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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
