(a)  Set the BAT switch on the Electrical Meters Battery and Galley Power Module (P5-13) to the OFF position and install a DO-NOT-OPERATE tag.
 G.  AIRPLANES WITH THE ENGINE INSTRUMENT SYSTEM (EIS); Do a System Test of the Oil Quantity Indication System
 S 615-066-C00
 (1)  
Open the oil tank filler cap (AMM 12-13-11/301).

 S 615-067-C00

 (2)
Add 0.5 U.S. gallons (1.9 liters) of oil to the dry oil tank.

 S 215-068-C00

 (3)  
Make sure the applicable OIL QTY display reads zero to 6%.

 S 615-069-C00

 (4)  
Add 2.50 U.S. gallons (9.50 liters) of oil to the oil tank.

 S 215-070-C00

 (5)  
Make sure the applicable OIL QTY display reads 60% |6.

 S 615-071-C00

 (6)  
Add 1.75 U.S. gallons (6.65 liters) of oil to the oil tank.

 (7)  
Make sure the applicable OIL QTY display reads 94 - 100%.

 S 215-072-C00
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 865-073-C00
 (8)  Open this circuit breaker and attach a DO-NOT-CLOSE tag:
 (a)  P6-2 Load Control Center
 1) For Engine No. 1:
 a) EIS SEC 1

 2)  For Engine No. 2:
 a) EIS SEC 3

 S 215-075-C00
 (9)
Make sure the applicable OIL QTY display goes out of view.

 S 865-124-C00

 (10)
 Remove the DO-NOT-CLOSE tag and close this circuit breaker:

 (a)  P6-2 Load Control Center
 1) For Engine No. 1:
 a) EIS SEC 1

 2)  For Engine No. 2:
 a) EIS SEC 3

 S 865-078-C00
 (11) Remove the electrical power (AMM 24-22-00/201).
 (a)  Set the BAT switch on the Electrical Meters Battery and Galley Power Module (P5-13) to the OFF position and install a DO-NOT-OPERATE tag.
 S 415-079-C00
 (12) Close the fan cowl panel (AMM 71-11-02/201).
 TASK 79-31-00-705-116-C00
 4.  AIRPLANES WITH OIL TEMPERATURE INDICATORS; (AIRPLANES WITHOUT THE ENGINE INSTRUMENT SYSTEM (EIS)); Calibrate the Oil Quantity Indicator with Oil in the Tank
_________________________________________________________
 A.  General
 (1)  This procedure is for the calibration of oil quantity indicators after you replaced a defective indicator.
 B.  Equipment
 (1)  
PSD60-2R - Simmonds Precision Capacitance
 Tester,
 Simmonds Precision Product, Support Division,
 5250 N.W. 23rd Ave.,
 Ft. Lauderdale, Florida 33309

 (2)  
Model GTF-2, P/N 361-012-001 - Gull System Test Unit, Gull Airborne Instruments Inc., 55 Engineers Road, Smithtown, N.Y. 11787

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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 ALL  ú ú C03 Page 510 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(3)  
F72731-118 "T" cable,
 Simmonds Precision Product, Support Division,
 5250 N.W. 23rd Ave.,
 Ft. Lauderdale, Florida 33309

 (4)  
F72731-114 "T" cable,
 Gull Airborne Instruments Inc.,
 55 Engineers Road,
 Smithtown, N.Y. 11787

 (5)  
Tester grounding cable, banana plug to
 alligator clip

 C. Consumable Materials
 (1)  D00599, Oil, (CP2442) engine - CFMI SB 79-001
 D. References
 (1)  
AMM 12-13-11/301, Engine Oil Servicing

 (2)  
AMM 24-22-00/201, Manual Control

 (3)  
AMM 71-00-44/101, Power Plant (Oil Indicating)

 E. Access
 (1)  
　
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