757
MAINTENANCE MANUAL

ELECTRICAL SYSTEM CONTROL PANEL SEE A
FLT COMPT
SEE B
APU GEN EXT PWR ELECTRICAL
ON
O w
CONNECTORBUS TIE
ON
F
BUS TIE TERMINAL BLOCKAVAIL
F a ww
OIL OUTAUTO AUTO
w
w
ISLN ISLN

aa
UTILITY BUS

SPLINE
L BUS L R R BUS
BUSBUS ON ON OFF aOFF a
w w
OFF OFF
a a
R
GEN

L
GEN DRIVE DISC GEN
CONT

L R CONT
O O
ELECTRICAL
ww
FWDON ON
F F
CONNECTORDISCONNECTDRIVE DRIVE F
F a wa aa w
RESET RING
LEFT SIDE VIEW
GENERATOR DRIVE DISC SWITCH
B
M10063-ELECTRICAL SYSTEM CONTROL PANEL

A
IDG Disconnect Drive System
Figure 601

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-11-01
 ALL  ú ú 03 Page 602 ú Sep 15/85
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

IDG Service Fitting and Pressure Cap Inspection
Figure 602

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-11-01
 ALL  ú ú 01 Page 603 ú May 20/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
H40682
A

757
MAINTENANCE MANUAL

INTEGRATED DRIVE GENERATOR
SEE A
FILTER ELEMENT
FILTER COVER FWD
SEE B SEE C
O-RING
RED (BOTTOM VIEW) BUTTON
A
NORMAL (RESET)  EXTENDED
PRESSURE DIFFERENTIAL INDICATOR
B
DPI RESETS
REFER TO APPROPRIATE DOCUMENTATION
FOR DETAILS OF THE ALTERNATE DPI
PROCEDURE

REMOVE
2 34
1  IDG
DPI RESETS DECAL
C
DPI Reset Procedure
Figure 603

H41515
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-11-01
 ALL  ú ú 01 Page 604 ú May 20/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 E. Procedure
 S 866-006
 (1)  AIRPLANES WITH IDG DISCONNECT INHIBIT (POST-SB 24-59);
 Do the IDG Disconnect Inhibit Function Check as follows:

 NOTE: These airplanes use pins 1 and 13 on K10446 or K10556
____
 in the P36 panel (WDM 24-11-11).

 CAUTION: DO NOT ACTUATE THE DISCONNECT SWITCH FOR LONGER THAN 3
_______ SECONDS. ALLOW A MINIMUM OF 60 SECONDS BETWEEN ACTUATION PERIODS. FAILURE TO FOLLOW THIS PROCEDURE COULD DAMAGE THE IDG DISCONNECT FUNCTION.
 (a)  
Momentarily push the GEN DRIVE DISC switch on the P5 panel for the applicable IDG.

 (b)  
Slowly pull the disconnect reset ring to the outward travel limit. 1) Make sure there is no "click" sound when you pull the

 disconnect reset ring.

 (c)  
Permit the ring to slowly go back to the maximum inner position.

 S 716-088
 (2)  Do the IDG Disconnect Function check as follows:
 (a)  Open the applicable ENGINE SPEED CARD circuit breaker, 11B31 or 11B32, for the applicable IDG.
 CAUTION: DO NOT ACTUATE THE DISCONNECT SWITCH FOR LONGER THAN 3
_______ SECONDS. ALLOW A MINIMUM OF 60 SECONDS BETWEEN ACTUATION PERIODS. FAILURE TO FOLLOW THIS PROCEDURE COULD DAMAGE THE IDG DISCONNECT FUNCTION.
 (b)  Momentarily push the GEN DRIVE DISC switch on the P5 panel for the applicable IDG.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-11-01
 ALL  ú ú 02 Page 605 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 (c)  
Close the applicable ENGINE SPEED CARD circuit breaker, 11B31 or 11B32, for the applicable IDG.
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機維護手冊 電源 ELECTRICAL POWER 1(26)