737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
FROM SHEET 1 (BLOCK 5)
YES
NO
7
DO THE MEC FUEL SHUTOFF
LEVER POSITION CHECK (CUTOFF
POSITION CHECK)(AMM 71-00-59/
101, FIG. 114).
IS THE CUTOFF POSITION CHECK CORRECT?
YES
YES
NO
27 DO A DRY MOTOR (AMM 71-00-00/201) FOR 90 SEC-ONDS. START THE ENGINE AGAIN.
NO
DOES THE PROBLEM CONTINUE?
YES
YES
11 DO THE FUEL NOZZLE LEAK
CHECK (AMM 71-00-59/101,
FIG. 115).
IS DAMAGE/LEAKING NOZZLE
FOUND?
NO
YES
13 EXAMINE THE MAGNETIC CHIP
DETECTORS (AMM 79-00-00/601).
ARE SIGNS OF ENGINE OR
GEARBOX FAILURE FOUND?
NO
YES
15 EXAMINE THE FUEL FILTER(AMM 73-11-02/601) FOR
METALLIC MATERIAL.
IS UNUSUAL AMOUNT OF METALLIC MATERIAL FOUND?
NO
Instantaneous Lightup (Torching) with Start Lever Movement/Internal
Engine Fire After Shutdown
Figure 107 (Sheet 2)
A09643
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-00-41
ALL ú
ú C02 Page 117
ú Nov 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SLOW START/HUNG START BEFORE STARTER CUTOUT; EGT USUAL
YES
NO
NO
YES
YES
3 DO THE PNEUMATIC LEAK TEST
(AMM 71-00-00/501, TEST 1) AND
EXAMINE START DUCT FOR TOO
MUCH LEAKAGE.
IS LEAKAGE FOUND?
NO
YES
NO
NO
5 DO THE MEC SPECIFIC GRAVITY SETTING CHECK
(AMM 71-00-58/101, FIG. 103).
IS THE SETTING WITHIN THE PERMITTED RANGE FOR THE FUEL?
YES
SEE SHEET 2 (BLOCK 6)
PREREQUISITES
ENGINE OPERATION
NO
21 ON CIRCUIT BREAKER PANEL
P6, OPEN APPLICABLE ENG LEFT
AND RIGHT IGNITION, AND ENG
START VALVE CIRCUIT BREAKERS.
OPEN LEFT FAN COWL PANEL AND DISCONNECT CONNECTOR D424 FROM START VALVE. CLOSE START YESVALVE CIRCUIT BREAKER.
POSITION APPLICABLE ENGINE START SWITCH TO GRD POSITION.
DO A CHECK FOR 28V DC ATRELAY CONNECTOR SOCKET 2 (AIRPLANE GROUND).
IS THERE 28V DC?
NO
22 DO THE TROUBLESHOOTING OF THE APU FOR DUCT PRESSURE
FLUCTIONS (AMM 49-00-00/101)
IS DUCT PRESSURE NORMAL?
YES
42 REPLACE THE APPLICABLE
START/IGNITION SWITCH, S266 OR
S267 (WDM 80-11-11).
PUT THE AIRPLANE BACK TO THE USUAL CONDITION.
43 REPLACE THE APPLICABLE N2
TACHOMETER RELAY, R357 OR R358
(WDM 80-11-11).
PUT THE AIRPLANE BACK TO THE USUAL CONDITION.
Slow Start/Hung Start Before Starter Cutout; EGT Usual
Figure 108 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-00-41
ALL ú
ú C01 Page 118
ú Jul 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
FROM SHEET 1 (BLOCK 5)
YES
YES
6
EXAMINE ALL CDP TUBE
CONNECTIONS FOR LEAKS, AND CDP
TUBING FOR BLOCKAGE OR DAMAGE
(AMM 71-00-59/101, FIG. 104).
ARE LEAKS/BLOCKAGE/DAMAGE FOUND?
AND 9TH-STAGE PNEUMATIC DUCTING/VALVES FOR SIGNS OF LEAKS (AMM 71-00-58/101, FIG. 107).
ARE LEAKS FOUND?
COMPONENTS.
DO THE VSV ACTUATOR RIG CHECK (AMM 75-31-00/501), THEN (AMM 75-32-00/501). ADJUST THE VSV FEEDBACK CABLE IS THE RIG CHECK CORRECT? (AMM 75-31-02/501).
YES
YES
11 EXAMINE THE MAGNETIC CHIP
51 REPLACE THE ENGINE
DETECTORS (AMM 79-00-00/601). (AMM 71-00-02/401).
ARE SIGNS OF ENGINE OR
GEARBOX FAILURE FOUND?
NO SEE SHEET 3
(BLOCK 12)
Slow Start/Hung Start Before Starter Cutout; EGT Usual
Figure 108 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：737-300 400 500 AMM 飞机维护手册 动力装置 POWER PLANT 2
