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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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 (b)  
Install the bonding jumper to the electronic speed switch with the washers and nut (AMM 20-10-37/401). 1) You must have a resistance of 0.0025 ohm maximum.

 (c)  
Put the electronic speed switch on the mounting tray.

 (d)  
Install the washers and screws that attach the electronic speed switch to the mounting tray (SWPM 20-20-00). 1) You must have a resistance of 0.01 ohm maximum.

 (e)  
Connect the electrical connector to the electronic speed switch.


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 49-61-22
 ALL  ú ú 08 Page 404 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
S 414-007
 (2)  Close the No. 2 lowered ceiling panel in the aft end of the passenger compartment (AMM 25-21-71/401).
 S 864-008
 (3)  Set the circuit breaker and the switch: (a) Remove the DO-NOT-CLOSE tag and close this circuit breaker: 1) E3-3 Electrical Shelf, APU Control Unit (b) Remove the DO-NOT-OPERATE tag from the APU master switch on the P5 forward overhead panel.
 S 714-009
 (4)  Do an operational test of the electronic speed switch: (a) Start and operate the APU (AMM 49-11-00/201). (b) Let the engine operation become stable. (c) Make sure the engine operates correctly. (d) Do the APU usual shutdown (AMM 49-11-00/201).

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 49-61-22
 ALL  ú ú 07 Page 405 ú Nov 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
COMPRESSOR INLET TEMPERATURE SENSOR - REMOVAL/INSTALLATION
__________________________________________________________
 1.  General_______
 A.  This procedure contains the removal and the installation tasks for the temperature sensor (T2) for the compressor inlet. During this procedure, the sensor is referred to as the inlet temperature sensor.
 B.  The inlet temperature sensor is at the 7:30 position on the compressor plenum. You can get access to the sensor through the APU cowl door.
 TASK 49-61-32-004-001
 2.  Inlet Temperature Sensor Removal (Fig. 401)________________________________
 A.  Access
 (1)  
Location Zones
 101 Flight Compartment, LH
 205 Electronic Compartment
 703 APU Compartment


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

 

 B.  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.


 S 014-004
 CAUTION:_______BE CAREFUL WHEN YOU MOVE THE LOWER SHROUD. DAMAGE TO THE SHROUD DRAIN LINES CAN OCCUR.
 (3)  Remove the lower shroud:
 (a)  
Hold the lower shroud and open the shroud latches.

 (b)  
Remove the lower shroud.


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 49-61-32
 ú ú 02 Page 401 ú Nov 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES /MAINTENANCE MANUAL ////////////////////////

Compressor Inlet Temperature Sensor Installation
Figure 401

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