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 (a)  Remove the DO-NOT-OPERATE tag from the BAT switch.
 S 865-059-C00
 (5)  Make sure these circuit breakers are closed:
 (a)  P6-2 Load Control Center 1) For Engine No. 1: a) AIRPLANES WITHOUT THE ENGINE INSTRUMENT SYSTEM (EIS); ENG 1 OIL TEMP & PRESS AC
 b)  AIRPLANES WITH THE ENGINE INSTRUMENT SYSTEM (EIS); EIS SEC 1 EIS SEC 2
 2) For engine No. 2: a) AIRPLANES WITHOUT THE ENGINE INSTRUMENT SYSTEM (EIS); ENG 2 OIL TEMP & PRESS AC
 b)  AIRPLANES WITH THE ENGINE INSTRUMENT SYSTEM (EIS); EIS SEC 3 EIS SEC 4
 F.  Test of the Oil Pressure Indicating System
 S 865-019-C00
 (1)  
Apply 80 psi (551 kPa) air pressure to the oil pressure transmitter.

 S 215-020-C00

 (2)  
Make sure the oil pressure indication reads 80 |3 psi.

 S 865-021-C00

 (3)  
Keep the pressure at 80 psi (551 kPa) for 1 minute with the air pressure supply shut off.

 S 215-022-C00

 (4)
Monitor the oil pressure indicator to examine the system for leaks.

 (a)  If there are leaks in the system, the indication value will decrease.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 79-32-00
 ALL  ú ú C02 Page 504 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 865-060-C00
 (5)  Open these circuit breakers and attach DO-NOT-CLOSE tags:
 (a) P6-2 Load Control Center
 1) For Engine No. 1:
 a) AIRPLANES WITHOUT THE ENGINE INSTRUMENT SYSTEM (EIS);
 ENG 1 OIL TEMP & PRESS AC
 b) AIRPLANES WITH THE ENGINE INSTRUMENT SYSTEM (EIS);
 EIS SEC 1
 2) For engine No. 2:
 a) ENG 2 OIL TEMP & PRESS AC
 b) AIRPLANES WITHOUT THE ENGINE INSTRUMENT SYSTEM (EIS);
 ENG 2 OIL TEMP & PRESS AC
 c) AIRPLANES WITH THE ENGINE INSTRUMENT SYSTEM (EIS);
 EIS SEC 4
 S 215-061-C00
 (6)  AIRPLANES WITH OIL TEMPERATURE INDICATORS;
 (AIRPLANES WITHOUT THE ENGINE INSTRUMENT SYSTEM (EIS));
 Make sure the indicator goes back to zero or less.
 S 215-062-C00
 (7)  AIRPLANES WITH THE ENGINE INSTRUMENT SYSTEM (EIS);
 Make sure the pointer goes back to zero or less and goes out of view
 after two seconds.
 S 865-033-C00
 (8)  Remove the DO-NOT-CLOSE tags and close these circuit breakers:
 (a) P6-2 Load Control Center
 1) For engine No. 1:
 a) AIRPLANES WITHOUT THE ENGINE INSTRUMENT SYSTEM (EIS);
 ENG 1 OIL TEMP & PRESS AC
 b) AIRPLANES WITH THE ENGINE INSTRUMENT SYSTEM (EIS);
 EIS SEC 1
 2) For engine No. 2:
 a) AIRPLANES WITHOUT THE ENGINE INSTRUMENT SYSTEM (EIS);
 ENG 2 OIL TEMP & PRESS AC
 b) AIRPLANES WITH THE ENGINE INSTRUMENT SYSTEM (EIS);
 EIS SEC 4
 S 865-039-C00
 (9)  Decrease the air supply pressure to 45 psi (310 kPa).
 S 215-040-C00

 (10) Make sure the oil pressure indication reads 45 psi |3 psi.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 79-32-00
 ALL  ú ú C03 Page 505 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 865-041-C00
 (11) Decrease the air supply pressure to the atmospheric pressure and monitor the oil pressure indicator.
 (a)  The indication must read 0 psi |3 psi.
 G. Put the Airplane Back to its Usual Condition
 S 085-042-C00
 (1) Remove the air pressure line from the oil pressure transmitter.
 (a)  Discard the O-ring.
 S 435-043-C00
 (2)  
Connect the tee fitting for the supply oil pressure to the oil pressure transmitter with a new O-ring, lubricated with engine oil.

 S 415-044-C00

 (3)  
　
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