R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 36-11-48Page 613 1201-227, 1May 01/05 1 1 1CES 1
R **ON A/C 001-049, 051-061, 101-105, 201-203,
TASK 36-11-48-790-002
Leak Check of Wing Bleed Air on the Pylon to Wing Ducting Flexible Seals and the Wing to Fuselage 'S' Duct
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: 361100-07
2. Job Set-up Information______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) 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.)
R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 36-11-48Page 614 1 1 May 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 Energize the Aircraft Electrical Circuits from the
External Power
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power
27-80-00-866-004 Extending the Slats on the Ground
27-80-00-866-005 Retracting the Slats on the Ground
31-60-00-860-001 EIS Start Procedure
31-60-00-860-002 EIS Stop Procedure
32-00-00-481-001 Installation of the Safety Devices on the Landing
Gears
36-11-48-000-004 Removal of the Bleed Air Ducts
36-11-48-400-004 Installation of the Bleed Air Ducts
49-00-00-860-008 APU Start by External Power (131-9(A))
49-00-00-860-009 APU Shutdown by External Power (131-9(A))
53-35-11-000-001 Removal of the Wing-to-Fuselage Fairings
53-35-11-400-001 Installation of the Wing-to-Fuselage Fairings
36-11-48-991-021 Fig. 603
36-11-48-991-024 Fig. 604
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3. Job Set-up
__________ (Ref. Fig. 603/TASK 36-11-48-991-021, 604/TASK 36-11-48-991-024) Subtask 36-11-48-941-057
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 36-11-48-860-058
B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1)
Fully extend the slats (Ref. TASK 27-80-00-866-004).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the slat/flap control lever.
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