-
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.
WARNING : DO NOT GET AIRCRAFT FUEL:
_______
-
IN YOUR MOUTH
-
IN YOUR EYES
-ON YOUR SKIN FOR A LONG TIME.
AIRCRAFT FUEL IS POISONOUS.
WARNING : YOU MUST USE THE NECESSARY PRECAUTIONS TO PREVENT INJURY FROM HEAT.
_______ THE LOCATION FOR THIS TASK CAN BE VERY HOT.
1. Reason for the Job
__________________
Refer to the MPD TASK: 282100-07
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 safety barriers
No specific warning notice
No specific access platform 1.5 m (4 ft. 11 in.)
1EFF : ALL 1 28-20-00Page 401 1 1 Nov 01/04 1 1 1CES 1 B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-012 Material No. 19-010
C. Expendable Parts
USA VV-P-236 PURE MINERALVASELINE OR PETRO- LATUM (Ref. 20-31-00)USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
-------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ------------------------------------ |IPC-CSN----------------------------------
10 O-rings 28-21-06 01 -100
13 O-rings 28-21-06 01 -170
14 O-rings 28-21-06 01 -070
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-912-002 Electrical Bonding of Components With Conductive Bolts and Screws in the Tanks
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
28-00-00-910-001 28-21-00-790-002 31-60-00-860-001 Fuel Safety ProceduresVisual Check of Pipes, Couplings and LP Valve External to Tank From Front Spar to HP Valve For Leaks With Booster Pump On and LP Valve OpenEIS Start Procedure
31-60-00-860-002 71-00-00-710-002 73-11-10-000-004 EIS Stop ProcedureWet Motoring CheckRemoval of the Fuel Filter Element
73-11-10-400-004 Installation of the Fuel Filter Element
78-30-00-040-040 78-30-00-440-040 Deactivation of the Thrust Reverser SystemReactivation of Thrust Reverser
28-20-00-991-001 Fig. 401
1EFF : ALL 1 28-20-00Page 402 1 1 Nov 01/04 1 1 1CES 1
3. Job Set-up
__________ Subtask 28-20-00-941-050
A. Safety Precautions
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
(1)
Put the safety barriers in position.
(2)
You must obey the fuel safety procedures when you do work on the fuel system (Ref. TASK 28-00-00-910-001).
Subtask 28-20-00-860-050
B. Aircraft Maintenance Configuration
(1)
Deactivate the thrust reverser system (Ref. TASK 78-30-00-040-040).
(2)
Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
(3)
Put a warning notice in position to tell persons not to energize the FADEC 1(2).
(4)
Use external power to energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(5)
Do the EIS start procedure (ECAM only) (Ref. TASK 31-60-00-860-001), then: - on the ECAM control panel (CP), push in the FUEL pushbutton switch
(P/BSW)
-make sure that the engine LP valves are shown closed (amber cross-line) on the ECAM lower display unit (DU).
Subtask 28-20-00-865-050
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FUEL/LP VALVE/MOT1/ENG2 2QG A09
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