-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
6. On the panel 40VU:
-wait 30 minutes and then release (out) the CTR TK PUMP 2 P/BSW.
7. Calculate the quantity of fuel transferred to the right wing inner cell.
**ON A/C 301-399,
Subtask 28-21-00-710-071-A
B. Operational Leak Test
-
the CTR TK PUMP 2 shows green in-line (pump on).
On the panel 40VU:
-
the CTR TK PUMP 2 P/BSW OFF lightcomes on.
The quantity of fuel transferred in 30minutes must be less than 110 kg (240lb).
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the panel 40VU: - push (in) the R TK PUMPS 1 P/BSW. On the panel 40VU:- the R TK PUMPS 1 P/BSW OFF light goesoff - the R TK PUMPS 1 P/BSW FAULT light comes on momentarily and then goes off.
On the ECAM lower DU:
- the R TK PUMP 1 shows green in-line (pump on).
2. On the panel 40VU: - wait 30 minutes and then release (out) the R TK PUMPS 1 P/BSW. On the panel 40VU:- the R TK PUMPS 1 P/BSW OFF lightcomes on.
3. Calculate the quantity of fuel transferred to the left wing inner cell. The quantity of fuel transferred in 30minutes must be less than 110 kg (240lb).
4. On the panel 40VU: On the panel 40VU:
R 1EFF : ALL 1 28-21-00Page A526 1 1 Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
-make sure all the fuel pump P/BSWs are in the OFF position.
5. On the panel 40VU:
-push (in) the L TK PUMPS 1 P/BSW.
6. On the panel 40VU:
-wait 30 minutes and then release (out) the L TK PUMPS 1 P/BSW.
7. Calculate the quantity of fuel transferred to the right wing inner cell.
**ON A/C ALL
5. Close-up
________
Subtask 28-21-00-860-090
A. Aircraft Configuration
-all pump OFF lights are on.
On the ECAM lower DU:
-
the amber cross-line shows (pump off).
On the panel 40VU:
-
the L TK PUMPS 1 P/BSW OFF light goesoff
-
the L TK PUMPS 1 P/BSW FAULT light comes on momentarily and then goes off.
On the ECAM lower DU:
-
the L TK PUMPS 1 shows green in-line (pump on).
On the panel 40VU:
-
the L TK PUMPS 1 P/BSW OFF lightcomes on.
The quantity of fuel transferred in 30minutes must be less than 110 kg (240lb).
(1)
Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(2)
Refuel, defuel or transfer fuel as necessary (Ref. TASK 12-11-28-650-003), (Ref. TASK 28-25-00-650-001) or (Ref. TASK 28-25-00-869-001).
(3)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
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Subtask 28-21-00-942-084
B. Removal of Equipment
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the safety barriers.
(3)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
R 1EFF : ALL 1 28-21-00Page A528 1 1 Aug 01/05 1 1 1CES 1
MAIN FUEL PUMP SYSTEM - INSPECTION/CHECK
________________________________________ TASK 28-21-00-280-001 Check Suction Valves For Full and Free Movement 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.
1.
Reason for the Job
__________________
Refer to the MPD TASK: 282100-06
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
No specific access platform 3 m (9 ft. 10 in.)
98D57004014000 1 HOOK-COVER (RIB2-SURGE DOORS)
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本文鏈接地址：A320飛機維護手冊 AMM FUEL 燃油3(18)
