1EFF : ALL 1 36-11-48Page 442 1 1 Feb 01/05R 1 1 1CES 1
DUCTS - BLEED AIR, WINGS - INSPECTION/CHECK
___________________________________________
TASK 36-11-48-790-001
R Perform Leak Check on Bleed Air Ducting in Wing Area between Bleed Air R Precooler, Wing Anti Ice Valve and Wing/Fuselage Connection
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
CAUTION : DO NOT USE ENGINE POWER WHEN YOU DO A LEAK TEST OF THE WING ANTI-ICE
_______
DUCTS. HOT AIR FROM THE ENGINE CAN CAUSE INJURY.
1. Reason for the Job
__________________
Refer to the MPD TASK: 361148-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific distilled water No specific leak detection solution No specific safety barriers No specific warning notice No specific GAPC 0 to 3.5 bar ( 0 to 51 psi) No specific access platform, adjustable 4.0 m (13 ft. 1 in.) 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 36-11-48Page 601 1201-227, 1May 01/05 1 1 1CES 1
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 19-001 OTH 16/2/38 SWG
WIRE,SS,BRAIDED (Ref. 20-31-00) Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002
24-41-00-862-002
27-80-00-866-004
27-80-00-866-005
31-60-00-860-001
31-60-00-860-002
32-00-00-481-001
36-11-48-000-004
36-11-48-400-004
49-00-00-860-005
49-00-00-860-006
49-00-00-860-008
49-00-00-860-009
R 53-35-11-000-001
R 53-35-11-400-001
R 57-41-37-000-004
R
R
R 57-41-37-000-005
R 57-41-37-000-009
R 57-41-37-400-002
R
R
R 57-41-37-400-005
R 57-41-37-400-009
36-11-48-991-022
36-11-48-991-023
Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerExtending the Slats on the GroundRetracting the Slats on the GroundEIS Start ProcedureEIS Stop ProcedureInstallation of the Safety Devices on the Landing GearsRemoval of the Bleed Air DuctsInstallation of the Bleed Air DuctsAPU Start by External Power (APS 3200)APU Shutdown by External Power (APS 3200)APU Start by External Power (131-9(A))APU Shutdown by External Power (131-9(A)) Removal of the Wing-to-Fuselage Fairings Installation of the Wing-to-Fuselage Fairings Removal of the Pressure-Relief Panels 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB) Removal of the NACA Duct Panel 521BB(621BB) Removal of the Access Panel 521BT(621BT) Installation of the Pressure-Relief Panels 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB) Installation of the NACA Duct Panel 521BB(621BB) Installation of the Access Panel 521BT(621BT)Fig. 601Fig. 602
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 36-11-48Page 602 1201-227, 1May 01/05 1 1 1CES 1
3. Job Set-up
__________
(Ref. Fig. 601/TASK 36-11-48-991-022, 602/TASK 36-11-48-991-023) Subtask 36-11-48-941-056
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Make sure that the ground safety locks are installed on the landing gear (Ref. TASK 32-00-00-481-001).
(3)
Put a warning notice on the panel 115VU, to tell persons not to start the engine(s).
(4)
Put a warning notice on the panel 114VU, to tell persons not to operate the flap/slat controls.
Subtask 36-11-48-860-056
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM PNEUMATIC 气源 1(111)
