71-00-02
 ALL  ú ú C01B Page 482F ú Jul 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
Put the Airplane Back To Its Usual Condition
____________________________________________
 Put the Airplane Back To Its Usual Condition

 S 494-077-C00
 (5)  ENGINES WITH THE VIBRATION ISOLATORS FOR THE FORWARD MOUNT/ THRUST REVERSER HINGES; Remove the thrust reverser hold-open rods as follows (Fig. 401):
 (a)  
Remove the ball lock pin that attaches the hold-open rod to the strut compression rod fitting.

 (b)  
Hold the hold-open rod and remove the screws that attach the
 fitting to the thrust reverser compression pad.

 (c)  
Install the cap screws and washers on the hold-open rods.

 S 414-256-C00
 WARNING: OBEY THE INSTRUCTIONS IN THE PROCEDURE TO CLOSE THE THRUST
_______ REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
 (6)  
Close the thrust reversers (AMM 78-31-00/201).

 S 424-080-C00

 (7)  
Install the fan cowl panels (AMM 71-11-02/401).

 NOTE: To make the installation easier, use tapered thread
____
 protectors on the fan cowl attach bolts.

 S 424-081-C00
 (8)  
If removed, install the forward fairing (AMM 54-32-01/401).

 S 864-082-C00

 (9)  
Remove the circuit breaker lockset, and close this circuit breaker:

 (a)  P6-3 Main Power Distribution Panel
 1) SHUTOFF VALVE ENG

 S 864-083-C00
 (10) Do the activation procedure for the leading edge flaps and slats as follows
 NOTE: If you did the deactivation procedure for the leading
____
 edge devices only, do the activation procedure for the
 leading edge devices only (AMM 27-81-00/201).

 (a)  Remove the circuit breaker lockset, and close this circuit
 breaker:
 1) P6-2 Main Power Distribution Panel

 a) FLAP SHUTOFF VALVE
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 71-00-02
 ALL  ú ú C01B Page 482G ú Jul 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
Put the Airplane Back To Its Usual Condition
____________________________________________ Put the Airplane Back To Its Usual Condition
 (b)
Remove the DO-NOT-OPERATE tag from the flap control lever. S 864-084-C00

 (11)
 Remove the DO-NOT-0PERATE tag from the HYD PUMPS ENG switch on the pilots' overhead panel, P5, for the applicable engine.

 S 864-283-C00

 (12)
 Remove the DO-NOT-OPERATE tags from the start levers. S 944-172-C00

 (13)
 Remove all objects from the engine inlet and work area which can go through the engine during an engine operation.

 S 714-085-C00

 (14)
 Test the engine with the Power Plant Test Reference Table, Test number 9 or 10, as applicable (AMM 71-00-00/501).

 CAUTION:_______ DO NOT LEAVE TOOLS OR OTHER OBJECTS IN THE ENGINE INLET.  IF
 THESE OBJECTS GO THROUGH THE ENGINE, DAMAGE TO THE ENGINE CAN
 OCCUR.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 71-00-02
 ALL  ú ú C01B Page 482H ú Jul 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
POWER PLANT (PRESERVATION AND DEPRESERVATION) - MAINTENANCE PRACTICES
_____________________________________________________________________
 1.  General
_______
 A.  This section contains instructions for power plant preservation,
 preservation renewal, and depreservation.

 (1)  
The instructions usually apply to power plants that are installed (on-wing).
　
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