/27-51-00-990-806
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL; AIRPLANES WITH VERTICAL TORQUE TRIP
INDICATORS
27-51-00
Page 534
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Trailing Edge Flap Drive System Adjustment
Figure 503 (Sheet 2 of 6)/27-51-00-990-806
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL; AIRPLANES WITH HORIZONTAL TORQUE TRIP
INDICATORS
27-51-00
Page 535
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Trailing Edge Flap Drive System Adjustment
Figure 503 (Sheet 3 of 6)/27-51-00-990-806
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL; AIRPLANES WITH VERTICAL TORQUE TRIP
INDICATORS
27-51-00
Page 536
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Trailing Edge Flap Drive System Adjustment
Figure 503 (Sheet 4 of 6)/27-51-00-990-806
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL; AIRPLANES WITH HORIZONTAL TORQUE TRIP
INDICATORS
27-51-00
Page 537
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Trailing Edge Flap Drive System Adjustment
Figure 503 (Sheet 5 of 6)/27-51-00-990-806
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-00
Page 538
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Trailing Edge Flap Drive System Adjustment
Figure 503 (Sheet 6 of 6)/27-51-00-990-806
 
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