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A 11 C01443 FC TE FLAP POS/SKEW SNSR & IND RIGHT
A 12 C00213 FC TE FLAP POS/SKEW SNSR & IND LEFT
SUBTASK 27-59-02-420-009
(2) Install the sensor input assembly [81]:
(a) Apply a layer of compound, C00913 to the mating surface of the sensor input assembly [81]
and the flap track [90].
(b) Apply compound, C00913 to the shank and threads of the bolts [99].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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(c) Put the sensor input assembly [81] in its location on the flap track [90].
(d) Install the bolts [99], washers [100], washers [101] and nuts [102] that attach the sensor
input assembly [81] to the flap track [90].
(e) Install the bolt [85], washer [86], washer [87], washer [88] and nut [89] to attach the jumper
wire [84] and the sensor input assembly [81] to the flap track [90].
NOTE: Install the washer [87] under the jumper wire [84].
(f) Make sure the bonding resistance between the flap track [90] and the jumper wire [84] is
less than 8 milliohms.
(g) Apply a bead of sealant, A02315 or sealant, A00247 around the bolt [85] and the nut [89].
SUBTASK 27-59-02-420-010
(3) Install the control rod [92]:
(a) Apply compound, C00913 to the shank and threads of the bolts [93].
(b) Put the control rod [92] in its position between the carriage [91] and the crank arm [98].
NOTE: Make sure the adjustable end of the control rod [92] attaches to the crank arm
[98].
(c) Install the bolts [93], washers [94], bushings [95], washers [96] and nuts [97] to attach the
control rod [92].
NOTE: Install the bolt [93] that attaches the control rod [92] to the crank arm with the head
toward the center of the flap track [90]. Install the bolt [93] that attaches the control
rod [92] to the carriage [91] with the head away from the center of the flap track
[90].
SUBTASK 27-59-02-820-003
(4) Do this task: Flap Skew Detection System Adjustment, TASK 27-59-00-820-801.
SUBTASK 27-59-02-420-011
(5) If the flap skew sensor [83] is not installed, do this task: Inboard Flap Outboard Skew Sensor
Installation, TASK 27-59-01-400-803.
SUBTASK 27-59-02-210-003
(6) Before you connect the electrical connector [82], 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 27-59-02-420-012
(7) Connect the electrical connector [82] to the flap skew sensor [83].
SUBTASK 27-59-02-860-014
(8) 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
737-600/700/800/900
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EFFECTIVITY
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SUBTASK 27-59-02-440-003
(9) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
SUBTASK 27-59-02-860-015
(10) 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 27-59-02-730-003
(11) Do this task: Flap Skew Detection System Functional Test, TASK 27-59-00-730-801.
------------------------- END OF TASK ---------------------------
TASK 27-59-02-000-804
8. Inboard Flap Inboard Skew Mechanism Removal
(Figure 204)
A. General
(1) This task is applicable to the flap skew mechanisms installed on flap supports No. 4 and 5.
(2) You can remove the flap skew mechanism with the flap skew sensor [121] either removed or
installed. This task shows the removal with the flap skew sensor [121] installed.
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
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737-600-700-800-900 飞机维护手册5 AIRCRAFT MAINTENANCE MANUA(140)
