SUBTASK 76-11-07-860-015-F00
(4) Open these circuit breakers and install safety tags:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 9 C00440 FLIGHT CONTROL AUTO SPEED BRAKE
F/O Electrical System Panel, P6-3
Row Col Number Name
A 16 C01345 LANDING GEAR AUTOBRAKE BITE CONT 2
A 18 C00583 LANDING GEAR AUTOBRAKE BITE CONT 1
C 18 C01398 LANDING GEAR TAKEOFF WARNING CUTOFF
D 18 C00451 LANDING GEAR AURAL WARN
SUBTASK 76-11-07-860-016-F00
(5) Attach the DO NOT OPERATE tag, STD-858, to the thrust levers.
SUBTASK 76-11-07-010-006-F00
(6) Open this access panel:
Number Name/Location
112A Forward Access Door
SUBTASK 76-11-07-010-007-F00
(7) Remove the applicable access panels:
(TASK 53-14-01-020-801)
Number Name/Location
113AC Fwd Nose Wheel Well Upper Access Panel
114AC Fwd Nose Wheel Well Upper Access Panel
G. Autothrottle Switchpack Assembly Removal
ILF ALL; AUTOTHROTTLE SWITCHPACK WITH REPLACEABLE SWITCHES P/N 254A1150-1, -2, -7,
-8, -9, -10
SUBTASK 76-11-07-020-003-F00
(1) Remove the a switchpack [9] as follows:
(a) For the left switchpack [9], disconnect the electrical connectors, D11128P and D11130P.
(b) For the right switchpack [9], disconnect the electrical connectors, D11132P and D11134P.
(c) Remove the bolt [4], washer [7], and nut [8].
(d) Move the rod [5] from the crank [6].
(e) Remove the two bolts [2], washers [14], and nuts [13].
(f) Slide the switchpack [9] off the bushing [1] and remove the switchpack [9].
NOTE: It is not necessary to remove the bushing in order to remove the switchpack.
ILF ALL; AUTOTHROTTLE SWITCHPACK WITH INTEGRATED SWITCHES P/N 254A1150-11, -12,
-13, -14, -15, -16
SUBTASK 76-11-07-020-006-F00
(2) Remove the applicable switchpack [9] as follows:
(a) For the left switchpack [9], disconnect the electrical connectors, D11128P and D11130P.
(b) For the right switchpack [9], disconnect the electrical connectors, D11132P and D11134P.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-07
Page 403
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
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