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TASK 27-81-00-860-803.
SUBTASK 27-81-00-860-024
(11) Do a check of the flap panel clearances.
(a) For all but the aft 5 inches (127 millimeters) of the flap, make sure the gap between the
inboard leading edge flap [1] and the outboard leading edge flap [2] is 0.060-0.150 inch
(1.52-3.81 millimeters).
(b) For the aft 5 inches (127 millimeters) of the flap, make sure the gap between the inboard
leading edge flap [1] and the outboard leading edge flap [2] is 0.060-0.250 inch (1.52-6.35
millimeters).
SUBTASK 27-81-00-210-002
(12) If the flap panel clearances are out of tolerance, do a check of the wing and flap panel for
damage or warpage.
NOTE: This check is to make sure that the flap and the wing align correctly. There is no
adjustment that you can do.
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G. Put the Airplane Back to Its Usual Condition
SUBTASK 27-81-00-080-004
WARNING: CAREFULLY REMOVE THE LEADING EDGE FLAP ACTUATOR LOCK TO PREVENT
ACCIDENTAL OPERATION OF THE LEADINGE EDGE FLAPS. THE LEADING EDGE
FLAPS CAN MOVE QUICKLY. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE
TO EQUIPMENT.
(1) Remove the lockout set, SPL-1734 from the leading flaps. To remove the lockout set, do this task:
Leading Edge Flap and Slat Locks Removal, TASK 27-81-00-080-801.
SUBTASK 27-81-00-860-025
WARNING: MAKE SURE PERSONS AND EQUIPMENT ARE CLEAR OF THE LEADING EDGE FLAPS
AND SLATS AND THE TRAILING EDGE FLAPS. THE LEADING EDGE FLAPS AND
SLATS AND THE TRAILING EDGE FLAPS CAN MOVE QUICKLY. THIS CAN CAUSE
INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(2) Do this task: Leading Edge Flaps and Slats Retraction, TASK 27-81-00-860-804.
------------------------- END OF TASK ---------------------------
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Leading Edge Flap Adjustment
Figure 501 (Sheet 1 of 5)/27-81-00-990-804
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Leading Edge Flap Adjustment
Figure 501 (Sheet 2 of 5)/27-81-00-990-804
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Leading Edge Flap Adjustment
Figure 501 (Sheet 3 of 5)/27-81-00-990-804
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Leading Edge Flap Adjustment
Figure 501 (Sheet 4 of 5)/27-81-00-990-804
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Leading Edge Flap Adjustment
Figure 501 (Sheet 5 of 5)/27-81-00-990-804
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TASK 27-81-00-820-802
3. Leading Edge Slat Actuator and Main Track Downstop Adjustment
(Figure 502)
A. General
(1) You must adjust the leading edge slats with the wing unsupported outboard of the engine
nacelle. You can adjust the leading edge slats with the airplane on the gear or on jacks inboard
of the engine nacelle. The airplane must not have fuel on the outboard wing.
B. References
Reference Title
27-81-00-080-801 Leading Edge Flap and Slat Locks Removal (P/B 201)
27-81-00-480-801 Leading Edge Flap and Slat Locks Installation (P/B 201)
27-81-00-860-804 Leading Edge Flaps and Slats Retraction (P/B 201)
29-11-00-860-801 Hydraulic System A or B Pressurization (P/B 201)
29-11-00-860-805 Hydraulic System A or B Power Removal (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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