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Dec 31/95
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 35 OXYGEN
UF94200
EFFECTIVITY Page 97
ALL
CABIN PORTABLE OXYGEN EQUIPMENT
DESCRIPTION/OPERATION
FIRST AID MASK
The continuous-flow first aid oxygen mask provides
oxygen for therapeutic purposes.
The flexible supply hose connects the mask to the
calibrated continuous flow outlet of the bottle.
TMUOXYP02-T02 LEVEL 3
EFFECTIVITY 35-32-00 Page 4
Dec 31/95
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 35 OXYGEN
UF94200
EFFECTIVITY Page 98
ALL
CABIN PORTABLE OXYGEN EQUIPMENT DESCRIPTION/OPERATION
TMUOXYP02-P02 LEVEL 3
EFFECTIVITY 35-32-00 Page 5
Dec 31/95
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 35 OXYGEN
UF94200
EFFECTIVITY Page 99
ALL
CABIN PORTABLE OXYGEN EQUIPMENT
DESCRIPTION/OPERATION
SMOKE HOOD SYSTEM
The smoke hood system provides breathing means and
eyes protection for one user in case of emergency:
fire, or an emission of smoke and/or noxious gases.
It permits him to move freely.
The smoke hood container is provided with a
good-condition indicator and a tamper seal for the
pre-flight inspection.
The annular container in the hood, full of compressed
oxygen, releases the amount of oxygen that the user
needs.
The gas circulation is generated when the user breathes
in and out.
TMUOXYP02-T03 LEVEL 3
EFFECTIVITY 35-32-00 Page 6
Dec 31/95
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 35 OXYGEN
UF94200
EFFECTIVITY Page 100
ALL
TMUOXYP02-P03 LEVEL 3
CABIN PORTABLE OXYGEN EQUIPMENT DESCRIPTION/OPERATION
EFFECTIVITY 35-32-00 Page 7
Dec 31/95
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 35 OXYGEN
UF94200
EFFECTIVITY Page 101
ALL
THIS PAGE INTENTIONALLY LEFT BLANK
TMUOXYP02 LEVEL 3
EFFECTIVITY 35-32-00 Page 8
Dec 31/95
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 35 OXYGEN
UF94200
EFFECTIVITY Page 102
ALL
35 - OXYGEN
35-11-41 OXYGEN CYLINDER -
REMOVAL/INSTALLATION
CONTENTS:
Precautions
Removal
Installation
TMUOXYI02 LEVEL 3
EFFECTIVITY 35-11-41 Page 1
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 35 OXYGEN
UF94200
EFFECTIVITY Page 103
ALL
OXYGEN CYLINDER
PRECAUTIONS
WARNING :
KEEP ALL HYDROCARBONS (FUEL, LUBRICANTS, ETC...) AWAY
FROM ALL SOURCE OF OXYGEN. OXYGEN BECOMES EXPLOSIVE
WHEN IT TOUCHES HYDROCARBONS.
CLEAN THE TOOLS AND MAKE SURE YOUR HANDS ARE CLEAN TO
PREVENT CONTAMINATION OF THE OXYGEN SYSTEM.
CAUTION :
PUT DRY AND CLEAN, METAL OR PLASTIC PLUGS AN ALL PIPES
OR UNITS REMOVED TEMPORARILY.
PUT EACH PIPE OR UNIT IN A SEALED VINYL BAG.
REMOVAL
Put the access platform in position and open the access
door 812.
The oxygen cylinder has to be removed in case of low
content or leakage. Close the oxygen cylinder ON/OFF
valve.
Energize the aircraft electrical circuits ; make sure
that the avionics equipment ventilation operates
correctly.
Check that the OXYGEN/CREW/OXY/SPLY circuit-breaker
1 HT is closed.
Bleed and empty the oxygen system:
- press the OXYGEN/CREW SUPPLY pushbutton.
- On one of the oxygen masks, actuate the PRESS
TO TEST AND RESET slider several times to empty
the system.
- release the OXYGEN/CREW SUPPLY pushbutton.
- open, safety and tag the OXYGEN/CREW/OXY/SPLY
circuit breaker 1 HT.
Loosen the nut and disconnect the pressure regulator
transmitter assembly from the oxygen cylinder.
Put a blanking cap on the pressure regulator and put
it in a sealed vinyl bag.
Put an oxygen cylinder cap on the cylinder valve.
Disconnect the HP safety hose from the cylinder head ;
discard the sleeve and put a blanking cap on the union.
Put an oxygen cylinder stowage cap on the cylinder
valve.
Loosen the nut and disengage the pin from the clamp
to remove the cylinder from the support.
TMUOXYI02-T01 LEVEL 3
EFFECTIVITY 35-11-41 Page 2
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 35 OXYGEN
UF94200
EFFECTIVITY Page 104
ALL
OXYGEN CYLINDER - REMOVAL
TMUOXYI02-P01 LEVEL 3
EFFECTIVITY 35-11-41 Page 3
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