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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
621YB Lower Leading Edge Access Panel - Slat Station 488.04
G. Prepare for the Adjustment
SUBTASK 27-81-00-010-001
(1) Remove the applicable access panels:
(a) For the left wing, remove 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
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-81-00
Page 519
Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(Continued)
Number Name/Location
521LB Lower Leading Edge Access Panel - Slat Station
216.76
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, remove 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
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-81-00
Page 520
Jun 10/2004
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(Continued)
Number Name/Location
621XB Lower Leading Edge Access Panel - Slat Station
467.98
621YB Lower Leading Edge Access Panel - Slat Station
488.04
SUBTASK 27-81-00-860-033
(2) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-81-00-820-002
(3) Do a preliminary adjustment of the auxiliary track forward support (Figure 503) (View A-A):
(a) Install the preload shim assembly, which is part of the kit, SPL-1739, at the forward
supports for the auxiliary tracks.
1) Remove the nuts [74] and washers [75] from the clevis [76].
2) Lift the auxiliary track [72] with the clevis [76] through the auxiliary track support.
3) Install the preload shim assembly, which is part of the kit, SPL-1739, and the shims [77]
on the clevis [76].
4) Put the clevis [76] back in its position on the auxiliary track support.
5) Install the washers [75] and nuts [74] on the clevis [76].
SUBTASK 27-81-00-820-003
(4) Do a preliminary adjustment of the auxiliary track aft support (Figure 503) (View B-B):
NOTE: If you do a minimum slat adjustment, preliminary adjustment of the auxiliary track aft
suppport is not necessary.
(a) Loosen the upper aft aux track locking bolt [91].
1) Loosen the nut [90].
　
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