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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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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本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) 動(dòng)力裝置 POWER PLANT 1(148)
