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  
1  
2 
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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.
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 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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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