TASK 49-11-00-862-156
 10. APU System Deactivation (The APU Removed)
_______________________
 A. General
 (1)  
This procedure gives the steps to prepare the airplane for flight without the APU installed.

 (2)  
To prepare the airplane for flight without the APU installed, you must remove the APU and install protective caps, covers and plugs in the upper shroud and exhaust muffler. Also, you must deactivate the air inlet door, APU fuel valve, APU master switch, and open the applicable circuit breakers.

 B. Special Tools and Equipment
 (1)  
G57NB-5 Collar - Circuit Breaker, Nylon Molding Corp., 1617 S. California, Monrovia, CA 91016 (two are necessary)

 (2)  
C49001-1 Tool Kit - APU Deletion. This kit contains these parts:

 (a)  
1 muffler plug assembly

 (b)  
1 dummy plug assembly

 (c)  
1 door lock assembly

 (d)  
2 spacers

 (e)  
1 cover plate

 (f)  
1 tape

 (g)  
3 decals

 (h)  
1 clamp

 (i)  
2 cap assemblies

 (j)  
1 protective cap

 (k)  
3 pressure caps

 (l)  
10 caps

 (3)  
F80136-33 Tool Kit - APU Deletion (optional to the C49001-1 Tool Kit). This kit contains these parts:

 (a)  
1 muffler plug assembly

 (b)  
2 push rod assemblies

 (c)  
1 cover plate

 (d)  
1 duct cap

 (e)  
10 feet of tying braid

 (f)  
1 dummy plug assembly

 (g)  
1 tape

 (h)  
3 decals

 (i)  
4 pressure caps

 (j)  
1 clamp

 (k)  
8 electrical caps

 (l)  
2 electrical plugs

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 49-11-00
 ALL  ú ú 05 Page 227 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES/MAINTENANCE MANUAL ////////////////////////
C. Standard Tools and Equipment
 (1)  Air Source - Dry Compressed, 30 psig (206 kPa) maximum
 D. Consumable Materials
 (1)  
B00715 Solvent - Methyl Ethyl Ketone, TT-M-261

 (2)  
B00666 Solvent - Methyl Propyl Ketone (this is an alternative to Methyl Ethyl Ketone)

 (3)  
G01043 Cloth - Lintfree

 E. References
 (1)  
AMM 49-11-00/401, APU Power Plant

 (2)  
AMM 49-15-00/501, Air Inlet Door

 (3)  
AMM 49-15-31/401, Air Inlet Door Actuator

 F. Access
 (1)  
Location Zones
 101 Control Cabin, LH
 102 Control Cabin, RH
 216 Left Main Wheel Well
 701 Tail Compartment
 703 APU Compartment

 (2)  
Access Panels
 3701 Stabilizer Trim Access Door
 3804 APU Cowl Door

 G. Procedure
 S 032-193
 (1)  
Remove the APU power plant (AMM 49-11-00/401).

 S 862-194

 (2)  
Do the deactivation for the APU fuel valve (Fig. 203):

 NOTE: The APU fuel valve is found in the left main wheel well.
____
 (a)  
Disconnect the electrical connector, D920, for the APU fuel valve.

 (b)  
FOR THE C49001-1 TOOL KIT; Install the cap assembly to the electrical connector and electrical receptacle for the APU fuel valve.

 (c)  
FOR THE F80136-33 TOOL KIT; Do these steps: 1) Install a cap on the electrical connector for the APU fuel

 valve. 2) Tie the electrical harness with the cap chain to the airplane structure with the braid. 3) Install a cap on the electrical receptacle of the APU fuel valve.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 49-11-00
 ALL  ú ú 07 Page 228 ú Jul 12/00
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) AIRBORNE AUXILIARY POWER 1(73)