-Inlet cover part No. LMC11G84-1
-Exhaust cover part No. LMC11G84-2, or
Texstar Plastics,
802 Ave J East, P.O. Box 534036,
Grand Prairie, TX 75051
-Inlet cover part No. 5101505
-
Exhaust cover part No. 5101504
B.
Consumable Materials
(1)
Oil - Engine (AMM 70-10-01/201)
(2)
Oil - Preservative, MIL-L-6085, CP2259
(contains a corrosion inhibitor)
(AMM 70-10-01/201)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-00-03
ALL ú ú C01 Page 208 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(3)
Oil, Additive - Anti-Corrosion, CP2309
(AMM 70-10-01/201)
C.
References
(1)
AMM 12-13-11/301, Engine Servicing
(2)
AMM 71-00-00/201, Power Plant
D.
Access
(1)
Location Zones
506 Engine No. 1
606 Engine No. 2
E.
Power Plant Preservation
S 612-038-C00
(1) Fill the engine oil tank (AMM 12-13-11/301) with a minimum of 20 quarts (19 liters) of one of the mixtures that follow:
(a)
Engine oil and at least 5 percent by volume preservative oil (CP2259) or,
(b)
Engine oil and at least 7 percent by volume anti-corrosion oil additive (CP2309).
S 862-039-C00
WARNING:_______USE AMM 71-00-00/201 TO OPERATE THE POWER PLANT. IF YOU DO NOT USE THIS PROCEDURE, YOU CAN CAUSE DAMAGE TO EQUIPMENT OR INJURY TO PERSONS.
(2)
Use the Power Plant Operation (Normal) procedure to start the engine (AMM 71-00-00/201).
S 862-040-C00
(3)
Let the engine become stable at low idle for 15 to 20 minutes.
S 862-041-C00
(4)
Use the Power Plant Operation (Normal) Procedure to do the engine shutdown (AMM 71-00-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-00-03
ALL ú ú C01 Page 209 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 432-042-C00
(5)
Install the inlet and exhaust covers to prevent fan windmilling and to prevent foreign object damage (FOD).
S 932-130-C00
(6)
Attach a tag to the power plant to show that the fuel system and oil system preservation was done with preservation oil.
(a)
Include the date of the preservation procedure.
TASK 71-00-03-622-043-C00
7. Power Plant Preservation Renewal - Up to 90 Days - Serviceable Power Plant__________________________________________________________________________
A. General
(1)
The procedures in AMM 71-00-03/201 are for engines that are installed on-wing. Procedures for engines that are removed from the airplane are in the CFMI Engine Shop Manual, Section 72-00-00, Page 1201.
B.
Access
(1)
Location Zones
506 Engine No. 1
606 Engine No. 2
C.
Preservation Renewal
S 622-044-C00
(1)
The Preservation Renewal procedure is not permitted.
S 622-045-C00
(2)
You must do the procedure for Power Plant Preservation for 30 to 365 days (serviceable power plant) if the power plant will be kept longer.
TASK 71-00-03-622-046-C00
8. Power Plant Preservation - 30 to 365 Days - Serviceable and Not serviceable___________________________________________________________________________ Power Plant___________
A. General
(1) Do not apply a spray of preservation oil to the inlet, compressor, turbine, or exhaust.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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 动力装置 POWER PLANT 1(153)
