(a) Set the BAT switch on the Electrical Meters Battery and Galley Power Module (P5-13) to the OFF position and install a DO-NOT-OPERATE tag.
G. AIRPLANES WITH THE ENGINE INSTRUMENT SYSTEM (EIS); Do a System Test of the Oil Quantity Indication System
S 615-066-C00
(1)
Open the oil tank filler cap (AMM 12-13-11/301).
S 615-067-C00
(2)
Add 0.5 U.S. gallons (1.9 liters) of oil to the dry oil tank.
S 215-068-C00
(3)
Make sure the applicable OIL QTY display reads zero to 6%.
S 615-069-C00
(4)
Add 2.50 U.S. gallons (9.50 liters) of oil to the oil tank.
S 215-070-C00
(5)
Make sure the applicable OIL QTY display reads 60% |6.
S 615-071-C00
(6)
Add 1.75 U.S. gallons (6.65 liters) of oil to the oil tank.
(7)
Make sure the applicable OIL QTY display reads 94 - 100%.
S 215-072-C00
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S 865-073-C00
(8) Open this circuit breaker and attach a DO-NOT-CLOSE tag:
(a) P6-2 Load Control Center
1) For Engine No. 1:
a) EIS SEC 1
2) For Engine No. 2:
a) EIS SEC 3
S 215-075-C00
(9)
Make sure the applicable OIL QTY display goes out of view.
S 865-124-C00
(10)
Remove the DO-NOT-CLOSE tag and close this circuit breaker:
(a) P6-2 Load Control Center
1) For Engine No. 1:
a) EIS SEC 1
2) For Engine No. 2:
a) EIS SEC 3
S 865-078-C00
(11) Remove the electrical power (AMM 24-22-00/201).
(a) Set the BAT switch on the Electrical Meters Battery and Galley Power Module (P5-13) to the OFF position and install a DO-NOT-OPERATE tag.
S 415-079-C00
(12) Close the fan cowl panel (AMM 71-11-02/201).
TASK 79-31-00-705-116-C00
4. AIRPLANES WITH OIL TEMPERATURE INDICATORS; (AIRPLANES WITHOUT THE ENGINE INSTRUMENT SYSTEM (EIS)); Calibrate the Oil Quantity Indicator with Oil in the Tank
_________________________________________________________
A. General
(1) This procedure is for the calibration of oil quantity indicators after you replaced a defective indicator.
B. Equipment
(1)
PSD60-2R - Simmonds Precision Capacitance
Tester,
Simmonds Precision Product, Support Division,
5250 N.W. 23rd Ave.,
Ft. Lauderdale, Florida 33309
(2)
Model GTF-2, P/N 361-012-001 - Gull System Test Unit, Gull Airborne Instruments Inc., 55 Engineers Road, Smithtown, N.Y. 11787
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737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(3)
F72731-118 "T" cable,
Simmonds Precision Product, Support Division,
5250 N.W. 23rd Ave.,
Ft. Lauderdale, Florida 33309
(4)
F72731-114 "T" cable,
Gull Airborne Instruments Inc.,
55 Engineers Road,
Smithtown, N.Y. 11787
(5)
Tester grounding cable, banana plug to
alligator clip
C. Consumable Materials
(1) D00599, Oil, (CP2442) engine - CFMI SB 79-001
D. References
(1)
AMM 12-13-11/301, Engine Oil Servicing
(2)
AMM 24-22-00/201, Manual Control
(3)
AMM 71-00-44/101, Power Plant (Oil Indicating)
E. Access
(1)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 滑油 OIL(46)
