A319 Limitations Sept2021 Flashcards
A319 Limitations
FLIGHT MANEUVERING LOAD ACCELERATION LIMITS
Clean configuration…………..-1 g to +2.5 g
Other configurations………….0 g to +2 g
RUNWAY SLOPE
Runway slope (mean)………………… ±2 %
RUNWAY ALTITUDE
Runway altitude……………………..14 100 ft
NOMINAL RUNWAY WIDTH
Nominal runway width……………………45 m
Minimal runway width…………………….30 m
Maximum demonstrated crosswind (takeoff and landing)
38 kt (gust included)
Maximum tailwind for takeoff
15 kt
Maximum tailwind for landing
15 kt
For landing with a tailwind greater than 10 kt
use FLAPS FULL only.
The maximum wind for passenger door operation is
65 kt
The maximum wind for FWD and AFT cargo door operation is
40 kt (or 50 kt, if the aircraft nose is into the wind, or if the FWD and AFT cargo doors are on the leeward side)
The FWD and AFT cargo doors must be closed before the wind speed exceeds
65 kt.
MAXIMUM RECOMMENDED CROSSWIND ON WET AND CONTAMINATED RUNWAYS
Good 38 kt / 38 kt Good to Medium 29 kt / 29 kt Medium 25 kt / 25 kt Medium to Poor 20 kt / 20 kt Poor 15 kt / 15 kt
TAKEOFF LIMITATIONS ON CONTAMINATED RUNWAYS
Takeoff is not recommended on the following runway conditions:
‐ Water on top of Compacted Snow,
‐ Dry Snow or Wet Snow over Ice.
Takeoff is not permitted on the following runway condition:
‐ Wet ice.
COCKPIT WINDOW OPEN MAXIMUM SPEED
200 kt
MAXIMUM FLAPS/SLATS SPEEDS
1 230 kt HOLDING 1 + F 215 kt TAKEOFF 2 200 kt TAKEOFF/APPROACH 3 185 kt TAKEOFF/APPROACH/LANDING FULL 177 kt LANDING
MAXIMUM OPERATING SPEED VMO/MMO
VMO………………………………….350 kt
MMO……………………………….. M 0.82
Maximum speed with the landing gear extended (VLE)
280 kt /M 0.67
Maximum speed at which the landing gear may be extended (VLO extension)
250 kt /M 0.60
Maximum speed at which the landing gear may be retracted (VLO retraction)
220 kt /M 0.54
MAXIMUM TIRE SPEED
Maximum ground speed…………………………195 kt
MINIMUM CONTROL SPEED FOR LANDING (VMCL)
VMCL
109 kt
WIPERS MAXIMUM OPERATING SPEED
Maximum speed…………………………..230 kt
Maximum taxi weight
75 900 kg
Maximum takeoff weight (brake release)
75 500 kg
Maximum landing weight
62 500 kg
Maximum zero fuel weight
58 500 kg
Minimum weight
35 400 kg
With passengers on board, it is not recommended to exceed
20 min without air conditioning supply.
The lack of fresh air supply will significantly reduce the cabin’s air quality.
The flight crew must not use bleed air from the APU BLEED and from the
HP Air Start Unit at the
same time, to prevent any adverse effect on the Bleed Air System.
AVIONICS VENTILATION
OAT ≤ 49 °C
No limitation
AVIONICS VENTILATION
49 °C < OAT ≤ 55 °C
2 h
AVIONICS VENTILATION
55 °C < OAT ≤ 60 °C
1 h
AVIONICS VENTILATION
60 °C < OAT ≤ 64 °C
0.5 h
Maximum positive differential pressure
9.0 PSI
Maximum negative differential pressure
-1.0 PSI
Safety relief valve setting
8.6 PSI
Maximum differential pressure (Δp) and safety valve setting tolerance
± 7 hPa (0.1 PSI).
Outflow valve closure
15000ft
Max cabin Alt selection
14000ft
Cab Alt Warning
9550ft (+/- 350ft)
Max Norm Cab Alt
8000ft
Max Operating Alt
39800ft
The flight crew must not use conditioned air from the packs and from the
LP Air Conditioning Unit at
the same time, to prevent any adverse effect on the Air Conditioning system.