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and supplies oxygen to the crew member in case of
emergency :fire, or an emission of smoke and/or noxious
gases.
The crew smoke hood system allows freedom of movement
to extinguish a fire. It can also be used as an
emergency-oxygen supply if the fixed emergency-oxygen
system does not work.
LOCATION
The smoke hood is vacuum packed in a transport/storage
container.
The crew smoke hoods are installed in the cockpit in
the first officer’s console (702VU).
Smoke hoods for cabin attendants are installed in the
cabin.
TMUOXYQ02-T01 LEVEL 3
EFFECTIVITY 35-31-00 Page 2
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 35 OXYGEN
UF94200
EFFECTIVITY Page 88
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CREW PORTABLE OXYGEN SYSTEM DESCRIPTION AND OPERATION
TMUOXYQ02-P01 LEVEL 3
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 35 OXYGEN
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CREW PORTABLE OXYGEN SYSTEM
DESCRIPTION AND OPERATION
DESCRIPTION
The hood is fire resistant and has an autonomy of 15
minutes.
The container is provided with a good condition
indicator, normally green (red : hood unserviceable),
and a tamper seal used for the preflight inspection.
TMUOXYQ02-T02 LEVEL 3
EFFECTIVITY 35-31-00 Page 4
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 35 OXYGEN
UF94200
EFFECTIVITY Page 90
ALL
CREW PORTABLE OXYGEN SYSTEM DESCRIPTION AND OPERATION
TMUOXYQ02-P02 LEVEL 3
EFFECTIVITY 35-31-00 Page 5
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 35 OXYGEN
UF94200
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CREW PORTABLE OXYGEN SYSTEM
DESCRIPTION AND OPERATION
OPERATION
When doned, the automatic start lever connected to the
annular container, releases the compressed oxygen
stored inside the container.
Then, the oxygen fills up the compartment between the
external and the internal hood.
During inhalation, the oxygen flows to the inner
compartment through the absorption system.
During exhalation, the absorption system traps the
carbon dioxyde contained in the expired gas through a
layer of soda lime.
A pressure control valve prevents an increase of
pressure in the hood.
A phonic membrane allows the user to communicate
easily.
NOTE :
- A slight noise of oxygen flow is heard by
the wearer during operation.
When the noise of oxygen flow stops, the
hood should no longer be used.
TMUOXYQ02-T03 LEVEL 3
EFFECTIVITY 35-31-00 Page 6
Dec 31/95
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 35 OXYGEN
UF94200
EFFECTIVITY Page 92
ALL
CREW PORTABLE OXYGEN SYSTEM DESCRIPTION AND OPERATION
TMUOXYQ02-P03 LEVEL 3
EFFECTIVITY 35-31-00 Page 7
Dec 31/95
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 35 OXYGEN
UF94200
EFFECTIVITY Page 93
ALL
SELF EXAMINATION
What is the function of the hood absorption
system ?
A - To add oxygen to the expired gas.
B - To trap the carbon dioxyde contained in
the expired gas.
C - To allow the expired gas to flow out of
the hood.
TMUOXYQ02 LEVEL 3
EFFECTIVITY 35-31-00 Page 8
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MECHANICS / ELECTRICS & AVIONICS COURSE 35 OXYGEN
UF94200
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35 - OXYGEN
35-32-00 CABIN PORTABLE OXYGEN EQUIPMENT
DESCRIPTION/OPERATION
CONTENTS:
Bottle
First Aid Mask
Smoke Hood System
TMUOXYP02 LEVEL 3
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CABIN PORTABLE OXYGEN EQUIPMENT
DESCRIPTION/OPERATION
BOTTLE
The oxygen source is a high pressure cylinder with a
capacity of 310 liters (11 cubic feet).
The high pressure cylinders are installed in brackets
equipped with quick release clamps.
TMUOXYP02-T01 LEVEL 3
EFFECTIVITY 35-32-00 Page 2
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 35 OXYGEN
UF94200
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ALL
CABIN PORTABLE OXYGEN EQUIPMENT DESCRIPTION/OPERATION
TMUOXYP02-P01 LEVEL 3
EFFECTIVITY 35-32-00 Page 3
　
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