(Continued)
F/O Electrical System Panel, P6-3
Row Col Number Name
E 6 C01395 ENGINE FUEL ENGINE 1 HPSOV IND
2) Make sure that these circuit breakers are closed:
CAPT Electrical System Panel, P18-2
Row Col Number Name
B 2 C01317 ENGINE 1 START LEVER CHAN B
F/O Electrical System Panel, P6-2
Row Col Number Name
B 7 C01319 ENGINE 2 START LEVER CHAN B
3) Push the applicable ENGINE START LEVER to the IDLE position.
CAUTION
DO NOT ACTUATE THE DISCONNECT SWITCH FOR MORE THAN 3
SECONDS. ALLOW A MINIMUM OF 60 SECONDS BETWEEN
ACTUATION PERIODS. FAILURE TO FOLLOW THIS PROCEDURE CAN
CAUSE DAMAGE TO IDG.
(b) Push the DISCONNECT switch on the P5 panel to the DISCONNECT position.
NOTE: Put a person near the IDG listening for a click and feeling for a movement while
lightly holding the IDG Disconnect Reset Ring. There should be a click and
movement should be felt when the applicable DISCONNECT switch is pushed.
(c) Make sure that the DRIVE light on the P5 panel stays on.
(d) Push the BAT switch on the P5 panel to the OFF position.
(e) Put the ENGINE START LEVER in the CUTOFF position
(f) 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
B 1 C01316 ENGINE 1 START LEVER CHAN A
F/O Electrical System Panel, P6-2
Row Col Number Name
B 6 C01318 ENGINE 2 START LEVER CHAN A
D 4 C00459 ENGINE 2 IGNITION RIGHT
D 6 C00151 ENGINE 2 IGNITION LEFT
F/O Electrical System Panel, P6-3
Row Col Number Name
B 3 C00360 FUEL SPAR VALVE ENG 2
B 4 C00359 FUEL SPAR VALVE ENG 1
B 5 C00540 FUEL SPAR VALVE IND
E 3 C01321 ENGINE FUEL ENGINE 2 HPSOV CONT
E 4 C01396 ENGINE FUEL ENGINE 2 HPSOV IND
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-11-11
Page 603
D633A101-ILF Feb 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
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