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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-59-00
Page 515
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Trailing Edge Flap Skew Detection System Test
Figure 503 (Sheet 2 of 2)/27-59-00-990-803
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Page 516
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
FLAP SKEW SENSORS - MAINTENANCE PRACTICES
1. General
A. This procedure has these tasks:
(1) A removal of the outboard flap skew sensor for the outboard flap
(2) An installation of the outboard flap skew sensor for the outboard flap
(3) A removal of the inboard flap skew sensor for the outboard flap
(4) An installation of the inboard flap skew sensor for the outboard flap
(5) A removal of the outboard flap skew sensor for the inboard flap
(6) An installation of the outboard flap skew sensor for the inboard flap
(7) A removal of the inboard flap skew sensor for the inboard flap
(8) An installation of the inboard flap skew sensor for the inboard flap.
B. There are eight flap skew sensors on the trailing edge flaps. One at each of the flap supports.
TASK 27-59-01-000-801
2. Outboard Flap Outboard Skew Sensor Removal
(Figure 201)
A. General
(1) This task is applicable to the flap skew sensors installed on flap supports No. 1 and 8.
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
544 Left Wing - Fairing Flap Support No. 1
644 Right Wing - Fairing Flap Support No. 8
D. Procedure
SUBTASK 27-59-01-860-001
(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.
SUBTASK 27-59-01-040-001
(2) Do this task: Trailing Edge Flap System Deactivation, TASK 27-51-00-040-801.
SUBTASK 27-59-01-860-002
(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 27-59-01-020-001
(4) Disconnect the electrical connector [8] from the flap skew sensor [5].
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EFFECTIVITY
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SUBTASK 27-59-01-020-002
(5) Remove the flap skew sensor [5]:
(a) Remove the bolt [4], washer [3] and washer [1] that attach the jumper wire [2] to the flap
skew sensor [5].
(b) Remove the bolts [6] and washers [7] that attach the flap skew sensor [5] to the sensor
input assembly [10].
(c) Remove the flap skew sensor [5] from the sensor input assembly [10].
------------------------- END OF TASK ---------------------------
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Outboard Flap Outboard Skew Sensor Installation
Figure 201 (Sheet 1 of 2)/27-59-01-990-801
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Oct 10/2003
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Outboard Flap Outboard Skew Sensor Installation
Figure 201 (Sheet 2 of 2)/27-59-01-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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TASK 27-59-01-400-801
3. Outboard Flap Outboard Skew Sensor Installation
(Figure 201)
A. General
(1) This task is applicable to the flap skew sensors installed on flap supports No. 1 and 8.
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
 
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