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below the lower surface of the main flap [1] when the seals are compressed.
SUBTASK 27-51-12-080-001
(15) Remove the rig pin from the crankshaft [3] if it is necessary.
SUBTASK 27-51-12-420-003
(16) At the outboard flap support, connect the crankshaft [3] to the aft flap drive rod [10] (Figure 401):
(a) Use the crankshaft [3] to manually extend the aft flap assembly [2] until the crankshaft [3]
aligns with the aft flap drive rod [10].
(b) Install the bolt [4], washer [5], bushing [6], washer [7] and nut [8] that attach the crankshaft
[3] to the aft flap drive rod [10].
NOTE: Make sure the head of the bolt [4] is on the inboard side.
(c) Tighten the nut [8] to 30-50 pound-inches (3.4 to 5.6 newton-meters).
(d) Install the pin [9] through the nut [8].
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-12-440-001
(1) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
SUBTASK 27-51-12-860-002
(2) Retract the trailing edge flaps to the retracted position. To retract the flaps, do this task: Retract
the Trailing Edge Flaps, TASK 27-51-00-860-804.
------------------------- END OF TASK ---------------------------
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INBOARD AFT FLAP - INSPECTION/CHECK
1. General
A. This procedure contains a task to do an inspection of the attachment points for the inboard aft flap.
The attachment points are the aft flap drive rods and the aft flap tracks.
TASK 27-51-12-200-801
2. Inboard Aft Flap Inspection
(Figure 601)
A. References
Reference Title
27-51-12-000-801 Inboard Aft Flap Removal (P/B 401)
27-51-12-400-801 Inboard Aft Flap Installation (P/B 401)
B. Tools/Equipment
Reference Description
STD-1096 Micrometer - Depth, 0-1 Inch, Readable to 1/1000 Inch
STD-1097 Caliper - Vernier, 0-6 Inch, Readable to 1/1000 Inch
C. Location Zones
Zone Area
553 Left Wing - Inboard Flap
653 Right Wing - Inboard Flap
D. Procedure
SUBTASK 27-51-12-020-005
(1) Do this task: Inboard Aft Flap Removal, TASK 27-51-12-000-801.
SUBTASK 27-51-12-020-006
(2) Use these tools to do a check for wear on the part of the inboard aft flap:
(a) micrometer (0-1 Inch, readable to 1/1000 Inch), STD-1096
(b) readable to 1/1000 inch vernier 0 - 6 inch caliper, STD-1097.
SUBTASK 27-51-12-020-007
(3) Examine the parts of the inboard aft flap (Table 601):
(a) Remove the parts that you will measure.
(b) Measure the parts with a micrometer (0-1 Inch, readable to 1/1000 Inch), STD-1096 or a
readable to 1/1000 inch vernier 0 - 6 inch caliper, STD-1097.
(c) Compare the dimensions you measured with the permitted wear dimensions.
(d) If the parts are not in tolerance, replace or repair the parts.
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册4(102)
