S 424-016-C00

 (2)  
Install the oil temperature bulb:

 (a)  
Lubricate a new O-ring with engine oil.

 (b)  
Put the O-ring on the oil temperature bulb.

 (c)  
Screw the bulb into the boss on the scavenge filter housing.

 (d)  
Tighten the bulb.

 (e)  
Install lockwire on the bulb.

 S 434-017-C00
 (3)
Connect the electrical connector to the oil temperature bulb.

 S 864-055-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) AIRPLANES WITHOUT THE ENGINE INSTRUMENT SYSTEM (EIS); ENG 1 OIL TEMP & PRESS AC
 b)  AIRPLANES WITH THE ENGINE INSTRUMENT SYSTEM (EIS) AND WITH SECONDARY DISPLAY UNIT P/N 10-62178-201; EIS SEC 1
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 79-34-01
 ALL  ú ú C02 Page 405 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
c) AIRPLANES WITH THE ENGINE INSTRUMENT SYSTEM (EIS) AND
 WITH SECONDARY DISPLAY UNIT P/N 10-62178-202;
 EIS SEC 1
 EIS SEC 5
 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) AND
 WITH SECONDARY DISPLAY UNIT P/N 10-62178-201;
 EIS SEC 3
 c) AIRPLANES WITH THE ENGINE INSTRUMENT SYSTEM (EIS) AND
 WITH SECONDARY DISPLAY UNIT P/N 10-62178-202;
 EIS SEC 3
 EIS SEC 6
 S 794-029-C00
 (5)  When you do the next engine run, do the idle leak check
 (AMM 71-00-00/501, Test No. 3).
 (a) Make sure that both oil temperature indications show
 approximately the same temperature.
 S 614-019-C00
 (6)  Fill the engine with oil (AMM 12-13-11/301).
 S 414-020-C00
 (7)  Close the left fan cowl panel (AMM 71-11-02/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 79-34-01
 ALL  ú ú C01 Page 406 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 TEMPERATURE INDICATOR - REMOVAL/INSTALLATION
________________________________________________
 1.  General
_______
 A.  This procedure has two tasks:
 (1)  
The first task is the removal of the oil temperature indicator.

 (2)  
The second task is the installation of the indicator.

 B.  The oil temperature indicator is located on the pilot's center instrument panel (P2).
 TASK 79-34-02-004-001-C00
 2.  Oil Temperature Indicator Removal
_________________________________
 A.  Access
 (1)  Location Zone
 101 Control Cabin

 B.  Procedure
 S 864-002-C00
 (1)  Open this circuit breaker and attach a DO-NOT-CLOSE tag:
 (a)  P6 Load Control Center
 1) ENG 1 OIL TEMP & PRESS AC
 2) ENG 2 OIL TEMP & PRESS AC

 S 034-003-C00
 (2)  Loosen the clamp adjustment screw for the oil temperature indicator on the pilot's center instrument panel (P2).
 NOTE: The adjustment screw is the larger screw located above and to
____
 the right of the indicator.

 S 024-004-C00
 (3)  
Pull the indicator out from the panel so you can get access to the electrical connector.

 S 034-005-C00

 (4)  
Disconnect the electrical connector from the indicator.

 (a)  If both oil temperature indicators are removed at the same time, clearly identify the D604 connector for engine No. 1 and the D606 connector for engine No. 2.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 滑油 OIL(70)