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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
(j) Move the flap control lever to the 40-unit position.
NOTE: This will reduce the load on the electric motor.
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(k) Move the ALTN FLAP control switch to the DOWN position and hold it until the flaps stop
moving.
(l) Make sure the left pointer is in the 40-unit white band and the right pointer is in the 30-unit
white band.
(m) Remove the safety tag and close this circuit breaker:
F/O Electrical System Panel, P6-2
Row Col Number Name
A 11 C01443 FC TE FLAP POS/SKEW SNSR & IND RIGHT
(n) Make sure the right pointer moves to the 40-unit white band.
(o) Make sure the tips of the pointers align in the limit of 0.06 inch (1.5 millimeters).
(p) Move the ALTN FLAPS ARM switch to the OFF position.
SUBTASK 27-58-02-860-007
(8) Move the flap control lever to the UP position to retract the flaps.
SUBTASK 27-58-02-710-003
(9) Do the test of the flap position indicator [1] in the UP position:
(a) Make sure the pointers on the flap position indicator [1] are in the UP white band.
(b) Make sure the tips of the pointers on the flap position indicator [1] align in the limit of 0.06
inch (1.5 millimeters).
F. Put the Airplane Back to Its Usual Condition
SUBTASK 27-58-02-860-008
(1) Remove system B hydraulic power, do this task: Hydraulic System A or B Power Removal,
TASK 29-11-00-860-805.
------------------------- END OF TASK ---------------------------
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FLAP SKEW DETECTION SYSTEM - ADJUSTMENT/TEST
1. General
A. This procedure has these tasks:
Table 501/27-59-00-993-805
Display (Sensor)
Skew Sensor Input (Flap Position)
UP 10-Unit 40-Units
F1 SKEW 295.7 to 311.0 95.9 to 113.6 224.4 to 242.1
F2 SKEW 330.5 to 346.0 149.1 to 166.7 279.2 to 296.9
F3 SKEW 0.0 to 13.2 164.7 to 181.5 288.7 to 305.5
F4 SKEW 332.8 to 346.9 121.0 to 138.5 265.1 to 282.1
F5 SKEW 13.1 to 27.2 221.5 to 239.0 77.9 to 94.9
F6 SKEW 346.8 to 360.0 178.5 to 195.3 54.5 to 71.3
F7 SKEW 14.0 to 29.5 193.3 to 210.9 63.1 to 80.8
F8 SKEW 49.0 to 64.3 246.4 to 264.1 117.9 to 135.6
(1) An adjustment of the mechanisms for the flap skew detection system.
(2) A functional test of the flap skew detection system.
TASK 27-59-00-820-801
2. Flap Skew Detection System Adjustment
A. General
(1) This task includes the adjustment of the flap skew mechanisms on all of the flap supports.
(2) It is not necessary for the flap skew sensors to be installed on the flap skew mechanism when
you do the adjustment.
B. References
Reference Title
27-51-00-040-801 Trailing Edge Flap System Deactivation (P/B 201)
27-51-00-440-801 Trailing Edge Flap System Reactivation (P/B 201)
27-51-00-820-802 Trailing Edge Flap Drive System Adjustment (P/B 501)
27-51-00-860-804 Retract the Trailing Edge Flaps (P/B 201)
27-51-00-980-801 Trailing Edge Flap System Manual Operation (P/B 201)
27-58-01-000-801 Flap Position Transmitter Removal (P/B 401)
32-00-01-480-801 Landing Gear Downlock Pins Installation (P/B 201)
C. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
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Reference Description
SPL-1679 Adapter - Drive, Flap Torque Tube Spline
(Part #: F70300-1, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
SPL-1726 Clamp Set - Trailing Edge Flap Torque Tube
(Part #: C27022-1, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
D. Consumable Materials
Reference Description Specification
C00913 Compound - Nondrying Resin Mix Corrosion
Inhibiting Material
BMS3-27
E. Location Zones
Zone Area
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737-600-700-800-900 飞机维护手册5 AIRCRAFT MAINTENANCE MANUA(125)
