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DIMENSIONSPrincipal Dimensions
LIMITATIONSNumber of PassengersOperating WeightsTaxi speed limitAutomatic approach and landing
SYSTEMS (The other systems are the same)Aircraft General ATA 20Autoflight ATA 22Flight Controls ATA 27Fuel ATA 28Hydraulic ATA 29Ice and Rain Protection ATA 30Indicating and recording ATA 31Lights ATA 33Navigation ATA 34Doors ATA 52
PERFORMANCECargo CapacityMagnetic IndicatorsWeight and BalanceSpecial Operations
FLIGHT TECHNIQUES180° turns on a runwayILS Final app and Visual geometryMinimum visual ground segmentsAdverse Weather
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LIMITATIONS
NUMBER OF PASSENGERS
A319A319A320A320
180180 145 145
150 (AVA)150 (AVA) 120 (AVA)120 (AVA)
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WEIGHT LIMITATIONS
Maximum taxi weightMaximum taxi weight 75900 kg 77400 kg
Maximum takeoff weightMaximum takeoff weight 75500 kg 77000 kg
Maximum landing weightMaximum landing weight 62500 kg 66000 kg
Maximum zero fuel weightMaximum zero fuel weight 58500 kg 62500 kg
Minimum weightMinimum weight 35400 kg 37320 kg
A319A319 A320A320
In exceptional cases (in flight turn back or diversion), an immediate landing at weight above maximum landing weight is permitted, provided the pilot follows the overweight landing procedure.
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LIMITATIONS
TAXI SPEED
A319A319 A320A320
When the taxi weight is higher than 76000 kg, do not exceed a taxi speed of 20 kt during a turn.
N/A
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LIMITATIONS
AUTOMATIC APPROACH, LANDING AND ROLL OUT
A319A319
A320A320
ENGINE OUT
CAT II and CAT III fail passive autoland are only approved in configuration 3 and FULL, and if engine-out procedures are completed before reaching 1000 feet in approach.
ENGINE OUT
CAT II and CAT III fail passive autoland are only approved in configuration FULL, and if engine-out procedures are completed before reaching 1000 feet in approach.
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AIRCRAFT GENERAL (ATA 20)
Number of passengers (See Limitations)
Dimensions (See Limitations)
A319A319A320A320
180150 (AVA)
145120 (AVA)
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AIRCRAFT GENERAL (ATA 20)
Ground Maneuvering
A319A319A320A320
Minimum pavement width for 180° turn is:
A319: 21mA320: 23m
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AUTOFLIGHT (ATA 22)
RUDDER TRAVEL LIMITATION (1.22.40)This function limits rudder deflection as a function of speed in order to avoid high structural loads.
A319A319A320A320
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FLIGHTCONTROLS (ATA 27)
SPEEDBRAKES AND GROUND SPOILERS (1.27.10)This function limits rudder deflection as a function of speed in order to avoid high structural loads.
A319A319A320A320The maximum speedbrake deflection in manual flight is:
40° for spoilers 3 and 4
20° for spoiler 2.
The maximum speedbrake deflection with autopilot engaged is:
25° for spoilers 3 and 4
12.5° for spoilers 2.
The maximum speedbrake deflection with autopilot engaged is achieved with half speedbrake deflection.
The maximum speedbrake deflection is:
25° for spoilers 3 and 4
12.5° for spoiler 2 in configuration 3, and 17.5° in other config.
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A319A319A320A320
SYSTEMS
FLIGHTCONTROLS (ATA 27)
RUDDER TRAVEL LIMITATION (1.22.40)This function limits rudder deflection as a function of speed in order to avoid high structural loads.
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FLIGHTCONTROLS (ATA 27)
PITCH CONTROL – FLIGHT MODE (1.27.20)The normal law flight mode is a load-factor-demand mode, with automatic trim and protection throughout the flight envelope.
A319A319A320A320When high speed or high mach protection is active, the THS setting is limited between the setting at the aircrafts entry into this protection and 11° nose-up.
N/A
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FLIGHTCONTROLS (ATA 27)
FLAPS FULL (1.27.50)
A319A319A320A320
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FLIGHTCONTROLS (ATA 27)
WARNINGS AND CAUTIONS (1.27.50)
A319A319A320A320FLAP LVR NOT ZERO
Flap lever is not in the zero position, and the aircraft is above 22000 feet.
N/A
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LIGHTS (ATA 33)
PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM / EXIT SIGNS (1.33.30)
A319A319A320A320
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DOORS (ATA 52)
BULK CARGO DOOR (1.52.10)The bulk cargo door opens inwards and upwards. It is a plug-type door that is mechanically-locked and manually-operated.This door can either be opened from the outside or the inside.
A319A319A320A320
NOT INSTALLED
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CARGO LOADING
CARGO CAPACITYThe maximum load for each compartment is as follows:
A319A319A320A320
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LANDING
FORWARD C.G.
A319A319A320A320
When referring to CG lower than 27%, an operational margin is taken into account. It is the reason why performance at forward CG (lower than 25%) must be used for operational CG lower than 27%.
WEIGHT: -1000 Kg (-600 Kg / abv 7000´ft)
FLEX TEM°: -2°C
SPEEDS: + 1 kT
N/A
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PERFORMANCE
LANDING
CORRECTIONS ON LANDING DISTANCE
Wind : per 10 kt tailwind add 19%.
No correction for headwind due to wind correction on approach speed.
Airport elev : per 1000 ft above sea level add 3%.
Forward CG : add 2%
Wind : per 10 kt tailwind add 19%
No correction for headwind due to wind correction on approach speed.
Airport elev : per 1000 ft above sea level add 3%.
A319A319A320A320
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FLIGHT TECHNIQUES
TAXI
180° TURN ON RUNWAYFor the CM 2, the procedure is symmetrical. (Taxi on the left-hand side of the runway)
A319A319A320A320
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FLIGHT TECHNIQUES
ILS FINAL APPROACH AND LANDING GEOMETRY
A319A319A320A320
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FLIGHT TECHNIQUES
MINIMUM VISUAL GROUND SEGMENTS (Flare phase)
A319A319A320A320