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Boeing 737-600 - Subtask 76-11-07-820-004-F00; Subtask 76-11-07-420-004-F00; Subtask 76-11-07-420-008-F00; Subtask 76-11-07-860-029-F00

Boeing 737-600
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ILF ALL; AUTOTHROTTLE SWITCHPACK WITH REPLACEABLE SWITCHES P/N 254A1150-1, -2, -7, -8, -9, -10
(Continued)
Table 403/76-11-07-993-806-F00 (Continued)
Switchpack Switch Connector Pin (Lead ID)
Right S8 D11132P 16 (NO), 17 (C), 18 (NC)
Right S9 D11132P 22 (NO), 23 (C), 24 (NC)
(d) Loosely install the applicable switch [12] on the switchpack [9].
(e) Install two screws [11] and the two washers [10].
(f) Make sure the replaced wiring is held in the applicable wire bundle sheath.
SUBTASK 76-11-07-820-004-F00
(2) Adjust the switch [12] as follows:
(a) Make sure that the applicable switch roller is set on the largest radius of the cam.
(b) Push the switch [12] to the cam until switch actuation occurs.
(c) Move the switch [12] 0.005 in. (0.127 mm) 0.010 in. (0.254 mm) more on the cam and
hold the position.
(d) Tighten the screw [11].
SUBTASK 76-11-07-420-004-F00
(3) If you did not remove the autothrottle switchpack assembly, do this task: Switch Check and
Adjustment, TASK 76-11-07-820-801-F00.
SUBTASK 76-11-07-420-008-F00
(4) If you removed the autothrottle switchpack assembly, do this task: Autothrottle Switchpack
Assembly - Installation, TASK 76-11-07-400-802-F00.
H. Put the Airplane Back to its Usual Condition
SUBTASK 76-11-07-860-029-F00
(1) Open these circuit breakers and install safety tags:
CAPT Electrical System Panel, P18-3
Row Col Number Name
ILF 583
C 7 C01678 WEATHER RADAR RT RIGHT
F/O Electrical System Panel, P6-1
Row Col Number Name
ILF ALL; AUTOTHROTTLE SWITCHPACK WITH REPLACEABLE SWITCHES P/N 254A1150-1, -2, -7,
-8, -9, -10
D 13 C00120 WEATHER RADAR RT
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
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-07
Page 420
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL

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