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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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IF THE PROBLEM CONTINUES,
YES
REPLACE THE BLEED AIR VALVE, V56 (AMM 49-52-11/401).

EGT Is Too High or Out of Control during the Application of the Bleed Load
Figure 122 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT THE ETC ú
 49-00-00
 ú ú 02 Page 180N ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A53639
EGT IS TOO HIGH OR PREREQUISITES OUT OF CONTROL DUR-
NONE ING THE APPLICATION
OF THE BLEED LOAD

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

2.
PROPORTIONAL CONTROL VALVE PROBLEM (AMM 49-52-31/401)

3.
ELECTRONIC TEMPERATURE CONTROL, M1459, PROBLEM (AMM 49-61-71/401)

4.
TEMPERATURE SENSOR, T2, FOR THE COMPRESSOR INLET PROBLEM (AMM 49-61-32/401)

5.
ETC THERMOCOUPLE PROBE PROBLEM (AMM 49-71-31/401)

6.
CLOGGED TEE FITTING FOR THE CONTROL AIR LINE

7.
3-WAY SOLENOID VALVE PROBLEM (AMM 49-52-61/401)

8.
BLEED AIR VALVE, V56, PROBLEM (AMM 49-52-11/401).


FAULT ISOLATION:

SEE SHEET 2 (BLOCK 2)
EGT Is Too High or Out of Control during the Application of the Bleed Load
Figure 122A (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH THE ETC ú
 49-00-00
 ú ú 02 Page 180O ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E05975
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES /MAINTENANCE MANUAL ////////////////////////
FROM SHEET 1
(BLOCK 1)

YES

YES
2


MAKE SURE THE TEE FITTING

52 CLEAN THE TEE FITTING FOR FOR THE CONTROL AIR LINE IS THE CONTROL AIR LINE NOT CLOGGED. (AMM 49-52-91/701) OR REPLACE THE TEE FITTING.
NOTE:THE ORIFICE OF THE TEE
FITTING MUST BE 0.080
TO 0.084 INCH

(2.03 TO 2.13 mm).
 IS THE TEE FITTING
CLOGGED?


NONO
3 DO A CHECK OF THE INSTAL-53 REMOVE AND INSTALL THE
LATION OF THE 3-WAY SOLENOID 3-WAY SOLENOID VALVE OR
VALVE.REPLACE THE VALVE

IS THE 3-WAY SOLENOID (AMM 49-52-61/401).
VALVE INSTALLED CORRECTLY?


YES NO
4 REPLACE THE PROPORTIONAL 54 THE SYSTEM IS OK.
CONTROL VALVE (AMM 49-52-31/
401).

 DOES THE PROBLEM CONTINUE?

YES YES

5 DO THE ADJUSTMENT OF THE
ELECTRONIC TEMPERATURE CONTROL
(AMM 49-61-71/501).


DOES THE EGT ADJUST TO THE RECOMMENDED TEMPERATURE RANGE?

NO SEE SHEET 3
(BLOCK 21)

EGT Is Too High or Out of Control during the Application of the Bleed Load
Figure 122A (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH THE ETC ú
 49-00-00
 ú ú 02 Page 180P ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E05983
FROM SHEET 2 (BLOCK 5)
NO
NO

21 REPLACE THE ELECTRONICTEMPERATURE CONTROL, M1459 (AMM 49-61-71/401).

DOES THE PROBLEM CONTINUE?YES

NO

22 REPLACE THE TEMPERATURE SENSOR, T2, FOR THE COMPRESSOR INLET (AMM 49-61-32/401).

DOES THE PROBLEM CONTINUE? YES

NO

23 REPLACE THE ETC THERMO-COUPLE PROBES (AMM 49-71-31/ 401).

DOES THE PROBLEM CONTINUE?

EGT Is Too High or Out of Control during the Application of the Bleed Load
Figure 122A (Sheet 3)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH THE ETC ú
 49-00-00
 ú ú 02 Page 180Q ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E05990
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES /MAINTENANCE MANUAL ////////////////////////
BLEED AIR FOR MAIN ENGINE START IS NOT SUFFICIENT PREREQUISITES
 
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