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

D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(b) For the right wing, open this access panel:
Number Name/Location
611AB Inboard Leading Edge, Lower Removable Access
Panel
F. Leading Edge Flap Proximity Sensor Removal
SUBTASK 27-88-11-020-004
(1) Remove the proximity sensor [44]:
(a) Disconnect the wires at the splice.
(b) To remove the proximity sensor [44] from the leading edge flap, remove the nuts [43],
washers [42], and bolts [41].
(c) To remove the proximity sensor [44] from the structure, remove the washers [42], shim [46]
and bolts [47].
(d) Remove the proximity sensor [44].
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-88-11
Page 418
Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Leading Edge Flap Proximity Sensor Installation
Figure 402 (Sheet 1 of 2)/27-88-11-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-88-11
Page 419
Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Leading Edge Flap Proximity Sensor Installation
Figure 402 (Sheet 2 of 2)/27-88-11-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-88-11
Page 420
Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-88-11-400-802
5. Leading Edge Flap Proximity Sensor Installation
(Figure 402)
A. References
Reference Title
27-81-00-080-801 Leading Edge Flap and Slat Locks Removal (P/B 201)
27-81-00-860-804 Leading Edge Flaps and Slats Retraction (P/B 201)
B. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
SPL-1734 Lockout Set - Leading Edge Slats and Krueger Flaps Actuators
(Part #: C27051-29, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
(Opt Part #: C27051-1, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -BBJ)
C. Consumable Materials
Reference Description Specification
A00165 Adhesive - Neoprene BMS5-7 Type I
C00913 Compound - Nondrying Resin Mix Corrosion
Inhibiting Material
BMS3-27
D. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
512 Left Wing - Krueger Flap No. 2
513 Left Wing - Krueger Flap No. 1
612 Right Wing - Krueger Flap No. 3
613 Right Wing - Krueger Flap No. 4
E. Access Panels
Number Name/Location
511AB Inboard Leading Edge, Lower Removable Panel
611AB Inboard Leading Edge, Lower Removable Access Panel
F. Leading Edge Flap Proximity Sensor Installation
SUBTASK 27-88-11-420-004
(1) Install the flap proximity sensor [44]:
(a) Apply a thin coat of compound, C00913 to the threads of the bolts [41] or [47].
(b) To install the proximity sensor [44] on the leading edge flap, install the bolts [41], washers
[42] and nuts [43].
(c) To install the proximity sensor [44] on the structure, install the bolts [47], shim [46] and
washers [42].
(d) Find the same color wires and make a splice.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-88-11
Page 421
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(e) Attach the wires together to make a bundle.
SUBTASK 27-88-11-820-001
(2) With the flap in the extend position, make sure the gap between the proximity sensor [44] and the
target [45] is 0.115-0.135 inch (2.92-3.43 millimeters).
(a) If the gap is out of tolerance, adjust the gap between the proximity sensor [44] and the
target [45].
1) Remove the bolts [47], washers [42] and shim [46].
2) Add or remove shim [46] as it is necessary to get the correct gap between the proximity
sensor [44] and the target [45].
3) Install the bolts [47] and washers [42].
4) Bond shims [46] to the support bracket with adhesive, A00165.
G. Put the Airplane Back to Its Usual Condition
SUBTASK 27-88-11-080-002
WARNING: CAREFULLY REMOVE THE LEADING EDGE FLAP ACTUATOR LOCK TO PREVENT
ACCIDENTAL OPERATION OF THE LEADINGE EDGE FLAPS. THE LEADING EDGE
　
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7 AIRCRAFT MAINTENANCE MANUA(113)