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时间:2011-04-03 11:28来源:蓝天飞行翻译 作者:航空
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IN ONE HOUR STARTS OR TRIES TO START  (STARTER "ON" TIME) OPERATION  (BEFORE YOU TRY TO START AGAIN) COOL DOWN 
1  0-90 SEC (MAX)  0 MINUTES 
2  0-90 SEC (MAX)  5 MINUTES (MIN) 
73  0-90 SEC (MAX)  60 MINUTES (MIN) 


VISUALLY EXAMINE THE BRUSH ASSEMBLIES FOR DISCOLORATION IN THE STARTER AFTER YOU TRY TO START THE APU A THIRD TIME.

-51.1  -40.0  -28.9  -17.8 -6.7  15.6  37.8  60.0 
(-60)  (-40)  (-20)  (0)  (20)  (60)  (100)  (140) 
OUTSIDE AIR TEMPERATURE, `C (`F) 
MAXIMUM TIME TO START 

Operation Limits
Figure 201 (Sheet 4)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. úAIRPLANES WITH THE ETC ú

 49-11-00
 ú ú 01.1 Page 205 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES /MAINTENANCE MANUAL ////////////////////////
TEMP  BAROMETRIC PRESSURE, Hg 
`F  `C  28.00  29.00  30.00 

10 20 50 80 90 100 0 60 70 30 40  -17.8 -12.2 -6.7 -1.1 4.4 10.0 15.6 21.1 26.7 32.2 37.8  42.0 44.0 43.0 41.0 40.0 39.0 38.0 37.0 36.0 35.0 34.0  46.0 45.0 43.0 42.0 41.0 40.0 39.0 38.0 37.0 36.0 35.0  46.0 47.0 45.0 44.0 43.0 42.0 41.0 39.0 38.0 37.0 36.0 

MINIMUM AIR PRESSURE OF THE APU BLEED, PSIG
NO ELECTRICAL LOAD
NO BLEED AIR LOAD

Operation Limits
Figure 201 (Sheet 5)

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 49-11-00
 ALL  ú
 ú  03  Page 206
 ú  Mar 15/91 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(4)  Figure 201A shows the normal operating temperatures for the outside air temperature (OAT) and the APU exhaust gas temperature (EGT) in the fully loaded condition. Figure 201B shows the normal operating temperatures for the outside air temperature (OAT) and the APU exhaust gas temperature (EGT) in the main engine start condition.
 B. Special Tools and Equipment
 (1)  
F80164-35 Screen - Air Inlet

 (2)  
F80164-28 Bolt - Latch


 C. References ú (1) AMM 12-11-00/301, Fuel System
 (2)  AMM 12-33-01/301, Cold Weather Maintenance
 D. Access
 (1)  
Location Zones
 101 Control Cabin, LH
 102 Control Cabin, RH
 205 Electronic Compartment
 215 Left Main Wheel Well


 (2)  
Access Panels
 1101 External Power Receptacle Door
 1201 Electronic Equipment Access Door

 

 E. Procedure ú ú S 862-260 ú         ú
WARNING:_______IF A REFUELING OPERATION IS IN THE AREA, OBEY THE WARNINGS AND ú CAUTIONS IN THE REFUELING PROCEDURE BEFORE YOU DO THE APU START ú AND OPERATION PROCEDURE. IF YOU DO NOT OBEY THE WARNINGS AND ú CAUTIONS, INJURY TO PERSONS CAN OCCUR. ú ú (1) If there is a refueling operation in the area, make sure you obey ú the WARNINGs and CAUTIONs in the refueling procedure ú (AMM 12-11-00/301).
 S 492-216
 (2)  
If you must operate the APU when the service door for the aft galley is open, install the air inlet screen to the airplane (Fig. 202).

 S 712-053

 (3)  
Set the master dim and test switch to TEST to make sure the APU indicator lights on the P5 forward overhead panel operate correctly.

 S 862-054

 (4)  
Make sure these circuit breakers are closed:

 (a)  
E3-3 Electrical Shelf, APU Control Unit

 (b)  
P6-2 Load Control Center Assembly
 1) MASTER WARN & CONT

 

 

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 49-11-00
 ALL  ú ú 01.1 Page 207 ú Jul 12/02
 
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