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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)  
Remove the DO-NOT-OPERATE tag from the APU master switch on the P5 forward overhead panel.


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 49-71-00
 ALL  ú ú 04 Page 512 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
EXHAUST GAS TEMPERATURE INDICATOR - REMOVAL/INSTALLATION
________________________________________________________
 1.  General
_______
 A.  This procedure contains the removal and installation tasks for the exhaust gas temperature (EGT) indicator. The EGT indicator is installed in the P5 forward overhead panel.
 TASK 49-71-11-004-001
 2.  Exhaust Gas Temperature Indicator Removal (Fig. 401)
_________________________________________
 A.  Access
 (1)  Location Zones
 101 Control Cabin, LH

 B.  Procedure
 S 864-003
 (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 024-006
 (2)  Remove the EGT indicator:
 (a)  
Turn the clamping screw counterclockwise to loosen the EGT indicator.

 (b)  
Pull the EGT indicator out of the panel.

 (c)  
Disconnect the electrical plug from the EGT indicator.


 TASK 49-71-11-404-011
 3.  Exhaust Gas Temperature Indicator Installation (Fig. 401)
______________________________________________
 A.  References
 (1)  AMM 49-11-00/201, APU Power Plant
 B.  Access
 (1)  Location Zones
 101 Control Cabin, LH

 C.  Procedure
 S 424-013
 (1)  Install the EGT indicator:
 (a)  
Connect the electrical plug to the EGT indicator.

 (b)  
Push the EGT indicator into the panel.

 (c)  
Turn the clamping screw clockwise to tighten the EGT indicator.


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 49-71-11
 ALL  ú ú 01 Page 401 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES /MAINTENANCE MANUAL ////////////////////////
SEE A
FLIGHT COMPARTMENT
CLAMPING SCREW
PANEL
ELECTRICAL EXHAUST GAS PLUGTEMPERATURE INDICATOR
A
Exhaust Gas Temperature Indicator Installation
Figure 401

G37890
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 49-71-11
 ALL  ú ú 01 Page 402 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
S 864-016
 (2)  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 914-025
 (3)  Start and operate the APU for a minimum of five minutes (AMM 49-11-00/201).
 S 214-028
 (4)  Look at the EGT indicator. (a) The temperature on the EGT indicator increases and become stable during the APU operation.
 S 914-027
 (5)  Do the APU usual shutdown (AMM 49-11-00/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 49-71-11
 ALL  ú ú 01 Page 403 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
EXHAUST GAS TEMPERATURE THERMOCOUPLE PROBE - REMOVAL/INSTALLATION
 
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