(d)
Put the APU switch to OFF.
(e)
Stop the APU (MM 49-11-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
21-00-01
ALL ú ú 01 Page 202 ú Jun 20/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
S 422-012
(9)
Install the check valve that you removed from the pneumatic ground connector (AMM 36-11-03/401).
S 862-013
(10)
Start the APU again (AMM 49-11-00/201).
S 862-014
(11)
Set the APU switch to ON.
S 862-015
(12)
Operate the left and right air conditioning packs:
NOTE: this procedure uses the APU bleed air to remove the oil from
____
the air conditioning system.
WARNING: MAKE SURE THERE IS AN EXIT FOR THE CONDITIONED AIR IN THE
_______ AIRPLANE. ACCIDENTAL CABIN PRESSURIZATION CAN CAUSE INJURY TO PERSONS.
(a)
Make sure the pressurization outflow valve is open or a minimum of one passenger entry door is open.
(b)
Set the position of these switches on the overhead P5 panel as follows: 1) L and R PACK switches to STBY-C (or STBY-N) 2) TRIM AIR to ON. 3) L and R RECIRC FAN to ON.
(c)
Let the air conditioning packs operate until the conditioned air in the airplane has no smell of the oil contamination.
(d)
Set the L and R PACK switches of OFF.
S 862-016
(13)
Start the engines and let the engines operate at ground idle speed (AMM 71-00-00/201).
(14)
Set the APU switch to OFF.
S 862-017
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
21-00-01
ALL ú ú 01 Page 203 ú May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
S 862-018
(15) Operate the air conditioning packs:
NOTE: This procedure uses the engine bleed air to remove the oil
____ contamination from the conditioned air in the airplane.
(a)
Set these switches on the overhead P5 panel as follows: 1) L and R PACK switches to STBY-C (or STBY-N) 2) L and R ENG bleed air switch to ON.
(b)
Let the air conditioning packs operate until the conditioned air in the airplane has no smell of the oil contamination.
(c)
Set the L and R PACK switches of OFF.
S 862-019
(16)
Stop the engines (AMM 71-00-00/201).
S 862-020
(17)
Set these switches to OFF on the overhead P5 panel:
(a)
TRIM AIR.
(b)
L and R RECIRC FAN.
S 282-021
(18)
Examine these components for oil contamination:
(a)
Heat exchangers.
(b)
Recirculation air filter.
(c)
Galley vent fan filter.
S 162-022
(19)
Clean the components or replace them if they have too much
contamination.
S 162-023
(20)
Do the procedure again until the conditioned air in the airplane has no smell of the oil contamination.
D.
Put the Airplane Back to its Usual Condition.
(1)
Close the access doors to the air conditioning bays.
S 862-025
(2)
Remove the electrical power if it is not necessary
(AMM 24-22-00/201).
S 412-024
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
21-00-01
ALL ú ú 01 Page 204 ú May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 FAULT ISOLATION/MAINT MANUAL
DISTRIBUTION
COMPONENT SHT 102 FIG. QTY ACCESS/AREA REFERENCE
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：757 AMM 飞机维护手册 空调 AIR CONDITIONING 1(13)
