S 715-003-C00
(3)
Make sure the oil temperature indication for the two engines is approximately equal.
S 865-004-C00
(4)
Stop the engines (AMM 71-00-00/201).
TASK 79-34-00-735-006-C00
3. System Test - Oil Temperature Indicating System
_______________________________________________
A. Equipment
(1)
Thermometer - Digital, VWR Model 400, VanWaters and Rogers, 100 Rue McArthur, Valley Field, Quebec, Canada.
(2)
Probe - Temperature, YS1 409B, VanWaters and Rogers.
(3)
Resistor, 130 ohm - 1% accuracy, local purchase.
B. References
(1)
AMM 24-22-00/201, Manual Control
(2)
AMM 31-42-01/401, Engine Instrument System
(3)
AMM 71-11-02/201, Fan Cowl Panels
C. Access
(1)
Location Zone
502 LH Fan Cowl, Left Nacelle
602 LH Fan Cowl, Right Nacelle
(2)
Access Panels
5746L Left Fan Cowl Panel, Left Nacelle
5846R Left Fan Cowl Panel, Right Nacelle
D. Prepare for the Test (Fig. 501)
S 015-007-C00
(1)
Open the left fan cowl panel (AMM 71-11-02/201).
S 485-008-C00
(2)
Attach the temperature probe to the "oil-out" tube for the scavenge oil filter.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
79-34-00
ALL ú ú C02 Page 502 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 OUT" TUBE OIL TEMPERATURE BULB
CONNECTOR
"OIL IN" TUBE
SCAVENGE OIL FILTER
FWD
A
Oil Temperature Indicating System Test Connections
Figure 501 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ENGINES WITHOUT ú
79-34-00
CFMI SB 79-063 ú ú C01 Page 503 ú Jul 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
"OIL OUT" TUBE SEEB
OIL TEMPERATURE
ELECTRICAL BULB
CONNECTOR
"OIL IN" TUBE
FWD
SCAVENGE
OIL FILTER
B
Oil Temperature Indicating System Test Connections
Figure 501 (Sheet 2)
E33032
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ENGINES WITH ú
79-34-00
CFMI SB 79-063 ú ú C01 Page 504 ú Jul 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
E. Do the System Test
S 865-009-C00
(1) Supply electrical power to the applicable engine (AMM 24-22-00/201).
(a) Remove the DO-NOT-OPERATE tag from the BAT switch.
S 865-027-C00
(2) 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 TEMP & PRESS AC
b) AIRPLANES WITH THE ENGINE INSTRUMENT SYSTEM (EIS) AND SECONDARY ENGINE AND HYDRAULICS DISPLAY P/N 10-62178-201; EIS SEC 1 EIS SEC 2
c) AIRPLANES WITH THE ENGINE INSTRUMENT SYSTEM (EIS) AND SECONDARY ENGINE AND HYDRAULICS DISPLAY P/N 10-62178-202; EIS SEC 1 EIS SEC 2 EIS SEC 5
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