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时间:2011-04-03 11:32来源:蓝天飞行翻译 作者:航空
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SWITCH  BYPASS 
VALVE  COMBUSTION 
OIL PUMP  COOLING  CHAMBER 
FILTER  FAN  COMPRESSOR 
PRESSURE  SECTION  PORT EXHAUST 
REGULATOR 
VALVE  ACCESSORY 
DRIVE  TURBINE 
GEARBOX  SECTION 

PRESSURE PUMP COOLING AIR INLET
OIL PUMP 
VENT LINE 
FOR THE 
TURBINE 
SCAVENGE  BEARING 
PUMP  CAVITY 
VENT LINE FOR 
THE OIL TANK 
LEGEND 
OIL VENT 
OIL RETURN 
OIL TANK  OIL PUMP SUCTION 
SWITCH FOR  OIL PUMP PRESSURE 
THE LOW OIL QUANTITY SCAVENGE PUMP SUCTION 
SCAVENGE PUMP PRESSURE 
APU Lubrication System Flow Diagram 
Figure 2 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 49-91-00
 ALL  ú ú 01 Page 4 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
OIL PUMP - REMOVAL/INSTALLATION
_______________________________
 1.  General
_______
 A.  This procedure gives the tasks to remove and install the oil pump assembly. You must remove the starter motor before you remove the oil pump assembly. The oil pump is installed on the gearbox assembly.
 TASK 49-91-11-004-001
 2.  Oil Pump Removal (Fig. 401)
___________________________
 A.  Standard Tools and Equipment
 (1)  Container - 5.0 U.S. Gallons (18.9 liters) Capacity
 B.  References
 (1)  
AMM 49-41-11/401, Starter Motor

 (2)  
AMM 49-91-11/601, Oil Pump

 (3)  
AMM 49-91-31/301, Oil Tank


 C.  Access
 (1)  
Location Zones
 101 Control Cabin, LH
 205 Electronic Compartment
 703 APU Compartment


 (2)  
Access Panels
 1201 Electronic Equipment Access Door
 3804 APU Cowl Door

 

 D.  Procedure
 S 864-002
 (1)  Set the switch and the circuit breaker:
 (a)  
Set the APU master switch on the P5 forward overhead panel to the OFF position and attach a DO-NOT-OPERATE tag.

 (b)  
Open this circuit breaker and attach a DO-NOT-CLOSE tag. 1) E3-3 Electrical Shelf, APU Control Unit


 S 014-003
 (2)  Open the APU cowl door:
 (a)  
Open the latches for the APU cowl door.

 (b)  
Open the APU cowl door.

 (c)  
Connect the door support rods.


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 49-91-11
 ALL  ú ú 01 Page 401 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES /MAINTENANCE MANUAL ////////////////////////
SEE B
SEE A
FWD
A
TACHOMETER
INLET LINE FOR
GENERATOR
ACCESSORY CONNECTOR THE OIL COOLER
OIL PUMP DRIVE SEE C ASSEMBLY GEARBOX WASHER (3 LOCATIONS)
CONNECTOR CABLE NUTFOR THE OIL (3 LOCATIONS)
TEMPERATURE
SWITCH

INLET LINE FORFWD THE OIL PUMP
STARTER
MOTOR

OIL FILTER
B
Oil Pump Installation Figure 401 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 49-91-11
 ALL  ú ú 01 Page 402 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
ACCESSORY 
DRIVE 
GEARBOX 
PACKINGS 
OIL PUMP 
ASSEMBLY 
INLET LINE FOR 
THE SCAVENGE PUMP 
GEARBOX  OIL 
INLET LINE  FILTER 
PACKING 
NUT 
LOW OIL PRESSURE SWITCH FOR THE OIL  INLET LINE FOR THE COMPRESSOR 
MANIFOLD 
 
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