79-31-00
ALL ú ú C01 Page 517 ú Nov 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(m)
Switch the CAPACITANCE FUNCTION switch to A/C + PROBE SIM + COMP SIM position.
(n)
Press the OIL QTY TEST switch momentarily and release.
(o)
Adjust the "E" screw to read 0 gallons or liters, if it is necessary.
H. Put the Airplane Back to it Usual Condition
S 865-114-C00
(1) Open these circuit breakers and attach DO-NOT-CLOSE tags:
(a) P6-2 Load Control Center
1) For Engine No. 1:
a) ENG 1 OIL QTY
2) For Engine No. 2:
a) ENG 2 OIL QTY
S 085-089-C00
(2) Disconnect the test set as follows:
(a)
Turn the tester to the OFF position.
(b)
Disconnect the tester from the "T" cable and the airframe ground.
(c)
Disconnect the "T" cable from the oil quantity indicator plug and the airplane electrical connector.
S 435-090-C00
(3)
Connect the electrical connector to the indicator.
S 865-091-C00
(4)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:
(a) P6-2 Load Control Center
1) For Engine No. 1:
a) ENG 1 OIL QTY
2) For Engine No. 2:
a) ENG 2 OIL QTY
S 215-093-C00
(5)
Make sure the oil quantity indicator reads 4.50 gallons (engine 1) | 1/2 dial division (17.10 liters) and 4.75 gallons (engine 2) | 1/2 dial division (18.05 liters).
(6)
Return the panel lighting to the normal level.
(7)
Remove the power from the airplane, if it is not necessary.
S 445-094-C00
S 865-095-C00
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79-31-00
ALL ú ú C01 Page 518 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
OIL QUANTITY TRANSMITTER - REMOVAL/INSTALLATION
_______________________________________________
1. General
_______
A. This procedure contains two tasks. The first task is to remove the oil quantity transmitter. The second task is to install the oil quantity transmitter. The oil quantity transmitter is found in the top of the oil tank on the right side of the engine.
TASK 79-31-01-004-001-C00
2. Oil Quantity Transmitter Removal
________________________________
A. References
(1) AMM 71-11-02/201, Fan Cowl Panel
B. 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
C. Procedure (Fig. 401)
S 864-049-C00
(1) 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 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
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79-31-01
ALL ú ú C02 Page 401 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
LUBE
SCAVENGE
TUBE
ELECTRICAL
CONNECTOR
LUBE
SUPPLY
TUBE
OIL
QUANTITY
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本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 滑油 OIL(50)
