-
the CTR TK L XFR (CTR TK R XFR) P/BSW.
If a fault occurs in the main transfer system:
-
the related FAULT annunciator will come on
-
the failure message FUEL L(R) XFR VALVE FAULT will be shown on ECAM.
The FAULT annunciator of the MODE SEL P/BSW will only come on in the AUTO configuration. If the FAULT annunciator of the MODE SEL P/BSW comes on, the P/BSW must be set to MAN. The crew then have manual control of the main transfer system.
The FAULT annunciator of the CTR TK L XFR (CTR TK R XFR) P/BSW can come on in the AUTO or the MAN configuration. If a FAULT annunciator of one of the CTR TK XFR P/BSWs comes on, that P/BSW must be set to OFF.
If one of the CTR TK XFR P/BSWs is set to OFF:
1EFF : 301-399, 1 28-26-00Page 15 1 1 Feb 01/05R 1 1 1CES 1
-fuel will transfer from the center (transfer) tank to one wing tank only
-the crew must crossfeed fuel (Ref. 28-23-00) from one wing tank to the other to keep the aerodynamic balance of the aircraft.
Gravity transfers fuel from the center (transfer) tank if the the two CTR TK XFR P/BSWs are set to OFF. Fuel only gravity transfers to the wing tanks when the level of fuel in the center (transfer) tank is greater than that in the wing tanks. When gravity transfer is in operation, approximately 2000 kg (4400 lb) of unusable fuel will remain in the center (transfer) tank.
(2) SD FUEL page jet pump indications R
(Ref. Fig. 010) R
8. BITE Test
_________
Not applicable
1EFF : 301-399, 1 28-26-00Page 16 1 1 Aug 01/05 1 1 1CES 1
SD FUEL Page Jet Pump Indications
Figure 010
R 1EFF : 301-399, 1 28-26-00 Page 17
1 1 Aug 01/05
1 1
1CES 1
MAIN TRANSFER SYSTEM - ADJUSTMENT/TEST
______________________________________
TASK 28-26-00-710-001
Operational Test of the Main Transfer System
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
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-11-28-650-003 Pressure Refuel with Automatic Control 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 Fuel Safety Procedures 28-25-00-650-001 Pressure Defuel 28-25-00-869-001 Fuel Transfer 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 28-26-00-991-001 Fig. 501
1EFF : 301-399, 1 28-26-00Page 501 1 1 May 01/04 1 1 1CES 1
3. Job Set-up
__________
(Ref. Fig. 501/TASK 28-26-00-991-001) Subtask 28-26-00-941-051
A. Safety Precautions
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
(1) You must obey the fuel safety procedures (Ref. TASK 28-00-00-910-001) when you do work on the fuel system.
(2) Put the safety barriers in position. Subtask 28-26-00-860-050
B. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
Do the EIS start procedure (ECAM only) (Ref. TASK 31-60-00-860-001).
(3)
On the ECAM Control Panel (CP), push (in) the FUEL pushbutton switch (P/BSW).
(4)
Make sure that the FUEL page is shown on the ECAM System Display Unit (SDU).
Subtask 28-26-00-650-050
C. Fuel Configuration
(1)
Refuel each wing tank to approximately 5000 kg (11000 lb) and the center tank to a minimum 3000 kg (6600 lb) (Ref. TASK 12-11-28-650-003).
(2)
On the ECAM SDU:
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