曝光臺 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者

544CR Flap Support No. 1 Access Cover
644CL Flap Support No. 8, Access Cover
644CR Flap Support No. 8, Access Cover
(b) Remove the bolts [14] that attach the access cover [3] and access cover [20] to the aft
fairing assembly [2].
(c) Remove the access cover [3] and access cover [20].
SUBTASK 27-51-28-020-003
(5) Remove the aft fairing assembly [2]:
(a) Support the aft fairing assembly [2].
(b) Disconnect the aft end of the aft fairing assembly [2]:
1) Remove the nut [30], washer [29], washer [27], bolt [26] and bushing [28] that attach the
drive rod assembly [32] to the carriage [25].
2) Remove the nut [39], washer [38], washer [36], bolt [35] and bushing [37] that attach the
attach beam assembly [33] to the flap track [7].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-28
Page 410
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(c) Disconnect the forward end of the aft fairing assembly [2]:
1) Remove the nut [19] and washer [18] from the pivot bolt [15].
2) Remove the pivot bolt [15], washer [16] and bushing [17] that attach the aft fairing
assembly [2] to the transmission attach fitting [10].
(d) Lower the aft fairing assembly [2] until you can get access to the nuts [11] on the jumper
wires [22].
(e) Remove the nuts [11] and washers [12] that attach the jumper wires [22].
(f) Remove the jumper wires [22] from the studs.
(g) Lower the aft fairing assembly [2].
SUBTASK 27-51-28-020-004
(6) If you will install a new aft fairing assembly [2], remove the fairing drive linkage from the aft
fairing assembly [2]:
NOTE: The fairing drive linkage includes the drive rod assembly [32], adjust link assembly [41],
adjust rod assembly [42] and the attach beam assembly [33].
(a) Remove the nut [47], washer [46], washer [44], bolt [43] and bushing [45] that attach the
adjust rod assembly [42] to the aft fairing assembly [2].
(b) Remove the adjust link assembly [41] from the aft fairing assembly [2]:
1) Remove the nut [57] and washer [58] from the bolt [62].
2) Remove the bolt [62], washer [63], washer [64] and washers [55].
NOTE: Make a note of the thickness and location of the washers [55].
3) Remove the bushing [60] and bushing [61] from the aft fairing assembly [2].
(c) Remove the nut [53], washer [52], washer [50], bolt [49] and bushing [51] that attach the
adjust link assembly [41] to the attach beam assembly [33].
(d) Remove the nut [30], washer [29], washer [27], bolt [26] and bushing [28] that attach the
drive rod assembly [32] to the attach beam assembly [33].
(e) Remove the nut [47], washer [46], washer [44], bolt [43] and bushing [45] that attach the
adjust rod assembly [42] to the adjust link assembly [41].
SUBTASK 27-51-28-010-003
(7) If it is necessary, remove the tailcone assembly [67] from the aft fairing assembly [2]:
(a) Remove the bolts [68] that attach the tailcone assembly [67] to the aft fairing assembly [2].
(b) Remove the tailcone assembly [67] from the aft fairing assembly [2].
------------------------- END OF TASK ---------------------------
TASK 27-51-28-400-802
5. Outboard Flap Outboard Support Aft Fairing Installation
(Figure 401)
A. General
(1) This task is applicable to the aft fairing on the No. 1 and No. 8 flap supports.
B. References
Reference Title
27-51-00-440-801 Trailing Edge Flap System Reactivation (P/B 201)
27-51-00-860-804 Retract the Trailing Edge Flaps (P/B 201)
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-28
Page 411
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(Continued)
Reference Title
27-51-28-820-801 Outboard Flap Outboard Support Fairing Adjustment (P/B 501)
C. Consumable Materials
Reference Description Specification
A02315 Sealant - Low Density, Synthetic Rubber. 2 Part BMS5-142
D00013 Grease - Aircraft And Instrument Grease MIL-PRF-23827
(NATO G-354)
(Supersedes
MIL-G-23827)
D00633 Grease - Aircraft General Purpose BMS3-33
D. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
2 Fairing assembly 27-51-28-01-210 GUN 001-028, 101-121,
155-157, 201-999
27-51-28-01-215 GUN 001-028, 101-121,
155-157, 201-999
15 Bolt 27-51-28-01-115 GUN 001-028, 101-121,
155-157, 201-999
31 Pin 27-51-28-01-110 GUN 001-028, 101-121,
155-157, 201-999
27-51-28-01-430 GUN 001-028, 101-121,
155-157, 201-999
32 Rod assembly 27-51-28-01-395 GUN 001-028, 101-121,
155-157, 201-999
　
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 飛機維護手冊5 AIRCRAFT MAINTENANCE MANUA(31)