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

(b) Apply a layer of grease, D00633 to the mating surfaces of the yoke [4] and the ballscrew
assembly [2].
(c) Put the ballscrew assembly [2] into the yoke [4].
(d) Apply a layer of grease, D00633 to the shank and threads of the bolts [16].
(e) Install the bolts [16], washers [17], washers [18] and nuts [19] to attach the ballscrew
assembly [2] to the yoke [4].
(f) Make sure the ballscrew assembly [2] is installed correctly in the yoke [4]:
1) Turn the transmission [3] until the nut [21] on the U-joint [20] is down.
2) Turn the ballscrew nut [13] until the upstop is 1808 from the upstop [22] on the yoke [4].
3) If the ball returns on the ballscrew nut [13] are not on the outboard side, change the
position of the ballscrew assembly [2]:
a) Remove the nuts [19], washers [18], washers [17] and bolts [16] that attach the
ballscrew assembly [2] to the yoke [4].
b) Turn the ballscrew assembly [2] 1808 in the yoke [4].
c) Install the bolts [16], washers [17], washers [18] and nuts [19].
(g) Tighten the nuts [19].
SUBTASK 27-51-42-420-003
(3) Connect the ballscrew assembly [2] with the gimbal assembly [14] to the carriage [1]:
(a) Move the gimbal assembly [14] aft on the ballscrew assembly [2] until it is at the downstop.
(b) On transmission No. 1, make sure the ball returns on the ballscrew nut [13] are on the
outboard side.
(c) On transmission No. 8, make sure the ball returns on the ballscrew nut [13] are on the
inboard side.
GUN 155 PRE SB 737-57-1264
(d) Apply grease, D00633 to the inside and outside surfaces of the carriage bushing [9] and
carriage bushing [15].
GUN 001-099, 101-122, 156, 157, 201-999; GUN 155 POST SB 737-57-1264
(e) Apply grease, D00633 to the outside surfaces of the carriage bushing [9] and carriage
bushing [15]
GUN ALL
(f) Lift the outboard flap until the carriage [1] aligns with the gimbal assembly [14].
(g) Install the carriage bushing [9] and carriage bushing [15] to attach the gimbal assembly [14]
to the carriage [1].
(h) Install the bolts [6], washers [7] and nuts [8] to hold the carriage bushing [9] and carriage
bushing [15] in the carriage [1].
(i) Tighten the nuts [8] to 65-75 pound-inches (7.4-8.4 newton-meters) more than the run on
torque.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-42
Page 408
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-51-42-640-001
(4) Lubricate the transmission [3], ballscrew assembly [2] and gimbal assembly [14]. To lubricate
them, do this task: Outboard Flap Outboard Ballscrew and Gimbal Lubrication,
TASK 12-22-51-640-805.
SUBTASK 27-51-42-820-001
(5) Do this task: Trailing Edge Flap Drive System Adjustment, TASK 27-51-00-820-802.
G. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-42-410-001
(1) Do this task: Outboard Flap Outboard Support Aft Fairing Installation, TASK 27-51-28-400-802.
SUBTASK 27-51-42-440-001
(2) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
SUBTASK 27-51-42-860-002
WARNING: KEEP PERSONS AND EQUIPMENT CLEAR OF THE FLIGHT CONTROL SURFACES, THE
THRUST REVERSERS, AND THE LANDING GEAR. THESE COMPONENTS CAN MOVE
SUDDENLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURIES TO
PERSONS AND DAMAGE TO EQUIPMENT.
(3) Supply system B hydraulic power, do this task: Hydraulic System A or B Pressurization,
TASK 29-11-00-860-801.
SUBTASK 27-51-42-860-003
(4) Use the primary system to retract the flaps to the retracted position. To retract the flaps, do this
task: Trailing Edge Flap System Operation With Primary Control, TASK 27-51-00-860-801.
SUBTASK 27-51-42-860-004
(5) Use the primary system to extend and retract the flaps. To extend and retract the flaps, do this
task: Trailing Edge Flap System Operation With Primary Control, TASK 27-51-00-860-801.
SUBTASK 27-51-42-860-005
(6) Remove system B hydraulic power, do this task: Hydraulic System A or B Power Removal,
TASK 29-11-00-860-805.
------------------------- END OF TASK ---------------------------
TASK 27-51-42-000-802
4. Outboard Flap Inboard Ballscrew and Gimbal Removal
(Figure 402)
A. General
(1) This task is applicable to the ballscrew and gimbal at flap supports No. 2 and 7.
B. References
Reference Title
27-51-00-040-801 Trailing Edge Flap System Deactivation (P/B 201)
27-51-00-860-803 Extend the Trailing Edge Flaps (P/B 201)
27-51-00-980-801 Trailing Edge Flap System Manual Operation (P/B 201)
27-51-28-000-804 Outboard Flap Inboard Support Aft Fairing Removal (P/B 401)
737-600/700/800/900
　
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 飛機維護手冊5 AIRCRAFT MAINTENANCE MANUA(66)