曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費(fèi)者

E. Prepare for the Removal
SUBTASK 27-51-11-860-001
(1) Extend the trailing edge flaps to the 40-unit position. To extend them, do this task: Extend the
Trailing Edge Flaps, TASK 27-51-00-860-803.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-11
Page 401
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-51-11-040-001
(2) Do this task: Trailing Edge Flap System Deactivation, TASK 27-51-00-040-801.
SUBTASK 27-51-11-860-002
(3) Use the manual drive system to extend the trailing edge flaps to the stops on the ballscrews. To
extend the flaps, do this task: Trailing Edge Flap System Manual Operation,
TASK 27-51-00-980-801.
SUBTASK 27-51-11-010-001
(4) Do this task: Inboard Flap Support Aft Fairing Removal, TASK 27-51-18-000-802.
SUBTASK 27-51-11-010-002
(5) Remove these panels from the wing to body fairing:
Number Name/Location
194BL Flap Track Lubrication Panel - Aft
194CL Aft Wing To Body Fairing Panel
or open these access panels:
Number Name/Location
194BR Flap Track Lubrication Panel - Aft
194CR Aft Wing To Body Fairing Panel
F. Inboard Trailing Edge Flap Removal
SUBTASK 27-51-11-020-006
(1) Disconnect the skew control rods for the skew mechanisms from the carriages (Figure 401):
(a) At the outboard carriage [13], remove the nut [8], washer [7], washer [5], bolt [4] and
bushing [6] that attaches the skew control rod [3] to the carriage [13].
(b) At the inboard carriage [52], remove the nut [47], washer [46], washer [44], bolt [43] and
bushing [45] that attaches the skew control rod [41] to the carriage [52].
SUBTASK 27-51-11-020-002
(2) Disconnect the aft flap drive rod [25] from the crankshaft [18]:
(a) Remove the pin [24], nut [23], washer [22], washer [20], bolt [19] and bushing [21] from the
crankshaft [18].
(b) Move the aft flap drive rod [25] away from the inboard flap assembly [1].
SUBTASK 27-51-11-980-002
(3) If the aft flap [2] is installed, move the aft flap [2] to the retracted position on the inboard flap
assembly [1]:
(a) Move the crankshaft [18] aft until the aft flap [2] is in the retracted position.
CAUTION: DO NOT USE A RIG PIN IN THE CRANKSHAFT TO HOLD THE AFT FLAP IN THE
RETRACTED POSITION. THIS CAN CAUSE DAMAGE TO THE CRANKSHAFT OR
THE FITTING ON THE MAIN FLAP.
(b) Install the restraint strap (part of the sling, SPL-1729) to hold the aft flap [2] in the retracted
position.
SUBTASK 27-51-11-480-001
(4) Install the sling, SPL-1729 [82] on the inboard flap assembly [1] (Figure 402):
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-11
Page 402
Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(a) Remove the existing bolts [85] at the inboard and outboard ends of the front spar on the
inboard flap assembly [1].
NOTE: Keep these bolts [85] for re-installation.
(b) Install the sling fittings [81] in the location of the bolts [85].
(c) Remove the existing bolts [86] at the rear spar at the aft end of the inboard flap
assembly [1].
NOTE: Keep these bolts [86] for re-installation.
(d) Install the sling fitting [84] in the location of the bolts [86].
(e) Connect the sling, SPL-1729 [82] to the sling fittings [81] and sling fitting [84].
(f) Connect the sling, SPL-1729 [82] to a 30 foot height (2000 lbs capacity) lift crane, STD-1095.
(g) Use the sling, SPL-1729 [82] to hold the weight of the inboard flap assembly [1].
SUBTASK 27-51-11-020-003
(5) Remove the stop fittings from the flap tracks (Figure 401):
(a) On the inboard flap track [39], remove the nut [56], washer [55], bushings [54] and bolt [53]
from the end of the flap track [39].
(b) On the outboard flap track [14], remove the roller stop [30], roller stop [37] and the aft fairing
support fitting [35]:
1) Remove the nuts [29], washers [28], bolt [27] and bolts [36] that attach the aft fairing
support fitting [35] to the flap track [14].
2) Remove the nuts [34], washers [33], washers [32] and bolts [31] that attach the aft
fairing support fitting [35], roller stop [30] and roller stop [37] to the flap track [14].
3) Remove the roller stop [30], roller stop [37] and the aft fairing support fitting [35] from
the flap track [14].
SUBTASK 27-51-11-020-004
(6) Remove the inboard flap assembly [1]:
(a) Hold the weight of the inboard flap assembly [1] with the sling, SPL-1729 [82] and 30 foot
height (2000 lbs capacity) lift crane, STD-1095.
(b) Disconnect the inboard carriage [52] from the gimbal [40]:
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飛機(jī)維護(hù)手冊(cè)4(84)