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49 Cards in this Set
- Front
- Back
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Max landing weight A319 |
137,788 lbs
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Max landing weight A320
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145,505 lbs
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Max landing weight A321
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171,519 lbs
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Maximum Certified Altitude
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FL398
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Runway Slope (Mean)
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+/- 2%
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Max runway altitude
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9200’
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Nominal runway width
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148’
Note: A319 and A320 can operate to runways as narrow as 98' when using "Narrow Runway Operations". |
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Max Demonstrated Crosswind
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38 knots (gust included)
Note: The maximum demonstrated crosswind value is not an Airplane Flight Manual (AFM) limitation. It is the maximum crosswind condition experienced during the aircraft certification campaign. Airbus recommends that operator should not intentionally operate in crosswinds that exceed this value. |
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Max tailwind - Takeoff
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15 knots
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Max tailwind - Landing
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10 knots
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Max wind for PAX door operation
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65 knots
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Max Operating Speeds (Vmo/Mmo)
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- Vmo 350 knots
- Mmo 0.82 Mach |
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Max speed with landing gear extended
(Vle) |
280 kt / M.67
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Max landing gear extension (operating) speed (Vlo)
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250 kt
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Max landing gear retraction speed
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220 kt
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Max altitude landing gear may be extended
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25,000 ft
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Windshield Wiper in Use Max speed
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230 kt
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Taxi Speed (A320/A321)
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When the taxi weight is higher than 167,550 lb, do not exceed a taxi speed of 20 kt during a turn.
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Air Conditioning With LP Ground Unit
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Do not use conditioned air simultaneously from PACK and LP ground unit (to avoid chattering of non-return valves).
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Air Conditioning With HP Ground Unit
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Do not use HP ground unit when the APU is supplying bleed air to avoid bleed system damage.
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Cabin Pressure
Max positive differential pressure Max negative differential pressure |
+8.6 psi
-1.0 psi |
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Minimum Height For Use Of Autopilot
- Takeoff with SRS mode - Go-Around (AP or FD engagement) - All other phases |
Takeoff with SRS mode - 100 ft AGL
Go-Around (AP or FD engagement) - 100 ft AGL All other phases: - 500 ft AGL (A319/A320) - 900 ft AGL (A321) |
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Minimum Height For Use Of Autopilot
(Approaches) |
Straight-in non-precision approach
- Applicable Minimum Circling Approach - Applicable Circling Minimums minus 100 ft. ILS approach when CAT 2 or CAT 3 is not displayed on the FMA - 160 ft AGL |
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Minimum Height For Use Of Autopilot
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: Minimum or 500 ft (A319/A320) Minimum or 900 ft (A321) |
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When can NAV mode be used in the terminal area?
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NAV mode may be used in the terminal area, provided:
-GPS PRIMARY is available, or -HIGH accuracy is displayed, and the appropriate RNP is checked or entered on the MCDU, or -NAVAID raw data is monitored. |
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Non-Precision Approaches with Engine-Out
(Limitations on AP usage) |
A319/A321
If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs in the following modes: FINAL APP, NAV V/S, NAV/FPA. Only FD use is permitted. A320... no such limitations |
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Maximum Wind Conditions for CAT II or CAT III
Automatic Approach, Landing and Roll Out APPLICABLE TO N502NK THRU N618NK |
- Headwind 30 kt
- Crosswind: CAT I - 20 kt CAT II or III - 15kt (for OpSpec) - Tailwind 10 kt Wind limitation is based on the surface wind reported by ATC. (Not on ND) |
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Maximum Wind Conditions for CAT II or CAT III
Automatic Approach, Landing and Roll Out APPLICABLE TO N619NK AND SUBSEQUENT |
• Headwind 30 kt
• Crosswind - 20 kt for Automatic Approach, Landing (without Automatic Rollout). - 15 kt for Automatic Rollout. Note: - Spirit Airlines is restricted to 15 kt for CAT II or CAT III automatic approaches by Operations Specifications approval. - For automatic landing in CAT I conditions the maximum crosswind component is 20 kt. • Tailwind 10 kt Wind limitation is based on the surface wind reported by ATC. (Not on ND) |
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Max altitude with flaps and/or slats extended
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20,000'
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Maximum Allowed Wing Fuel Imbalance
N619NK AND SUBSEQUENT |
Inner Tanks (Outer Tanks Balanced)
Tank Fuel Quantity (Heavier Tank) Full, Maximum Allowed Imbalance Full 1,102 lbs Outer Tanks (Inner Tanks Balanced): Maximum Allowed Imbalance 815 lbs |
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Maximum Allowed Wing Fuel Imbalance
N587NK, N588NK |
Wing Tanks
Tank Fuel Quantity (Heavier Tank) Full, Maximum Allowed Imbalance 2,910 lbs |
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Fuel Temperature
(Note on Jet A) |
For Jet A only, if TAT reaches -34°C, monitor ECAM FUEL SD page that fuel temperature remains higher than -36°C.
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Minimum Fuel Quantity for Takeoff
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Minimum Fuel Quantity for Takeoff: 3,307 lb
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Max brake temperature for takeoff (brake fans off)
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300°C
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APU Start Limitations (cycles)
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After 3 starter motor duty cycles, wait 60 min before attempting 3 more cycles.
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APU Bleed Extraction
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Max altitude with two PACKS operating 15,000 ft
Max altitude with one PACK operating 20,000 ft Air bleed extraction from the APU for wing and anti-ice is not permitted. |
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Maximum altitude for APU start on battery power
(emergency electrical configuration) |
25,000 ft
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APU starting
(with normal A/C power supply) and operation |
FL410
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Powerplant Time / EGT Limits
Starting |
No time limit / 635°C EGT
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Powerplant Time / EGT Limits
Takeoff and Go-Around A319/A320 |
5 min (10 min if one engine failed) / both 635°C
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Powerplant Time / EGT Limits
Takeoff and Go-Around A321 |
5 min (10 min if one engine failed) / both 650°C
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Powerplant Time / EGT Limits
Maximum Continuous (MCT) |
Unlimited / 610°C
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Powerplant
Min starting oil temp |
-40°C
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Powerplant
Min oil temp prior to exceeding idle |
-10°C
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Powerplant
Min oil quantity |
11qts + est. consumption (~0.3 qt/hr)
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Power plant starter limitations
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3 consecutive cycles:
- 2 cycles of 2 minutes each, - 3rd cycle of 1 minute. Pause between start attempts: 15 seconds. Cooling period, following 3 starts 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. |
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Reverse Thrust Limitations
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Max reverse should not be used < 70 knots or when airspeed starts to fluctuate.
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Reduced Thrust Takeoff Limitations
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Takeoff at reduced thrust is not permitted on contaminated runways.
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Powerplant
Starting Crosswind Operation on Ground |
Engine is capable of starting in crosswinds up to 35 knots.
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