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(4) Disconnect the electrical connector [93] from the flap skew sensor [100].
SUBTASK 27-59-01-020-008
(5) Remove the flap skew sensor [100]:
(a) Remove the bolt [99], washer [98] and washer [96] that attach the jumper wire [97] to the
flap skew sensor [100].
(b) Remove the bolts [91] and washers [92] that attach the flap skew sensor [100] to the sensor
input assembly [94].
(c) Remove the flap skew sensor [100] from the sensor input assembly [94].
------------------------- END OF TASK ---------------------------
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Inboard Flap Inboard Skew Sensor Installation
Figure 204 (Sheet 1 of 2)/27-59-01-990-804
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Inboard Flap Inboard Skew Sensor Installation
Figure 204 (Sheet 2 of 2)/27-59-01-990-804
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TASK 27-59-01-400-804
9. Inboard Flap Inboard Skew Sensor Installation
(Figure 204)
A. General
(1) This task is applicable to the flap skew sensors installed on flap supports No. 4 and 5.
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. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
95 Packing 27-59-00-04-034 GUN ALL
100 Sensor 27-59-00-04-022 GUN ALL
E. 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
F. Procedure
SUBTASK 27-59-01-860-017
(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 27-59-01-420-007
(2) Install the flap skew sensor [100]:
(a) Apply grease, D00633 to the packing [95].
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(b) Install the packing [95] on the flap skew sensor [100].
(c) Apply grease, D00633 to the shaft of the flap skew sensor [100] and the splines on the
sensor input assembly [94].
(d) Apply a thin layer of compound, C00913 to the mating surface of the flap skew sensor [100]
and the sensor input assembly [94].
(e) Engage the shaft on the flap skew sensor [100] with the sensor input assembly [94].
NOTE: The shaft has a missing tooth on the splines.
(f) Engage the alignment pin on the sensor input assembly [94] with the hole in the flap skew
sensor [100].
(g) Apply compound, C00913 to the shank and threads of the bolts [91].
(h) Install the bolts [91] and washers [92] to attach the flap skew sensor [100].
(i) Install the bolt [99], washer [98] and washer [96] to attach the jumper wire [97] to the flap
skew sensor [100].
(j) Make sure the bonding resistance between the flap skew sensor [100] and the jumper wire
[97] is less than 8 milliohms.
(k) Apply a bead of sealant, A02315 or sealant, A00247 to the head of the bolt [99].
SUBTASK 27-59-01-210-004
(3) Before you connect the electrical connector [93], 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
　
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