Limitations Flashcards
**Max Landing Weight **
320: Classic/Sharklet: 145,505 lbs
319: 137,788 lbs
321: 171,519 lbs
Max Zero Fuel Weight
320: Classic/Sharklet: 137,788 lbs
319: 128,970 lbs
321:
Classic/Sharklet: 162,701 lbs
Max field elevation for Autoland
6500 ft
Max FLEX temp for Takeoff
ISA +55°C
Max Certified Altitude
FL398
Turbulent Air Penetration Speeds
- At or below FL150: 250 knots
- FL150-FL310: 275 kts
- Above FL310: .76M
Max runway slope
+- 2%
Max Runway altitude
9,200’
Max Demonstrated Crosswind
38 kts (gust included)
Max Tailwind for takeoff
15 kts
Max Tailwind for landing
10 kts
Max wind speed for passenger door operation
65 kts
Max Landing Gear extended Speed (Vle)
280 kts/M.67
Max Landing Gear Extension (Vlo extend)
250 kts
Max Landing Gear Retraction speed (Vlo retract)
220 kts
Max atitude landing gear can be extended
FL250
Max airspeed windshield wipers can be used
230 kts
Max taxi speed to make a turn considering weight
If weight is greater than 167,550 lbs Max turning speed is 20 kts
Max positive cabin differential
+8.6 psi
Max negative cabin pressure differential
-1.0 psi
Min height for use of autopilot for takeoff in SRS mode
100’ AGL
Min height for use of autopilot for a straight-in non-precision approach
Applicable minimums
Min height for use of autopilot for a circling approach
Applicable minimums -100 ft
Min height for use of autopilot for an ILS approach where CAT 2 or CAT 3 is not displayed on the FMA
160 ft AGL
Min height for use of autopilot for Go-Around (AP or FD engagement)
100 ft AGL
Min height for use of autopilot for all other phases of flight
500 ft AGL
Max Taxi Weight
Classic: 170,637 lbs
Sharklet: 172,842 lbs
319: 167,330 lbs
321:
Classic: 205,911 lbs
Sharklet: 207, 014 lbs
Max Takeoff Weight
Classic: 169,755 lbs
Sharklet: 171,960 lbs
319: 166,448 lbs
321:
Classic: 205,029 lbs
Sharklet: 206,132 lbs
Use of the AP or FD in OPEN DES or DES mode is not permitted in approach, unless the FCU altitude is set at or above
Highest of:
319/320: Minimum or 500 ft
321: Minimum or 900 ft
Max brake temperature for takeoff
300°C
APU starter limit
After 3 starter motor duty cycles, must wait 60 min before attempting 3 more cycles
Max altitude APU bleed air if both PACKs are operating
15,000’
Max altitude for APU bleed if one PACK is operating
FL200
Can APU bleed air be used for wing anti-ice?
No
Max altitude APU can be started using battery power
FL250
Min Oil temperature for starting
-40°C
Min oil temperature before exceeding idle thrust
-10°C
Min oil quantity
11 qts +estimated consumption (~.3 qts/hr)
Engine Starter limits
Cycle 1-2………2 min each
Cycle 3………….1 min
15 second resting period between each attempt
Engine cooling period, following 3 start attempts or 4 minutes of continuous cranking
30 minutes
No running engagement of the starter when
N2 is above
10% on ground; or
18% in flight
Max crosswind for engine start
35 kts
Min speed for Max thrust reverse
70kts
When is a reduced thrust takeoff not permitted?
Contaminated Runway
Nominal Runway Width
148 ft
Note: (A319, A320, A321 Sharklet can operate to runways as narrow as 98 ft when operated in accordance with the “Operations on Narrow Runways” procedure.)
Max crosswind on wet or contaminated runways
Damp/wet: 38 kts
Slush/Dry snow/ wet snow of 1/8”: 29 kts
Compacted snow if OAT at or below -15°C: 29 kts
Dry snow(1/8"-4")/wet snow(1/8"-6/5")/slippery when wet: 25kts Compacted snow OAT above -15°C: 25 kts
Water/Slush(1/8”-1/2”): 20kts
Ice (cold & dry): 15kts
Max Tire Speed
195 kts
Max Cockpit Window Open
200 kts
Air conditioning with LP Ground Unit
Do not use conditioned air simultaneously from PACKS and LP ground unit ( to avoid chattering of non-return valves)
Is the use of autopilot permitted on Non-Precision Approaches with Engine Out?
320: yes
319/321: NO
Air Conditioning with HP Ground Unit
Do not use HP ground unit when the APU is supplying bleed air to avoid bleed system damage
