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

Inhibiting Material
BMS3-27
D00633 Grease - Aircraft General Purpose BMS3-33
G50171 Compound - Corrosion Inhibiting Compound,
Interior Application - D5026NS or ZC-026
D. Location Zones
Zone Area
544 Left Wing - Fairing Flap Support No. 1
644 Right Wing - Fairing Flap Support No. 8
E. Procedure
SUBTASK 27-59-01-860-003
(1) Make sure that these circuit breakers are open:
F/O Electrical System Panel, P6-2
Row Col Number Name
A 11 C01443 FC TE FLAP POS/SKEW SNSR & IND RIGHT
A 12 C00213 FC TE FLAP POS/SKEW SNSR & IND LEFT
SUBTASK 27-59-01-420-001
(2) Install the flap skew sensor [5]:
(a) Apply grease, D00633 to the packing [9].
(b) Install the packing [9] on the flap skew sensor [5].
(c) Apply grease, D00633 to the shaft of the flap skew sensor [5] and the splines on the sensor
input assembly [10].
(d) Apply a thin layer of compound, C00913 to the mating surface of the flap skew sensor [5]
and the sensor input assembly [10].
(e) Engage the shaft on the flap skew sensor [5] with the sensor input assembly [10].
NOTE: The shaft has a missing tooth on the splines.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-59-01
Page 205
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(f) Engage the alignment pin on the sensor input assembly [10] with the hole in the flap skew
sensor [5].
(g) Apply compound, C00913 to the shank and threads of the bolts [6].
(h) Install the bolts [6] and washers [7] to attach the flap skew sensor [5].
(i) Install the bolt [4], washer [3] and washer [1] to attach the jumper wire [2] to the flap skew
sensor [5].
(j) Make sure the bonding resistance between the flap skew sensor [5] and the jumper wire [2]
is less than 8 milliohms.
(k) Apply a bead of sealant, A02315 or sealant, A00247 to the head of the bolt [4].
SUBTASK 27-59-01-210-001
(3) Before you connect the electrical connector [8], examine the connector for corrosion.
WARNING: DO THE STEPS BELOW IF THE AIRPLANE OPERATES AT AIRPORTS WHERE
DEICING FLUID THAT CONTAIN POTASSIUM FORMATE IS USED. ALSO DO THE
STEPS FOR ALL AIRPLANES THAT YOU FOUND CORROSION IN THE
ELECTRICAL CONNECTORS IN THE MAIN WHEEL WELL. THE ELECTRICAL
CONNECTOR IS PART OF A SYSTEM THAT IS NECESSARY FOR SAFE FLIGHT.
(a) If there was corrosion, refer to (SWPM 20-60-03) to correct the problem.
(b) Apply the D5026NS or ZC-026 compound, G50171 to the connector (SWPM 20-60-03).
SUBTASK 27-59-01-420-002
(4) Connect the electrical connector [8] to the flap skew sensor [5].
SUBTASK 27-59-01-860-004
(5) Remove the safety tags and close these circuit breakers:
F/O Electrical System Panel, P6-2
Row Col Number Name
A 11 C01443 FC TE FLAP POS/SKEW SNSR & IND RIGHT
A 12 C00213 FC TE FLAP POS/SKEW SNSR & IND LEFT
SUBTASK 27-59-01-440-001
(6) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
SUBTASK 27-59-01-860-005
(7) Retract the trailing edge flaps to the UP position. To retract the flaps, do this task: Retract the
Trailing Edge Flaps, TASK 27-51-00-860-804.
SUBTASK 27-59-01-730-001
(8) Do this task: Flap Skew Detection System Functional Test, TASK 27-59-00-730-801.
------------------------- END OF TASK ---------------------------
TASK 27-59-01-000-802
4. Outboard Flap Inboard Skew Sensor Removal
(Figure 202)
A. General
(1) This task is applicable to the flap skew sensors installed on flap supports No. 2 and 7.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-59-01
Page 206
Feb 10/2004
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
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)
C. Location Zones
Zone Area
543 Left Wing - Fairing Flap Support No. 2
643 Right Wing - Fairing Flap Support No. 7
D. Procedure
SUBTASK 27-59-01-860-006
(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.
SUBTASK 27-59-01-040-002
(2) Do this task: Trailing Edge Flap System Deactivation, TASK 27-51-00-040-801.
SUBTASK 27-59-01-860-007
(3) Open these circuit breakers and install safety tags:
F/O Electrical System Panel, P6-2
Row Col Number Name
A 11 C01443 FC TE FLAP POS/SKEW SNSR & IND RIGHT
A 12 C00213 FC TE FLAP POS/SKEW SNSR & IND LEFT
SUBTASK 27-59-01-020-003
　
中國航空網 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(130)