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时间:2011-04-04 10:07来源:蓝天飞行翻译 作者:航空
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 71-00-00
 ALL  ú ú C01 Page 510 ú Jul 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
AIRPLANE NO. DATE
TEST NO. 6 - MEC TRIM 
POS ENG  OAT  BARO  WIND  PMC OFF (%N2)  PMC ON (%N1) 
(KNOTS) VELOCITY  (DEGREES) DIRECTION  TARGET  RECORDED  TARGET  RECORDED 


TEST NO. 7 - VIBRATION SURVEY 
ENG POS  OAT  BARO  STATIC T.O. TARGET (%N1)  SELECTOR SWITCH POSITION 

ACCEL  DECEL 
%N1  %N2  (UNITS) VIBRATION READING  %N1  %N2  (UNITS) VIBRATION READING 

 

 


VIBRATION PEAK  VIBRATION READING (UNITS)  READING (UNITS) MEAN VIBRATION  SOURCE 
%N1  %N2  SEC  SEC 30  SEC  60 SEC  SEC  90 SEC  SEC  120 SEC  FAN LPT HPT HPC 

 

 


TEST NO. 8 - ACCEL/DECEL CHECK 
POS ENG  OAT  BARO  TARGET VALUES (%N1)  ACCEL TIME (SEC) 
STATIC T.O.  ACCEL CHECK TARGET  TO 40% N1 LOW IDLE  TARGET ACCEL CHECK 40% N1 TO  TARGET ACCEL CHECK HIGH IDEL TO 

REMARKS; DISCREPANCIES
Engine Data and Record Sheet
Figure 501 (Sheet 2)

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 71-00-00
 ALL  ú ú C01 Page 511 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TEST NO. 12 ENGINE RUN DIAGNOSTIC CHECKS

NO. 1 
ENGINE MODEL CFM56-

NO. 2

RECORD PLA GAIN ADJUSTMENT
PLA GAIN, VOLTS DC 
PMC PLA RVDT DIFFERENTIAL VOLTAGE 

Engine Data and Record Sheet
Figure 501 (Sheet 3)

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 71-00-00
 ALL  ú
 ú  C02  Page 512
 ú  Jul 12/01 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
K20697
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TEST NO. 1 - PNEUMATIC LEAK TEST
________________________________
 TASK 71-00-00-795-001-C00
 2.  Test No. 1 - Pneumatic Leak Test________________________________
 A. References
 (1)
AMM 36-11-05/501, Engine Bleed Air Distribution System

 B.
Access

 (1)  
Location Zones
 506 Engine No. 1
 606 Engine No. 2


 (2)  
Access Panels
 5737L/5837R Fan Cowl Assy
 5746L/5846R Fan Cowl Assy
 5738L/5838R Thrust Reverser Cowl Assy
 5739L/5839R Thrust Reverser Cowl Assy


 C.
Procedure


 S 795-028-C00
 (1) Do the Pneumatic Ducts Leakage Test (AMM 36-11-05/501).
 (a) Examine these pneumatic ducts for a leak:
 NOTE:____You cannot have a jet of air at the couplings. You can have a small leakage around the coupling.
 1) Starter duct (up to the start valve), 2) 5th- and 9th-stage ducts (up to the bleed air check valve and the high stage valve), 3) Anti-ice duct on the inlet cowl (up to the TAI valve).
 S 365-023-C00
 (2) If it is necessary, repair the leaks.
 (a) Do this test again.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 71-00-00
 ALL  ú ú C02 Page 513 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TEST NO. 2 - ENGINE MOTORING
 
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