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SUBTASK 27-81-00-420-004
(10) Tighen the locking bolts [79] for the auxiliary track aft support to 130-200 pound-inches (14.7-22.6
newton-meters).
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SUBTASK 27-81-00-420-005
(11) Tighten the jam nut [82] on the auxiliary track aft support.
(a) Finger tight until the jam nut [82] touches the support shaft and tighten an additional quarter
turn.
SUBTASK 27-81-00-420-010
(12) Tighen the upper aft aux track locking bolt [91] to 130-200 pound-inches (14.7-22.6 newtonmeters).
SUBTASK 27-81-00-420-006
(13) Tighten the nut [74] on the auxiliary track forward support to 260-425 pound-inches (29.4-48.0
newton-meters).
SUBTASK 27-81-00-420-007
(14) Tighten the nuts [84] on the cam plate to 65-100 pound-inches (7.3-11.3 newton-meters) or the
cam plate bolts [90] 90-110 pound-inches (10.2-12.4 newton-meters).
NOTE: The recommended method is to tighten the nuts; the optional method is to tighten the
bolts.
SUBTASK 27-81-00-420-008
(15) Install lockwire, G01048 between the holes in the shim [77] of the auxiliary track forward support.
SUBTASK 27-81-00-420-009
(16) Install lockwire, G01048 on the preload adjustment bolt [73] on the detent arm [78].
I. Put the Airplane Back to Its Usual Condition
SUBTASK 27-81-00-860-036
WARNING: MAKE SURE PERSONS AND EQUIPMENT ARE CLEAR OF THE LEADING EDGE FLAPS
AND SLATS AND THE TRAILING EDGE FLAPS. THE FLAPS AND SLATS CAN MOVE
QUICKLY. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(1) Do this task: Leading Edge Flaps and Slats Retraction, TASK 27-81-00-860-804.
SUBTASK 27-81-00-410-001
(2) Install the applicable access panels:
NOTE: At the main track locations, the clearance between the access panel and the flex tab
must be 0.1000 -0.0400/+0.0800 inch (2.54 -1.02/+2.03 millimeters).
(a) For the left wing, install these access panels:
Number Name/Location
521CB Lower Leading Edge Access Panel - Slat Station
53.95
521DB Lower Leading Edge Access Panel - Slat Station
71.38
521EB Lower Leading Edge Access Panel - Slat Station
98.95
521FB Lower Leading Edge Access Panel - Slat Station
116.32
521JB Lower Leading Edge Access Panel - Slat Station
170.20
521KB Lower Leading Edge Access Panel - Slat Station
188.12
521LB Lower Leading Edge Access Panel - Slat Station
216.76
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(Continued)
Number Name/Location
521MB Lower Leading Edge Access Panel - Slat Station
234.65
521QB Lower Leading Edge Access Panel - Slat Station
289.17
521RB Lower Leading Edge Access Panel - Slat Station
307.75
521SB Lower Leading Edge Access Panel - Slat Station
337.62
521TB Lower Leading Edge Access Panel - Slat Station
356.14
521WB Lower Leading Edge Access Panel - Slat Station
415.79
521XB Lower Leading Edge Access Panel - Slat Station
435.91
521YB Lower Leading Edge Access Panel - Slat Station
467.98
521ZB Lower Leading Edge Access Panel - Slat Station
488.05
(b) For the left wing, install these access panels:
Number Name/Location
621CB Lower Leading Edge Access Panel - Slat Station
53.95
621DB Lower Leading Edge Access Panel - Slat Station
71.38
621FB Lower Leading Edge Access Panel - Slat Station
112.52
621HB Lower Leading Edge Access Panel - Slat Station
170.21
621JB Lower Leading Edge Access Panel - Slat Station
188.14
621KB Lower Leading Edge Access Panel - Slat Station
216.71
621LB Lower Leading Edge Access Panel - Slat Station
234.59
621QB Lower Leading Edge Access Panel - Slat Station
307.75
621RB Lower Leading Edge Access Panel - Slat Station
337.62
621SB Lower Leading Edge Access Panel - Slat Station
356.15
621TB Lower Leading Edge Access Panel - Slat Station
374.95
621VB Lower Leading Edge Access Panel - Slat Station
415.79
621WB Lower Leading Edge Access Panel - Slat Station
435.91
621XB Lower Leading Edge Access Panel - Slat Station
467.98
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-81-00
Page 532
Feb 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
　
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