(a) Include the date of preservation procedure.
(12)
Put the start lever back to the CUTOFF position.
S 862-066-C00
(13)
Remove the DO-NOT-CLOSE tag and close this circuit breaker:
S 862-065-C00
(a) P6 Main Power Distribution Panel
1) SHUTOFF VALVE ENG
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-00-03
ALL ú ú C01 Page 225 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TASK 71-00-03-622-067-C00
9. Power Plant Preservation Renewal - 30 to 365 Days - Serviceable and Not_______________________________________________________________________ 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.
Serviceable Power Plant
S 622-068-C00
(1)
Do the preservation procedure for 30 to 365 days (serviceable power plant).
S 622-069-C00
(2)
There is no limit on the number of times you can do this procedure.
D.
Not Serviceable Power Plant
S 622-070-C00
(1)
The Preservation Renewal procedure is not permitted.
(a)
You must do the servicing procedure for the power plant and make the power plant serviceable before the 30 to 365 days preservation time is expired.
TASK 71-00-03-622-071-C00
10. Power Plant Depreservation - 30 to 365 Days - Serviceable Power Plant_____________________________________________________________________
A. General
(1) This procedure gives instructions for the depreservation of an installed power plant that is serviceable. Depreservation includes fluid replacement in the oil and fuel systems.
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71-00-03
ALL ú ú C01 Page 226 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(2)
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.
References
(1)
AMM 12-13-11/301, Engine Servicing
(2)
AMM 71-00-00/201, Power Plant
(3)
AMM 71-00-00/501, Power Plant
C.
Access
(1)
Location Zones
506 Engine No. 1
606 Engine No. 2
D.
Power Plant Depreservation
S 032-072-C00
(1)
Remove the waterproof cover, vapor barrier film, and dessicant.
S 032-073-C00
(2)
Make sure you remove all of the tape from the inlet and exhaust areas and there is no unwanted material.
S 422-074-C00
(3)
Install the accessory units that you removed.
S 432-075-C00
(4)
Connect the lines and electrical connections that you removed.
S 682-076-C00
(5)
Drain the engine oil tank (AMM 12-13-11/301).
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