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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 27-59-01-420-005
(2) Install the flap skew sensor [67]:
(a) Apply grease, D00633 to the packing [70].
(b) Install the packing [70] on the flap skew sensor [67].
(c) Apply grease, D00633 to the shaft of the flap sensor [67] and the splines on the sensor input
assembly [61].
(d) Apply a thin layer of compound, C00913 to the mating surface of the flap skew sensor [67]
and the sensor input assembly [61].
(e) Engage the shaft on the flap skew sensor [67] with the sensor input assembly [61].
NOTE: The shaft has a missing tooth on the splines.
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EFFECTIVITY
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(f) Engage the alignment pin on the sensor input assembly [61] with the hole in the flap skew
sensor [67].
(g) Apply compound, C00913 to the shank and threads of the bolts [64].
(h) Install the bolts [64] and washers [63] to attach the flap skew sensor [67].
(i) Install the bolt [65], washer [66] and washer [69] to attach the jumper wire [68] to the flap
skew sensor [67].
(j) Make sure the bonding resistance between the flap skew sensor [67] and the jumper wire
[68] is less than 8 milliohms.
(k) Apply a bead of sealant, A02315 or sealant, A00247 to the head of the bolt [65].
SUBTASK 27-59-01-210-003
(3) Before you connect the electrical connector [62], 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 27-59-01-420-006
(4) Connect the electrical connector [62] to the flap skew sensor [67].
SUBTASK 27-59-01-860-014
(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 27-59-01-440-003
(6) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
SUBTASK 27-59-01-860-015
(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 27-59-01-730-003
(8) Do this task: Flap Skew Detection System Functional Test, TASK 27-59-00-730-801.
------------------------- END OF TASK ---------------------------
TASK 27-59-01-000-804
8. Inboard Flap Inboard Skew Sensor Removal
(Figure 204)
A. General
(1) This task is applicable to the flap skew sensors installed on flap supports No. 4 and 5.
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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)
32-00-01-480-801 Landing Gear Downlock Pins Installation (P/B 201)
C. Location Zones
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Left
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
541 Left Wing - Fairing Flap Support No. 4
641 Right Wing - Fairing Flap Support No. 5
D. Procedure
SUBTASK 27-59-01-480-001
WARNING: MAKE SURE THE DOWNLOCK PINS ARE INSTALLED ON ALL THE LANDING GEAR.
WITHOUT THE DOWNLOCK PINS, THE LANDING GEAR CAN RETRACT AND CAUSE
INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
(1) If the downlock pins are not installed in the nose and main landing gear, do this task: Landing
Gear Downlock Pins Installation, TASK 32-00-01-480-801.
SUBTASK 27-59-01-040-004
(2) Do this task: Trailing Edge Flap System Deactivation, TASK 27-51-00-040-801.
SUBTASK 27-59-01-860-016
(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 27-59-01-020-007
　
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