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时间:2011-04-09 10:23来源:蓝天飞行翻译 作者:航空
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 24-22-01
 ALL  ú ú 04 Page 407 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 864-045
 (25)
 Set the GEN CONT 1, 2, 3, and 4 switches to ON.

 S 214-046

 (26)
 Make sure the FIELD OFF lights on GEN FIELD MAN RESET switches 1, 2, 3, and 4 on the P461 panel are off.

 S 864-047

 (27)
 Open these circuit breakers:

 (a)  
P180 DC Power Distribution Panel
 1) 180B29 BCU-1 ALT
 2) 180B30 BCU-2 ALT

 

 S 864-048
 (28)
 Set the BATTERY switch to OFF.

 S 214-049

 (29)
 Make sure the message BATTERY OFF shows on the upper EICAS screen.

 S 864-050

 (30)
 Set the BATTERY switch to ON.

 S 214-051

 (31)
 Make sure the message BATTERY OFF does not show on the upper EICAS screen.

 S 864-052

 (32)
 Close these circuit breakers:

 (a)  
P180 DC Power Distribution Panel
 1) 180B29 BCU-1 ALT
 2) 180B30 BCU-2 ALT

 

 S 864-053
 (33)
 Set the STANDBY POWER switch to OFF.

 (34)
 Make sure the upper EICAS screen is not on.

 (35)
 Set the STANDBY POWER switch to AUTO.

 S 864-056

 (36)
 Get access to the maintenance page for the electrical system (AMM 45-10-00/201).

 S 214-057

 (37)
 On the maintenance page for the electrical system, make sure the currents for the main and APU battery are 2 amps or less.


 S 214-054
 S 864-055
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-22-01
 ALL  ú ú 04 Page 408 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 864-058
 (38)
 Set the STANDBY POWER switch to BAT.

 S 214-059

 (39)
 On the maintenance page for the electrical system, make sure the currents for the main and APU battery are more than 2 amps.

 S 864-060

 (40)
 Set the STANDBY POWER switch to AUTO.

 S 864-061

 (41)
 Start the APU and let it operate for 90 seconds (Ref 49-11-00/201).

 S 214-062

 (42)
 Make sure the FIELD OFF lights on the APU 1 and 2 switches on the P461 panel are off.


 NOTE: If the FIELD OFF lights are on, move the APU 1 and 2 field
____
 reset switches

 S 214-064
 (43)
 Make sure that the AVAIL lights on the APU GEN 1 and 2 switches are on.

 S 864-065

 (44)
 Set the APU GEN 1 and 2 switches to on.

 S 214-066

 (45)
 Make sure that the ON lights on the APU GEN 1 and 2 switches are on.

 (46)
 Set the EXT PWR 1 and EXT PWR 2 switches to on.

 (47)
 Make sure that the ON lights on the EXT PWR 1 and 2 switches are on.

 (48)
 Stop the APU (AMM 49-11-00/201).


 S 864-067
 S 214-068
 S 864-069
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-22-01
 ALL  ú ú 04 Page 409 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 864-075 CAUTION: THE ENGINES MUST NOT BE WINDMILING WHEN THE DISCONNECT SWITCHES
_______ ARE PRESSED. DAMAGE TO THE IDG COULD OCCUR.
 (49) Push the DRIVE DISC 1, 2, 3, and 4 switches. NOTE: The engines do not need to run.____
 S 214-071
 (50) Make sure the messages DRIVE DISC 1, 2, 3, and 4 show on the upper EICAS screen.
 S 864-076 CAUTION: THE ENGINES MUST NOT BE WINDMILLING WHEN THE IDG IS CONNECTED.
_______ DAMAGE TO THE IDG COULD OCCUR.
 (51)
 Engage the IDG on engines 1, 2, 3, and 4 (AMM 24-11-00/501). S 864-073

 (52)
 Remove electrical power if it is not necessary (AMM 24-22-00/201).
 
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