S 215-007-C00
(3)
Make sure the oil pressure value for the engine system in test is approximately the same as that for the other engine.
TASK 79-32-00-735-008-C00
3. System Test - Oil Pressure Indicating System
____________________________________________
A. Equipment
(1)
Vent Valve
(2)
Air pressure gauge, 0-100 psi (0-700 kPa) |1% accuracy.
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(3) Shut-off Valve
B. Consumable Materials
(1) 0-100 psi (0-700 kPa) adjustable dry air pressure source.
C. References
(1) 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 for the Test (Fig. 501)
S 015-009-C00
(1) Open the left fan cowl panel (AMM 71-11-02/201).
S 035-010-C00
WARNING:_______DO NOT LET THE ENGINE OIL STAY ON YOUR SKIN. IF THE ENGINE OIL STAYS ON YOUR SKIN, INJURY CAN OCCUR.
BE CAREFUL AROUND THE ENGINE OIL SYSTEM IMMEDIATELY AFTER ENGINE SHUT-DOWN. THE ENGINE OIL TEMPERATURE STAYS HIGH FOR SOME TIME AFTER THE ENGINE SHUT-DOWN AND CAN CAUSE INJURY.
CAUTION: IMMEDIATELY CLEAN OFF ALL ENGINE OIL THAT FALLS ON THE PAINTED
_______
SURFACES AND RUBBER PARTS OF THE AIRPLANE. THE SPECIFIED OIL
FOR THIS OIL SYSTEM WILL CAUSE DAMAGE TO THE PAINTED SURFACES
AND SOME TYPES OF RUBBER AND MUST NOT BE PERMITTED TO TOUCH
THESE PARTS OF THE ENGINE.
USE VERY CLEAN CONTAINERS AND EQUIPMENT. OIL CONTAMINATION BY SMALL QUANTITIES OF SOME ALKALINE CLEANERS CAN CAUSE A FAILURE OF THE SYNTHETIC OIL.
DO NOT PUT THE OIL THAT IS DRAINED FROM THE ENGINE BACK INTO THE ENGINE.
(2)
Disconnect the tee fitting for the oil supply pressure tube from the oil pressure transmitter.
S 485-011-C00
(3)
Connect an air pressure source to the pressure port for the oil
supply on the transmitter.
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SEE A
ELECTRICAL
LOW OIL PRESSURE
CONNECTOR
WARNING SWITCH
OIL PRESSURE TRANSMITTER
FORWARD TEE FITTING
PRESSURE TUBE OIL SUPPLY CONNECTOR ELECTRICAL FWD
VENT PRESSURE TUBE
FROM THE TGB
A
Oil Pressure Indicating System Test Connections
Figure 501
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S 865-012-C00
(4) Supply electrical power to the applicable engine.
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本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 滑油 OIL(55)
