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ENGINE FIRE PROTECTION: FIRE DETECTION LOGIC - DETECTION FAULT WARNING
TMUFIAA01-P03 LEVEL 3
EFFECTIVITY 26-12-00 Page 7
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 26 FIRE PROTECTION
UF94200
EFFECTIVITY Page 17
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TMUFIAA01 LEVEL 3
EFFECTIVITY 26-12-00 Page 8
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 26 FIRE PROTECTION
UF94200
EFFECTIVITY Page 18
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26 - FIRE PROTECTION
26-12-00 ENGINE FIRE PROTECTION - FIRE
PUSHBUTTON INTERFACES
CONTENTS:
General
Monitoring Interfaces
Supply Interfaces
Self Examination
TMUFIRH01 LEVEL 3
EFFECTIVITY 26-12-00 Page 1
Jun 30/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 26 FIRE PROTECTION
UF94200
EFFECTIVITY Page 19
ALL
ENGINE FIRE PROTECTION - FIRE PUSHBUTTON INTERFACES
GENERAL
During the engine fire procedure, the ENGINE FIRE
PUSHbutton is manually released out. This triggers
several automatic sequences simplifying further crew
actions and system monitoring.
MONITORING INTERFACES
Releasing the fire pushbutton out, cancels the
Continuous Repetitive Chime, signals the action to the
Flight Warning Computer (FWC) for further management
of other warnings and messages and illuminates the
SQUIB light on the Engine Fire Control panel.
SUPPLY INTERFACES
Quick isolation of all systems on the related engine
which could be the origin of the fire or feed the fire
is achieved as soon as the fire pushbutton is released
out. These systems are:
- Fuel.
- Air.
- Electric Power.
- Hydraulic Power.
The electric supply to the Engine Interface (EIU) is
also disconnected.
TMUFIRH01-T01 LEVEL 3
EFFECTIVITY 26-12-00 Page 2
Jun 30/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 26 FIRE PROTECTION
UF94200
EFFECTIVITY Page 20
ALL
ENGINE FIRE PROTECTION - FIRE PUSHBUTTON INTERFACES
TMUFIRH01-P01 LEVEL 3
EFFECTIVITY 26-12-00 Page 3
Jun 30/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 26 FIRE PROTECTION
UF94200
EFFECTIVITY Page 21
ALL
SELF EXAMINATION
When the ENG FIRE PUSHbutton is released out, which
corresponding fire valves are closed?
A - Fuel crossfeed valve.
B - LP fuel and hydraulic fire Shut Off
Valves.
C - HP fuel Shut Off Valve.
When the ENG FIRE PUSHbutton is released out, are
the bleed and the pack valves closed?
A - Yes.
B - No.
When the ENG FIRE PUSHbutton is released out, what
happens to the electrical generation?
A - IDG de-energized.
B - IDG disconnect.
C - IDG energized.
TMUFIRH01 LEVEL 3
EFFECTIVITY 26-12-00 Page 4
Jun 30/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 26 FIRE PROTECTION
UF94200
EFFECTIVITY Page 22
ALL
26 - FIRE PROTECTION
26-12-00 ENGINE FIRE PROTECTION
CONTENTS:
System Warnings
TMUFIR404 LEVEL 3
EFFECTIVITY 26-12-00 Page 1
Jan 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 26 FIRE PROTECTION
UF94200
EFFECTIVITY Page 23
ALL
ENGINE FIRE PROTECTION
SYSTEM WARNINGS
When an engine fire is detected, the continuous
repetitive chime sounds, the MASTER WARNING flashes,
the ENGINE FIRE PUSHbutton light and the FIRE light
on the ENGINE start panel come on.
ENGINE FIRE appears on the Engine Warning display.
TMUFIR404-T01 LEVEL 3
EFFECTIVITY 26-12-00 Page 2
Jan 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 26 FIRE PROTECTION
UF94200
EFFECTIVITY Page 24
ALL
ENGINE FIRE PROTECTION - SYSTEM WARNINGS
TMUFIR404-P01 LEVEL 3
EFFECTIVITY 26-12-00 Page 3
Jan 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 26 FIRE PROTECTION
UF94200
EFFECTIVITY Page 25
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TMUFIR404 LEVEL 3
EFFECTIVITY 26-12-00 Page 4
Jan 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 26 FIRE PROTECTION
UF94200
EFFECTIVITY Page 26
ALL
26 - FIRE PROTECTION
26-12-00 ENGINE FIRE PROTECTION - SYSTEM
OPERATION IN CASE OF ENGINE FIRE
 
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