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Apr 31/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 298
ALL
FUEL SYSTEM CONTROLS
TMUFUE302-P01 LEVEL 1
EFFECTIVITY 28-20-00 Page 15
Apr 31/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 299
ALL
PAGE LEFT INTENTIONALLY BLANK
TMUFUE302 LEVEL 1
EFFECTIVITY 28-20-00 Page 16
Apr 31/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 300
ALL
28 - FUEL SYSTEM
28-00-00 FUEL ECAM PAGE PRESENTATION
CONTENTS:
Fuel on Board
Fuel Used
Fuel Quantities
Fuel Temperatures
Engine LP Valves
Tank Pumps
Center Tank Transfer Valves
Crossfeed Valve
APU LP Valve
TMUFUE503 LEVEL 1
EFFECTIVITY 28-00-00 Page 1
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 301
ALL
TMUFUE503-P01 LEVEL 1
FUEL ECAM PAGE PRESENTATION
EFFECTIVITY 28-00-00 Page 2
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 302
ALL
FUEL ECAM PAGE PRESENTATION
TMUFUE503-P02 LEVEL 1
EFFECTIVITY 28-00-00 Page 3
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 303
ALL
FUEL ECAM PAGE PRESENTATION
TMUFUE503-P03 LEVEL 1
EFFECTIVITY 28-00-00 Page 4
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 304
ALL
FUEL ECAM PAGE PRESENTATION
TMUFUE503-P04 LEVEL 1
EFFECTIVITY 28-00-00 Page 5
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 305
ALL
FUEL ECAM PAGE PRESENTATION
TMUFUE503-P05 LEVEL 1
EFFECTIVITY 28-00-00 Page 6
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 306
ALL
FUEL ECAM PAGE PRESENTATION
TMUFUE503-P06 LEVEL 1
EFFECTIVITY 28-00-00 Page 7
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 307
ALL
THIS PAGE INTENTIONALLY LEFT BLANK
TMUFUE503 LEVEL 1
EFFECTIVITY 28-00-00 Page 8
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 308
ALL
28 - FUEL SYSTEM
28-20-00 FUEL FEED SYSTEM OPERATION
CONTENTS:
Auto Mode
- Normal Operation
- Abnormal Operation
Manual Mode
Self Examination
TMUFUE903 LEVEL 1
EFFECTIVITY 28-20-00 Page 1
Jul 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 309
ALL
FUEL FEED SYSTEM OPERATION
AUTO MODE
NORMAL OPERATION:
Aircraft configuration before take-off:
- full load of fuel,
- all 4 wing pumps on,
- CTR TK XFR Valve P/B switches on,
- MODE SEL P/B sw set to AUTO mode.
The CTR TK XFR Valves indications are green when in
closed position on the ECAM.
NOTE: L and R CTR TK XFR Valves control are independent
from each other.
At engine start, the fuel used indication is reset.
The engine identification number changes color from
amber to white at, or above idle.
Engines are supplied directly from the wing tanks.
That is take-off configuration.
TRANSFER SEQUENCE:
Each CTR TK XFR valve is controlled independently by
its adjacent wing tank level sensors (full and
underfull).
When the fuel level in one wing has decreased by 200
kg (underfull level reached), the CTR TK XFR valve is
controlled to open, and is displayed green, in line
on the ECAM.
Fuel is transferred from the center tank to the wing
tank. When the full level is reached, the CTR TK XFR
valve is controlled to close, and is displayed green,
cross line, on the ECAM.
NOTE: This sequence can be initiated on ground
depending upon the fuel level.
The transfer sequence is terminated; the center tank
　
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