A319/A320/A321
TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE
28 FUEL SYSTEM
This document must be used for training purpose only
Under no circumstances should this document be used as a reference.
It will not be updated.
All rights reserved.
No part of this manual may be reproduced in any form,
by photostat, microfilm, retrieval system, or any other means,
without the prior written permission of Airbus Industrie.
FUEL GENERAL
** System Design Philosophy (1) .................. 1
** Tank Usable Capacities (1) .................... 5
** ENG and APU Fuel Feed Presentation (1) ...... 11
** System Controls (1) .......................... 15
** Fuel ECAM Page Presentation (1) ............. 19
** System Normal Operation (1) .................. 35
** Fuel System Warnings (3) ..................... 61
STORAGE, VENTING AND RECIRCULATION
** Venting System Description/Operation (3).... 75
** Fuel IDG Cooling System Presentation (3).... 79
** Water Drain Valve Operation (2) ............. 85
** Tank & Venting System Components (3) ........ 89
FUEL DISTRIBUTION
** Engine Feed SYS Description/Operation (3).. 115
** APU Feed System Description/Operation (3).. 121
** Main Fuel Pump System Components (3) ....... 127
** Engine and APU Components (3)............... 151
REFUEL/DEFUEL
** Refuel/Defuel System Presentation (1) ...... 175
** Refuel/Defuel Control Panel (1) ............ 179
** Cockpit Preselector Presentation (1) ....... 185
** Refuel/Defuel System D/O (3)................ 189
** Automatic Refuel Operation (2) ............. 195
** Manual Refuel Operation (2)................. 201
** Defuel Operation (3) ........................ 205
** Fuel Transfer Operation (3)................. 211
** Refuel/Defuel System Components (3) ........ 219
FUEL INDICATING
** Quantity Indicating (3) ..................... 241
** Level Sensing (3)............................ 247
** Manual Measurement (2) ...................... 251
** QTY Indicating SYS Components (3) .......... 261
** Fuel Level Sensing Components (3) .......... 279
FUEL SYSTEM (A321)
** ENG and APU Fuel Feed Presentation (1) ..... 293
** System Controls (1) ......................... 297
** Fuel ECAM Page Presentation (1) ............ 301
** System Normal Operation (1)................. 309
** Fuel Transfer Operation (3)................. 315
** Quantity Indicating (3) ..................... 319
** Level Sensing (3)............................ 325
** QTY Indicating SYS Components (3) .......... 331
MAINTENANCE PRACTICES
SPECIFIC PAGES
** CFDS Specific Page Presentation (3) ...... 343
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY
ALL
28 FUEL SYSTEM
UF94200 TABLE OF CONTENTS Page
28 CONTENTS
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY
ALL
28 FUEL SYSTEM
UF94200 TABLE OF CONTENTS Page
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28 - FUEL SYSTEM
28-00-00 SYSTEM DESIGN PHILOSOPHY
CONTENTS:
General
Feed Concept
Management
Self Examination
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 1
ALL
SYSTEM DESIGN PHILOSOPHY
GENERAL
The fuel system stores fuel in 5 tanks. It supplies
fuel to the engines and APU and recirculates fuel to
cool the oil of the IDGs (Integrated Drive Generators).
A vent surge tank is fitted in each wing.
FEED CONCEPT
Engines are supplied by the center tank fuel via the
center tank pumps.
When the center tank fuel has been used, engines are
supplied by the wing tank pumps, first with the inner
cell fuel and then with the outer cell fuel which flows
to the inner cell.
MANAGEMENT
The different functions of the system are:
- Fuel level and temperature sensing, fuel
transfers, fuel recirculation, refuel/defuel
control and monitoring, indications, warnings
and test.
The fuel quantity indicating system comprises:
- 1 Fuel Quantity Indicating Computer (FQIC).
- 2 Fuel Level Sensor Control Units (FLSCUs).
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
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