Figure 102 (Sheet 6)
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A
747-400 MAINTENANCE MANUAL
AC GENERATION - ADJUSTMENT/TEST
_______________________________
1. General_______
A. This procedure identifies the task for the operational test of the ac generation system. The operational test includes tests for the three ac generation systems:
(1)
External Power
(2)
APU Power
(3)
Engine Power
B.
The operational test of the three ac generation systems will examine these components:
(1)
Bus control units (BCU)
(2)
Generator control units (GCU)
(3)
Auxiliary generator control unit (AGCU)
(4)
Generator circuit breaker (GCB)
(5)
Bus tie breaker (BTB)
(6)
Auxiliary power breaker (APB)
(7)
Split system Breaker (SSB)
C.
You must operate the engines and the APU to do the operational test.
D.
To do the operational test of the 115-volt ac standby power generation system, refer to 24-29-00/501.
TASK 24-20-00-715-001
2. Operational Test - AC Generation (Fig. 501 and 502)________________________________
A. References
(1)
AMM 24-22-00/201, Manual Control
(2)
AMM 45-10-00/201, Central Maintenance Computer System
(3)
AMM 49-11-00/201, Auxiliary Power Unit
(4)
AMM 71-00-00/201, Power Plant
(5)
WDM 24-21-11 thru WDM 24-21-71, WDM 24-22-11 thru WDM 24-22-74, WDM 24-23-11 thru WDM 24-23-82, WDM 24-27-21 thru WDM 24-27-52
(6)
SSM 24-21-01 thru SSM 24-21-06, SSM 24-22-01 thru SSM 24-22-07, SSM 24-23-01 thru SSM 24-23-09, SSM 24-27-01 thru SSM 24-27-08
B.
Access
(1)
Location Zone 118 Electrical and Electronics Compartment, RH 221 Control Cabin, LH
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747-400 MAINTENANCE MANUAL
GENERATOR FIELD
MANUAL RESET MODULE
SEE B
ELECTRICAL SYSTEM CONTROL MODULE
SEE A
FLIGHT COMPARTMENT
ELECTRICAL SYSTEM CONTROL MODULE GENERATOR FIELD MANUAL RESET MODULE (EXAMPLE)
A B
Electrical System Control Location Figure 501
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747-400
MAINTENANCE MANUAL
ELECTRICAL SYSTEM SYNOPTIC DISPLAY ELECTRICAL SYSTEM MAINTENANCE DISPLAY
A
A
EICAS Electrical System Displays
Figure 502
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747-400 MAINTENANCE MANUAL
(2) Access Panel
118A Electrical Power Receptacle Door
C. Prepare for the Test
S 865-002
(1) Apply external power to the airplane (AMM 24-22-00/201).
NOTE: Two external power sources are necessary to do this test.
____ If only one power source is available, use a "Y" adapter to apply power to the two external power receptacles.
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