24-11-01
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 434-045
 (26)
 Remove the covers and install the electrical connectors DG19A (8) and DG19B (2) to the IDG (1).

 S 614-046

 (27)
 Do this task:  "Fill the Integrated Drive Generator Oil" (AMM 12-13-07/301).

 S 864-065

 (28)
 If you opened these circuit breakers, remove the DO-NOT-CLOSE tags and close these circuit breakers.

 (a)  
On the P180 or P180-1 panel:
 1) C8 or M4, GCU 1
 2) B25, GCU 1 ALT

 (b)  
On the P514 panel:
 1) GCU 1 PHASE C SYNCH BUS

 S 864-066
 (29)
 If you opened these circuit breakers, remove the DO-NOT-CLOSE tags and close these circuit breakers.

 (a)  
On the P180 or P180-1 panel:
 1) C9 or M5, GCU 2
 2) B26, GCU 2 ALT

 (b)  
On the P614 panel:
 1) GCU 2 PHASE C SYNCH BUS

 S 864-067
 (30)
 If you opened these circuit breakers, remove the DO-NOT-CLOSE tags and close these circuit breakers.

 (a)  
On the P180 or P180-1 panel:
 1) C10 or M6, GCU 3
 2) B27, GCU 3 ALT

 (b)  
On the P515 panel:
 1) GCU 3 PHASE C SYNCH BUS

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-11-01
 ALL  ú ú 01P Page 422 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 864-068
 (31)
 If you opened these circuit breakers, remove the DO-NOT-CLOSE tags and close these circuit breakers.

 (a)  
On the P180 to P180-1 panel:
 1) C11 or M7, GCU 4
 2) B28, GCU 4 ALT

 (b)  
On the P615 panel:
 1) GCU 4 PHASE C SYNCH BUS

 S 794-048
 (32)
 Do this task:  "Test No. 3 - Ground Test - Idle Leak Check" (AMM 71-00-00/201).

 (a)  
Stop for three minutes while the oil level becomes stable.

 S 214-058
 (33)
 Do this task: "Examine the IDG Oil Level" (AMM 12-13-07/301).

 S 644-059

 (34)
 If it is necessary, do this task:  "Fill the Integrated Drive Generator Oil" (AMM 12-13-07/301).

 (35)
 Close the left thrust reverser half (AMM 78-31-00/201).

 S 714-050

 (36)
 Do this task:  "Operational Test - Generator Drive System" (AMM 24-11-00/501).

 S 414-049
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-11-01
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 INTEGRATED DRIVE GENERATOR - INSPECTION/CHECK
_____________________________________________
 1.  General
_______
 A.  This procedure contains these tasks to do a check of the IDG:
 (1)  Examine the pressure differential indicator (the red button) and the IDG scavenge filter.
 NOTE: The DPI extension procedure, single or alternate can be
____
 intermixed.

 (2)  
Examine the oil in the IDG.

 (3)  
Examine the IDG pressure oiler (service fitting) and pressure cap.

 B.  
If the IDG is replaced, the IDG scavenge filter element is installed in the IDG. The IDG and the IDG filter element is sent to the repair shop for analysis.

 C.  
Once the filter element is removed, do not install the same filter element in the IDG. A used filter element cannot be cleaned. Install a new filter element.

 D.  
When the intergrated drive generator shows signs of contamination, flush the oil coolers and the tubing with oil. If the scavenge filter o-ring is damaged or collapsed the oil coolers and tubing must be replaced.
　
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