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时间:2011-04-04 10:07来源:蓝天飞行翻译 作者:航空
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(s)  
Remove the pneumatic power if it is not necessary
 (AMM 36-05-00/201).


 (t)  
Remove the electrical power if it is not necessary
 (AMM 24-22-00/201).

 

 S 862-107-C00
 (8)  Start the engine with cross bleed air.
 (a)  
Make sure that engine to be started has been prepared for
 operation.


 (b)  
Make sure the operating engine is at idle.

 (c)  
Do the prestart procedure: 1) Prepare the check sheet to make a record of the engine data during the start and ground run operations.


 2) On the forward overhead panel P5, make sure these switches
 are in the correct position:
 a)  FWD, CTR, and AFT
 FUEL PUMPS switches
 on the Fuel Control Panel
 for the engine to be started -OFF
 b)  L PACK and R PACK
 switches on the
 Pneumatic Control Panel - OFF
 c)  ISOLATION VALVE switch on
 the Pneumatic Control Panel -OPEN
 d)  Applicable
 No.1 or 2 BLEED switch
 on the Pneumatic Control Panel
 for the operating engine -ON
 e)  WING ANTI-ICE switch on
 the Anti-Ice Control Panel -OFF
 f)  Applicable
 No. 1 or 2 ENG ANTI-ICE switch
 on the Anti-Ice Control Panel -OFF
 g)  Applicable HYD PUMPS
 "A" ENG 1 and ELEC 2 or
 "B" ELEC 1 and ENG 2 switches -ON
 3) On the aft overhead panel P5, make sure the applicable
 Engine 1 or 2 PMC switch is ON.
 4)  Make sure the applicable circuit breakers on the circuit breaker panel P6 are closed: a) For Engine No. 1:
 1.  
ENG 1 START VALVE

_

 2.  
ENGINE NO. 1 LEFT IGNITION

_

 3.  
ENGINE NO. 1 RIGHT IGNITION


_
 b)  For Engine No. 2:
 1.  
ENG 2 START VALVE

_

 2.  
ENGINE NO. 2 LEFT IGNITION

_

 3.  
ENGINE NO. 2 RIGHT IGNITION


_
 (d)  Move the thrust lever forward for the operating engine until
 the manifold duct pressure shows 30 psi minimum.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 71-00-00
 ALL  ú ú C11 Page 261 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(e)  
On the forward overhead panel P5, put the FUEL PUMPS FWD and AFT switches for tank numbered same as engine to be started to the ON position. 1) Make sure the two applicable LOW PRESSURE lights go out.

 (f)  
Continue with the usual start procedure.

 (g)  
Decrease the power to idle on the engine used for cross-start after engine being started attains starter cutout speed.

 (h)  
Put the ISOLATION VALVE switch to the AUTO position.


 S 862-108-C00
 (9)  Start the engine with the start valve manual override.
 NOTE: If the start valve electrical circuit becomes inoperative,
____
 the start valve can be opened manually.

 CAUTION: POSITIVE COMMUNICATION BETWEEN THE PERSONS IN THE FLIGHT
_______ COMPARTMENT AND THE GROUND MAINTENANCE PERSONS IS MANDATORY.
 (a)  Make sure you have interphone communication between the persons on the ground and the persons in the flight compartment.
 CAUTION: MANUAL OPERATION OF THE START VALVE WITHOUT AIR PRESSURE
_______
 IN THE INLET DUCT MAY DAMAGE THE VALVE.

 (b)  Do the usual engine start procedure except for these steps:
 WARNING: OBSERVE HAZARD AREAS, PAYING PARTICULAR ATTENTION TO
_______ ENTRY CORRIDOR. ENTRY INTO HAZARD AREA COULD RESULT IN SERIOUS PERSONAL INJURY OR LOSS OF LIFE.
 1)  Move the applicable ENGINE START switch to the GRD position.
 2)  Tell the person on the ground to manually open the start valve. a) Push a 3/8 inch square drive extension through the
 guide port for the start valve manual override (Fig. 209). b) Turn the butterfly valve 90° clockwise to the OPEN position. c) You must keep the valve in the OPEN position.
 
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