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时间:2011-04-09 10:16来源:蓝天飞行翻译 作者:航空
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 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
 S 865-006-C00
 (2)
Operate each engine at the same power setting (AMM 71-00-00/201).

 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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 79-32-00
 ALL  ú ú C02 Page 501 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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)  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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 79-32-00
 ALL  ú ú C02 Page 502 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
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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 79-32-00
 ALL  ú ú C03 Page 503 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 865-012-C00
 (4)  Supply electrical power to the applicable engine.
 
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