_______
SAFE PRESSURE OF 50psi (3.45bar).
(3)
On the refuel/defuel control panel 800VU:
(a)
Make sure that the numbers on the ACTUAL and the FUEL QTY displays increase.
(b)
Monitor the FUEL QTY displays. NOTE : Refer to the fuel tables for the maximum capacity of each
____ fuel tank and for the total fuel capacity (Ref. TASK 12-11-28-650-007).
(c)
When each tank has the correct fuel quantity put its REFUEL VALVE switch to the SHUT position.
(4)
When the fuel tank quantities are correct stop the pump on the fuel tanker/pump unit.
(5)
On the refuel/defuel control panel 800VU:
(a)
Put the MODE SELECT switch to the OFF position and put the guard on the switch.
(b)
Put the applicable REFUEL VALVES switch(es) to the NORM position and put the guard(s) on the switch(es).
(6)
If you have ground power available, make sure that the ECAM lower DU shows the correct fuel quantities.
5. Close-up
________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 12-11-28-860-058
A. Aircraft Configuration
(1)
If you refuelled the aircraft with battery power, on the refuel/defuel control panel (800VU), put the BATT POWER switch to the NORM position.
(2)
Make an entry in the aircraft technical log, to check the fuel configuration before the subsequent flight.
(3)
Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(4)
Disconnect the coupling of the fuel supply-hose from the aircraft refuel/defuel coupling.
(5)
Install the coupling cap. CAUTION : MAKE SURE THAT THE HANDLE OF THE REFUEL COUPLING CAP POINTS
_______ AFT WHEN THE CAP IS CLOSED AND LOCKED.
(6)
Install the refuel coupling cap 41QM.
**ON A/C 301-399,
Subtask 12-11-28-860-058-A
A. Aircraft Configuration
(1)
If you refueled the aircraft with battery power, on the refuel/defuel control panel (800VU), put the BATT POWER switch to the NORM position.
(2)
If you have external power available, do the EIS stop procedure (Ref. TASK 31-60-00-860-002) then de-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
(3)
Disconnect the coupling of the fuel supply-hose from the aircraft refuel/defuel coupling.
(4)
Install the coupling cap. CAUTION : MAKE SURE THAT THE HANDLE OF THE REFUEL COUPLING CAP POINTS
_______
AFT WHEN THE CAP IS CLOSED AND LOCKED.
(5) Install the applicable refuel coupling cap 101QM(41QM). **ON A/C ALL
Subtask 12-11-28-410-052
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Close the access door 192MB. Subtask 12-11-28-942-053
C. Removal of Equipment
(1)
Disconnect these bonding/ground cables:
-between the aircraft and the fuel tanker/pump unit
-
if applicable, between the fuel tanker/pump unit and the ground
-
if applicable, between the aircraft and the ground.
(2)
Remove the safety barriers.
1EFF : ALL 1 12-11-28Page 334 1 1 May 01/05R 1 1 1CES 1
(3)
Remove the warning notice(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 12-11-28Page 335 1 1 May 01/05R 1 1 1CES 1
TASK 12-11-28-650-005
Pressure Refuel without Electrical Power
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
WARNING : STOP THE FUEL TANKER 200 ft. (60 m) FROM THE AIRCRAFT NOSE WHILE THE
_______ WEATHER RADAR OPERATES. DO NOT OPERATE THE FUEL TANKER/PUMP UNIT UNTIL YOU STOP THE OPERATION OF THE WEATHER RADAR.
WARNING : MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START THE
_______ REFUEL/DEFUEL PROCEDURE. IN THE SAFETY AREA, DO NOT:
-SMOKE
-MAKE SPARKS OR FIRE
-USE ANY EQUIPMENT WHICH IS NOT APPROVED FOR REFUEL/DEFUEL
PROCEDURES.
AIRCRAFT FUEL IS FLAMMABLE.
WARNING : DO NOT SPILL FUEL ON THE ENGINES OR THE BRAKES. IF YOU SPILL FUEL ON
_______ ENGINES OR BRAKES THAT ARE HOT, IT CAN CAUSE FIRES.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
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 SERVICING 1(28)