ILF 625-627, 835, 838
TASK 76-11-02-010-802-F00
4. Start Lever Removal
(Figure 407 or Figure 408)
A. General
(1) The start levers are installed on the control stand.
B. References
Reference Title
25-11-01-000-801 Captain's and First Officer's Seat Removal (P/B 401)
C. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
D. Prepare for the Removal
SUBTASK 76-11-02-860-020-F00
(1) For engine 1, open these circuit breakers and install safety tags:
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
F/O Electrical System Panel, P6-3
Row Col Number Name
B 4 C00359 FUEL SPAR VALVE ENG 1
B 5 C00540 FUEL SPAR VALVE IND
E 5 C01320 ENGINE FUEL ENGINE 1 HPSOV CONT
E 6 C01395 ENGINE FUEL ENGINE 1 HPSOV IND
SUBTASK 76-11-02-860-021-F00
(2) For engine 2, open these circuit breakers and install safety tags:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 5 C01313 ENGINE 2 RUN/PWR
B 6 C01318 ENGINE 2 START LEVER CHAN A
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-02
Page 437
D633A101-ILF Feb 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
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