Air Conditioning Flashcards
Heat exchanges function to reduce the temperature
Of the hot pneumatic air
Pack outlet air temperature can be modulated downstream of the
Turbine by temperature control valve
If air cycle machine fails, the pack
May be operated in Heat exchanger cooling or bypass mode
Mixer unit is connected to packs, cabin air,
Emergency ram air inlet, low pressure ground connector
Trim air valves optimize temperature by
Adding hot air
Aircraft air conditioning system is controlled by
Two pack controllers, one zone controller
Pack controllers control the pack outlet temperature via
The Ram air heat exchanger inlet / outlet flaps, temperature control valves
Trim air valves are controlled by
Zone controller
Pack airflow is modulated by
Pack flow control valve
FAULT light in PACK for valve disagreement,
Pack outlet overheat, pack compressor overheat
Zone temperature selectors on overhead AIR panel are
Cockpit and cabin
Pack flow control valve closes automatically if
Eng start sequence is initiated, associated engine fire pb switch is pressed, ditching pb on
Cargo ventilating air is received from
Cabin air
Cargo compartment inlet and outlet valves and the extraction fans are controlled by
Cargo ventilation controller
FWR Cargo compartment inlet air can be heated by
Trim air ducted upstream of PACK 1
DITCHING ON cargo compartment isolation valves are closed and
Cargo extract fans stop automatically
Cargo compartment ventilation and heating is controlled by
CARGO ventilation controller, dual channel
Limitations air conditioning – passengers without air condition
20 min max
Prohibited A/C simultaneously from packs and
Low pressure ground units
Air flow by two carts not exceed
2x 1.6 kg/sec
No HP ground unit when
APU bleed air
Packs on APU BLEED airflow automatically on
HI
Temperature selectors available for
Bulk, FWD, cockpit, cabin
Zone temperatures can be monitored on the following ECAM system display pages
COND , CRUISE
High pressure cylinder O2 is in the
Lower left fuselage
A330 has
2 overpressure safety systems O2
CREW SUPPLY overhead controls
Supply solenoid valve
CKPT OXY amber below
300 psi
REGUL LO PR amber ECAM DOOR/OXY if O2 pressure drops to
50psi or lower on the low pressure circuit
If cabin altitude exceeds 35,000 ft mask inlets closes and Pilot breaths
100% O2.