GENERATOR DRIVE SYSTEM - ADJUSTMENT/TEST
1. General
A. This procedure has these tasks:
(1) The Operational Test For The Number 1 IDG.
(2) The Operational Test For The Number 2 IDG.
TASK 24-11-00-700-802
2. Number 1 IDG - Operational Test
(Figure 501, Figure 502)
A. General
(1) This procedure does these tests:
(a) The Operation Test
(b) The Load Test
(c) The IDG Disconnect and Connect Test.
(2) You must operate the engines to do an operational test of the IDG.
B. References
Reference Title
24-11-11-000-801 Integrated Drive Generator (IDG) Removal (P/B 401)
24-11-11-400-801 Integrated Drive Generator (IDG) Installation (P/B 401)
24-22-00-860-812 Remove Electrical Power (P/B 201)
24-22-00-860-813 Supply External Power (P/B 201)
71-00-00-700-819-F00 Stop the Engine Procedure (Usual Engine Stop) (P/B 201)
71-00-00-800-805-F00 Engine Ground Safety Precautions (P/B 201)
71-00-00-800-807-F00 Start the Engine Procedure (Selection) (P/B 201)
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. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
410 Subzone - Engine 1
D. Prepare for the Test
SUBTASK 24-11-00-860-001
(1) Do this task: Supply External Power, TASK 24-22-00-860-813.
E. The Operation Test
SUBTASK 24-11-00-710-002
(1) Do the operation test as follows:
(a) Set the AC meter selector switch on the P5–13 overhead panel to the GEN 1 position.
(b) Make sure that the AC meter on the P5 overhead panel shows these values:
1) AC VOLTS = 0
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-11-00
Page 501
D633A101-ILF Feb 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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