TASK 24-21-81-400-801
3. Generator Control Unit Installation
(Figure 401)
A. General
(1) There are three GCU's installed as follows:
(a) GCU 1, G10 - located on the E2-1 Rack
(b) GCU 2, G12 - located on the E4-2 Rack
(c) APU GCU, G14 - located on the E2-1 Rack
B. References
Reference Title
20-10-07-400-801 E/E Box Installation (P/B 201)
20-40-12-400-802 ESDS Handling for Metal Encased Unit Installation (P/B 201)
24-22-00-860-813 Supply External Power (P/B 201)
24-22-00-860-814 Remove External Power (P/B 201)
C. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
1 GCU 24-21-81-01-005 ILF 401, 405, 406, 409,
410, 412, 416
24-21-81-02-005 ILF 301, 304, 308, 310,
314, 315, 317-319, 323,
401, 402, 405, 406, 409,
410, 412, 416, 424, 425,
427-429, 451, 452,
501-504, 507-510,
512-516, 518-520,
523-528, 530-533, 536,
541, 542, 552, 571, 572,
703, 707, 708
24-21-81-02-005P ILF 301, 304, 308, 310,
314, 315, 317-319, 323,
401, 402, 405, 406, 409,
410, 412, 416, 424, 425,
427-429, 451, 452,
501-504, 507-510,
512-516, 518-520,
523-528, 530-533, 536,
541, 542, 552, 571, 572,
703, 707, 708
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-21-81
Page 407
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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