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SUBTASK 27-59-01-420-004
(4) Connect the electrical connector [38] to the flap skew sensor [35].
SUBTASK 27-59-01-860-009
(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 27-59-01-440-002
(6) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
SUBTASK 27-59-01-860-010
(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 27-59-01-730-002
(8) Do this task: Flap Skew Detection System Functional Test, TASK 27-59-00-730-801.
------------------------- END OF TASK ---------------------------
TASK 27-59-01-000-803
6. Inboard Flap Outboard Skew Sensor Removal
(Figure 203)
A. General
(1) This task is applicable to the flap skew sensors installed on flap supports No. 3 and 6.
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EFFECTIVITY
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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
542 Left Wing - Fairing Flap Support No. 3
642 Right Wing - Fairing Flap Support No. 6
D. Procedure
SUBTASK 27-59-01-860-011
(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 27-59-01-040-003
(2) Do this task: Trailing Edge Flap System Deactivation, TASK 27-51-00-040-801.
SUBTASK 27-59-01-860-012
(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 27-59-01-020-005
(4) Disconnect the electrical connector [62] from the flap skew sensor [67].
SUBTASK 27-59-01-020-006
(5) Remove the flap skew sensor [67]:
(a) Remove the bolt [65], washer [66] and washer [69] that attach the jumper wire [68] to the
flap skew sensor [67].
(b) Remove the bolts [64] and washers [63] that attach the flap skew sensor [67] to the sensor
input assembly [61].
(c) Remove the flap skew sensor [67] from the sensor input assembly [61].
------------------------- END OF TASK ---------------------------
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EFFECTIVITY
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Inboard Flap Outboard Skew Sensor Installation
Figure 203 (Sheet 1 of 2)/27-59-01-990-803
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EFFECTIVITY
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Inboard Flap Outboard Skew Sensor Installation
Figure 203 (Sheet 2 of 2)/27-59-01-990-803
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EFFECTIVITY
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TASK 27-59-01-400-803
7. Inboard Flap Outboard Skew Sensor Installation
(Figure 203)
A. General
(1) This task is applicable to the flap skew sensors installed on flap supports No. 3 and 6.
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)
27-59-00-730-801 Flap Skew Detection System Functional Test (P/B 501)
SWPM 20-60-03 Standard Wiring Practices Manual
C. Consumable Materials
Reference Description Specification
A00247 Sealant - Pressure And Environmental - Chromate
Type
BMS5-95
A02315 Sealant - Low Density, Synthetic Rubber. 2 Part BMS5-142
C00913 Compound - Nondrying Resin Mix Corrosion
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
542 Left Wing - Fairing Flap Support No. 3
642 Right Wing - Fairing Flap Support No. 6
E. Procedure
SUBTASK 27-59-01-860-013
(1) Make sure that these circuit breakers are open:
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737-600-700-800-900 飞机维护手册5 AIRCRAFT MAINTENANCE MANUA(132)
