79-31-00
ALL ú ú C02 Page 503 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 865-018-C00
(2) 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 215-020-C00
(3)
Make sure the OIL QTY display goes out of view.
S 865-121-C00
(4)
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 865-026-C00
(5) 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.
TASK 79-31-00-735-029-C00
3. System Test and Adjust - Oil Quantity Indicating System
_______________________________________________________
A. Equipment
(1) Container - 5 gallon (20 liter) capacity - for oil
B. Consumable Materials
(1) D00599, Oil, (CP2442) engine - CFMI SB 79-001
C. References
(1)
AMM 12-13-11/301, Engine Oil Servicing
(2)
AMM 24-22-00/201, Manual Control
(3)
AMM 71-11-02/201, Fan Cowl Panel
D. Access
(1)
Location Zones
506 Engine No. 1
606 Engine No. 2
(2)
Access Panels 5737L/5746L Engine No. 1 - Fan Cowl Assembly 5837R/5846R Engine No. 2 - Fan Cowl Assembly
E. Prepare to Do the System Test (Fig. 501)
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79-31-00
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ////////////////////////
SEE A
OIL QUANTITY TRANSMITTER
FILLER CAP
SCUPPER
OIL TANK
FWD
A
Oil Quantity Indicating System Figure 501
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
79-31-00
ALL ú ú C02 Page 505 ú Nov 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 015-030-C00
(1)
Open the fan cowl panel (AMM 71-11-02/201).
S 685-031-C00
(2)
Drain the engine oil tank (AMM 12-13-11/301).
S 865-032-C00
(3)
Supply the electrical power (AMM 24-22-00/201).
(a) Remove the DO-NOT-OPERATE tag from the BAT switch.
S 865-033-C00
(4) 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 QTY 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 QTY
b) AIRPLANES WITH THE ENGINE INSTRUMENT SYSTEM (EIS); EIS SEC 3
F. AIRPLANES WITHOUT THE ENGINE INSTRUMENT SYSTEM (EIS); System Test and Adjustment for the Oil Quantity Indication System (Fig. 501, Fig. 502)
S 615-040-C00
(1)
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