S 864-043

 (3)  
Put the applicable ENGINE BLEED switch to the OPEN position.

 S 794-050

 (4)  
Do method 1 or method 2 to apply pressurized air to the temperature sensor.

 (a)  
METHOD 1; Dry motor the applicable engine (AMM 71-00-00/201).

 (b)  
METHOD 2; Pressurize the pneumatic system upstream of the PRSOV (AMM 36-00-00/201).

 S 794-051
 (5)  
Examine the installation of the sensor for leakage.

 S 864-047

 (6)
Release the pressure in the pneumatic system (AMM 36-00-00/201).

 S 364-046

 (7)  
If there is leakage, you must repair the cause.

 S 744-044

 (8)  
Access the CMCS Existing Faults (AMM 45-10-00/201).

 (a)  
Make sure there are no applicable faults.

 G. Put the Airplane to Its Usual Condition
 S 414-021
 (1)  
For the applicable engine, install the access door that follows for the mid-lower forward strut (AMM 54-62-00/201).

 (a)  
452DR

 (b)  
462DR

 (c)  
472DR

 (d)  
482DR

 (2)
Remove electrical power if it is not necessary (AMM 24-22-00/201).

 S 864-023
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 36-22-02
 ALL  ú ú 02 Page 406 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.