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(5) PA = 86 bar (1250 psi), T = 11ºC (52ºF)
HA = 125 mm (4.9 in)
DIAGRAM 2
(2) PA = 92 bar (1330 psi), T = 11ºC (52ºF)
HA = 140 mm (5.5 in)
DIAGRAM 3
(3) PA = 92 bar (1330 psi)
TMULDGA06-T07 LEVEL 3
EFFECTIVITY 32-00-00 Page 16
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 334
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PRESSURE/EXTENSION GRAGH - VALUES OF THE FILM
TMULDGA06-P07 LEVEL 3
EFFECTIVITY 32-00-00 Page 17
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TMULDGA06 LEVEL 3
EFFECTIVITY 32-00-00 Page 18
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UF94200
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32 - LANDING GEAR
32-43-00 LOW PRESSURE CIRCUIT FILLING AND
BLEEDING
CONTENTS:
Precautions
Procedure
TMULDGM01 LEVEL 3
EFFECTIVITY 32-43-00 Page 1
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MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
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LOW PRESSURE CIRCUIT FILLING AND BLEEDING
PRECAUTIONS
Aircraft configuration: All safety precautions are
fulfilled (Refer to AMM).
PROCEDURE
- Yellow hydraulic circuit and brake accumulator
are depressurized.
- Use de-aerated hydraulic fluid.
- Disconnect hydraulic hoses from the master
cylinders and connect master cylinders to
hydraulic fluid recovery containers with vinyl
tubing.
- Open bleeder J, bleeder K remains closed.
- Fill the system with the hand pump until the
fluid flows from the vinyl pipe and there are
no air bubbles. Make sure that the supply
pressure is no more than 15 bars (217.6 psi).
- Close the bleeder J, open the bleeder K and
carry out the same procedure.
- Connect hydraulic hoses to the base of the left
and the right master cylinders.
- Connect the vinyl tubing to the reservoir
bleeder (do not unscrew the bleeder).
- Open the bleeders J and K of the dual valve
and continue to fill until the fluid which
flows from the reservoir bleeder is free of
air bubbles.
- Check that the reservoir is full (indicator
fully extended to the stop position).
- Open the reservoir bleeder to adjust the level
of the fluid in the reservoir to normal (the
piston is level with the green band).
- Close the supply valves of the dual valve.
- Close the bleeders on the dual valve and
reservoir.
- With the yellow hydraulic system
pressurized and the pressure of the green
hydraulic system depressurized push in the
pedals and check that the pressure value
shown on the brake yellow pressure triple
indicator is correct.
TMULDGM01-T01 LEVEL 3
EFFECTIVITY 32-43-00 Page 2
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 338
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LOW PRESSURE CIRCUIT FILLING AND BLEEDING
TMULDGM01-P01 LEVEL 3
EFFECTIVITY 32-43-00 Page 3
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32 - LANDING GEAR
32-41-00 WHEEL AND BRAKE
REMOVAL/INSTALLATION
CONTENTS:
MLG Wheel and Brake Removal/Installation
NLG Wheel Removal/Installation
TMULDVV0B LEVEL 2
EFFECTIVITY 32-41-00 Page 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
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WHEEL AND BRAKE REMOVAL/INSTALLATION
MLG WHEEL AND BRAKE REMOVAL/INSTALLATION
GENERAL
This procedure includes removal/installation
operations of the following components/systems:
- brake fan (optional),
- Tire Pressure Indicating System (optional),
- ABS wheel and brake.
Even if your aircraft is not equipped with one or both
optional systems or this type of wheel and brake, the
procedure remains the same.
PREPARATION
Outside,
- make sure that the landing gear safety devices
　
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