TASK 24-11-00-440-801
3. IDG - Activation
(Figure 201)
A. General
(1) This procedure adds electrical power to the IDG.
B. Location Zones
Zone Area
117 Electrical and Electronics Compartment - Left
118 Electrical and Electronics Compartment - Right
211 Flight Compartment - Left
212 Flight Compartment - Right
C. Procedure
SUBTASK 24-11-00-860-009
(1) Remove the safety tags and close these circuit breakers:
F/O Electrical System Panel, P6-4
Row Col Number Name
F 10 C01283 GENERATOR CONT UNIT 1
F 11 C01284 GENERATOR CONT UNIT 2
END OF TASK
TASK 24-11-00-700-801
4. IDG Oil System Static Leak Check
(Figure 202)
A. General
(1) The static leak check applies compressed air or nitrogen to the Integrated Drive Generator
(IDG) oil system through the IDG pressure fill fitting. The pressure is monitored to see if it
starts to decrease. A continuous decrease in pressure indicates there is a leak in the system.
B. References
Reference Title
12-13-21-200-801 IDG Oil Level Check (P/B 301)
71-00-00 P/B 201 POWER PLANT - MAINTENANCE PRACTICES (OPERATION
PROCEDURES)
71-11-02-010-801-F00 Open the Fan Cowl Panels (P/B 201)
71-11-02-410-801-F00 Close the Fan Cowl Panels (P/B 201)
C. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
SPL-8912 Test Equipment- Engine Generator Pressure
737-600, -700, -800
Part #: J24015-1 Supplier: 81205
Part #: J24015-23 Supplier: 81205
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-11-00
Page 204
D633A101-ILF Oct 15/2018
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
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