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时间:2011-04-03 11:28来源:蓝天飞行翻译 作者:航空
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FAULT ISOLATION:_______________ 
1 MOVE THE BLEED AIR SWITCH TO THE "OFF" POSITION. DOES THE EGT STAY 430`C OR ABOVE?  YES  (FIG. 132). TO 100 AMP ELECTRICAL LOAD GREATER THAN 430`C WITH A 50 51 DO THIS PROCEDURE: EGT IS 


THE BLEED AIR CONTROL SYSTEM TO FIND LEAKAGE (AMM 36-11-05/ 101).
EGT Is Greater Than 430`C With a 50 to 100 Amp Electrical Load and the APU Bleed Switch Is in the ON Position (Air Conditioning Packs are Closed) Figure 133
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 49-00-00
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES /MAINTENANCE MANUAL ////////////////////////
PREREQUISITES 
EGT IS GREATER THAN  NONE 
649`C DURING THE APU 
OPERATION 


POSSIBLE CAUSES:
1.
 DIFFERENTIAL PRESSURE REGULATOR PROBLEM (AMM 49-52-21/401)

2.
 BLEED AIR VALVE, V56, PROBLEM (AMM 49-52-11/401)

3.
 APU CONTROL THERMOSTAT PROBLEM (AMM 49-52-32/401).


FAULT ISOLATION:


51 ADJUST THE DIFFERENTIAL
PRESSURE REGULATOR
(AMM 49-52-21/501).
IF THE DIFFERENTIAL PRES-SURE REGULATOR CANNOT BE ADJUSTED, REPLACE THE REGULA-TOR (AMM 49-52-21/401).


YES
EGT Is Greater Than 649`C during the APU Operation
Figure 134

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 ú ú 01 Page 182R ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
PREREQUISITES 
EGT IS GREATER THAN  NONE 
649`C DURING THE APU 
OPERATION 


POSSIBLE CAUSES:
1.
 DIFFERENTIAL PRESSURE REGULATOR PROBLEM (AMM 49-52-21/401)

2.
 BLEED AIR VALVE, V56, PROBLEM (AMM 49-52-11/401)

3.
 PROPORTIONAL CONTROL VALVE PROBLEM (AMM 49-52-31/401).


FAULT ISOLATION:

EGT Is Greater Than 649`C during the APU Operation
Figure 134A

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 49-00-00
 ú ú 01 Page 182S ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E05801
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES /MAINTENANCE MANUAL ////////////////////////
PREREQUISITES 
EGT IS GREATER THAN  MAKE SURE THIS SYSTEM WILL OPERATE: 
760`C  APU (AMM 49-11-00/201) 


POSSIBLE CAUSES:
1.
 APU INTERNAL DAMAGE (AMM 49-11-00/401)

2.
 EGT INDICATOR, N24, PROBLEM (WDM 49-71-01).


FAULT ISOLATION:
YES

1 START AND OPERATE THE APU
51 DO THE APU USUAL SHUTDOWN (AMM 49-11-00/201). (AMM 49-11-00/201).
DID THE EGT INDICATOR DO THE INSPECTION OF THE SHOW A TEMPERATURE OF 760`CAPU (AMM 49-11-00/601).OR GREATER DURING THE APU IF INTERNAL DAMAGE IS START? FOUND, REPLACE THE APU
(AMM 49-11-00/401). NO
 IF THE DAMAGE CAN BE REPAIRED, REPAIR THE DAMAGE THAT YOU FIND.
YES
2 DID THE EGT INDICATOR SHOW
52 REPLACE THE APU
A TEMPERATURE OF 760`C OR

(AMM 49-11-00/401). GREATER DURING THE APU
OPERATION?

EGT Is Greater Than 760`C
Figure 135

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 ú  Jul 12/00 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
AUTOMATIC SHUTDOWN  PREREQUISITES 
FOR A LOW OIL PRES- MAKE SURE THIS SYSTEM WILL OPERATE: 
SURE OR THE "LOW OIL  APU (AMM 49-11-00/201) 
 
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