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Boeing 737-600 - Subtask 76-11-02-410-010-F00; Subtask 76-11-02-480-002-F00; Subtask 76-11-02-410-011-F00; Subtask 76-11-02-860-022-F00

Boeing 737-600
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ILF 625-627, 835, 838; 737-678 AIRCRAFT WITH P/N 254A1221-13/14
(e) Install the two clamps [210] on wire bundle [202] and two clamps [210] on wire
bundle [209] with one bolt [211] and two washers [212] for each clamp.
NOTE: Before you tighten the bolts [211], make sure that you can rotate the face
plate [218] along the lower edge at least 90 degrees aft for serviceability. Fasten
other moved spacers if loosened during removal of the wiring bundles.
ILF 625-627, 835, 838
(f) Connect the electrical connector [205], electrical connector [206], electrical
connector [207] and electrical connector [208] to the electrical connector panels.
(g) Install the face plate [218] on the control stand.
1) Install the five screws [216] to install the face plate [218] on the control stand.
(h) Install the lightplate [213] on the face plate [218].
(i) Install the lens cap [229] on the two engine start levers [201].
D. Put the Airplane Back to Its Usual Condition
SUBTASK 76-11-02-410-010-F00
(1) Install the side cover [203] and the side cover [222] on the control stand.
(a) Position the covers on the control stand.
(b) Tighten the eight quick-release fasteners [204] that hold side cover [203] to the control
stand.
(c) Tighten the 11 quick-release fasteners [204] that hole side cover [222] to the control
stand.
SUBTASK 76-11-02-480-002-F00
(2) Remove the protective mats from the aft electronics panel P8.
SUBTASK 76-11-02-410-011-F00
(3) Do this task: Captain's and First Officer's Seat Installation, TASK 25-11-01-400-801.
SUBTASK 76-11-02-860-022-F00
(4) For engine 1, remove the safety tags and close these circuit breakers:
CAPT Electrical System Panel, P18-2
Row Col Number Name
A 1 C00458 ENGINE 1 IGNITION RIGHT
A 3 C00153 ENGINE 1 IGNITION LEFT
A 4 C01390 ENGINE 1 ALTN PWR CHAN B
A 5 C01314 ENGINE 1 ALTN PWR CHAN A
B 1 C01316 ENGINE 1 START LEVER CHAN A
B 2 C01317 ENGINE 1 START LEVER CHAN B
B 3 C01312 ENGINE 1 RUN/PWR
B 4 C01003 ENGINE 1 THRUST REVERSER IND
B 5 C00276 ENGINE 1 THRUST REVERSER CONT
B 6 C01412 ENGINE 1 THRUST REVERSER INTLK
B 7 C01266 ENGINE 1 THRUST REVERSER SYNC LOCK
B 8 C01103 ENGINE 1 START VALVE
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-02
Page 445
D633A101-ILF Feb 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL

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