Boeing 737-600 - Subtask 80-11-00-420-001-F00; Subtask 80-11-00-860-010-F00; Subtask 80-11-00-860-011-F00; Subtask 80-11-00-860-009-F00

(Continued)
AMM Item Description AIPC Reference AIPC Effectivity
2 (cont.) 31-11-94-69-590 ILF 301, 304, 308, 310,
314
31-11-94-76-590 ILF 424, 425, 427-429
31-11-94-90-010 ILF 501-503, 514, 516,
524
D. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
E. Start Switch Installation
SUBTASK 80-11-00-420-001-F00
(1) Install the start switch [1] as follows:
(a) Put the start switch [1] in its position in the P5 overhead panel.
(b) Install the washer [4] and the nut [3].
1) Tighten the nut [3].
(c) If it is necessary, install the spacer [2] .
(d) Install the knob.
1) Tighten the screws on the knob.
(e) Connect the applicable wire back to the switch [1].
1) Install each wire lug to its terminal.
(f) If the start switch does not have a diode installed at the X1 and X2 terminals, do these
steps:
1) Use a new diode or the diode from the removed switch.
2) Install the cathode end of the diode to the X2 terminal.
3) Install the anode of the diode to the X1 terminal.
(g) Close and latch the P5 overhead panel.
F. Put the Airplane Back to Its Usual Condition
SUBTASK 80-11-00-860-010-F00
(1) For Engine 1, remove the safety tag and close this circuit breaker:
CAPT Electrical System Panel, P18-2
Row Col Number Name
B 8 C01103 ENGINE 1 START VALVE
SUBTASK 80-11-00-860-011-F00
(2) For Engine 2, remove the safety tag and close this circuit breaker:
F/O Electrical System Panel, P6-2
Row Col Number Name
C 4 C00154 ENGINE 2 START VALVE
SUBTASK 80-11-00-860-009-F00
(3) Remove the DO-NOT-OPERATE tag from the applicable start lever.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
80-11-00
Page 407
D633A101-ILF Feb 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL