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54 Cards in this Set
- Front
- Back
Wingspans (A319/A320/A321 w/o sharklet) |
111 feet, 10 inches |
|
Wingspans
(A320/A321 with sharklet) |
117 feet, 5 inches |
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Max landing weight A319 |
137,788 lbs |
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Max landing weight A320 (NEO) |
148,591 lbs |
|
Max landing weight A320 (non NEO) |
145,505 lbs |
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Max landing weight A321 |
171,519 lbs |
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Maximum Certified Altitude |
FL398 |
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Runway Slope (Mean) |
+/- 2% |
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Max runway altitude |
9,200’ non NEO 6,000' NEO |
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Nominal runway width |
148’ |
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Max Demonstrated Crosswind (takeoff and landing) |
NEO: Takeoff: 35 kts (gust incl.) Landing: 38 kts (gust incl.) Other: Takeoff: none Landing: 38 knots (gust included) |
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Max tailwind - Takeoff |
15 knots |
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Max tailwind - Landing |
10 knots |
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Max wind for PAX door operation |
65 knots |
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Max Operating Speeds (Vmo/Mmo) |
- Vmo 350 knots |
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Max speed with landing gear extended |
280 kt / M.67 |
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Max landing gear extension (operating) speed (Vlo) |
250 kt / M.60 |
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Max landing gear retraction speed |
220 kt / M.54 |
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Max altitude landing gear may be extended |
25,000 ft |
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Windshield Wiper in Use Max speed |
230 kt |
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Taxi Speed (A320/A320NEO/A321) |
When the taxi weight is higher than 167,550 lb, do not exceed a taxi speed of 20 kt during a turn. (This includes the NEO also.) |
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Air Conditioning With LP Ground Unit |
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 |
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: +9.0 psi (safety valve setting: 8.6 psi) Max negative: -1.0 psi |
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Minimum Height For Use Of Autopilot |
Takeoff with SRS mode - 100 ft AGL |
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Minimum Height For Use Of Autopilot |
Straight-in non-precision approach |
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Minimum Height For Use Of Autopilot |
...is not permitted in approach, unless the FCU altitude is set at or above: |
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When can NAV mode be used in the terminal area? |
NAV mode may be used in the terminal area, provided: |
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Non-Precision Approaches with Engine-Out |
A319/A321 |
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Maximum Wind Conditions for CAT II or CAT III |
- Headwind 30 kt |
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Maximum Wind Conditions for CAT II or CAT III |
• Headwind 30 kt (20kt for NEO) |
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Max altitude with flaps and/or slats extended |
20,000' |
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Maximum Allowed Wing Fuel Imbalance (sharklet and NEO) |
Fuel Imbalance at Takeoff: Inner Tanks (Outer Tanks Balanced) Tank Fuel Quantity (Heavier Tank): Full Maximum Allowed Imbalance: 3,306 lbs |
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Maximum Allowed Wing Fuel Imbalance
N587NK AND N588NK |
Fuel Imbalance in Flight and Landing: Wing Tanks Tank Fuel Quantity (Heavier Tank): Full Maximum Allowed Imbalance: 2,910 lbs |
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Maximum Allowed Wing Fuel Imbalance |
Fuel Imbalance at Takeoff: Wing Tanks Tank Fuel Quantity (Heavier Tank): Full Maximum Allowed Imbalance: 882 lbs |
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Minimum Fuel Quantity for Takeoff |
Minimum Fuel Quantity for Takeoff: 3,307 lb |
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Fuel Temperature |
For Jet A only, if TAT reaches -34°C, monitor ECAM FUEL SD page that fuel temperature remains higher than -36°C. |
|
Max brake temperature for takeoff (brake fans off) |
300°C |
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APU Start Limitations (cycles) |
After 3 starter motor duty cycles, wait 60 min before attempting 3 more cycles. |
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APU Bleed Extraction |
Max altitude with two PACKS operating 15,000 ft |
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Maximum altitude for APU start on battery power |
25,000 ft |
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APU starting |
FL410 |
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Powerplant Time / EGT Limits A319/A320/A321/A320NEO |
A319/A320/A321: No time limit / 635°C EGT A320 NEO: No time limit / 1018°C EGT (NEO) |
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Powerplant Time / EGT Limits |
5 min (10 min if one engine failed). With both engines operating: A319/A320: 635°C A321: 650°C A320 NEO: 1083°C |
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Powerplant Time / EGT Limits A319/A320/A321/A320NEO |
A319/A320/A321: Unlimited / 610°C A320NEO: 1043°C |
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Powerplant A319/A320/A321/A320NEO |
-40°C |
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Powerplant A319/A320/A321 |
-10°C |
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Min oil pressure: A320NEO |
65 PSI |
|
Powerplant |
non NEO: 11 quarts + est. consumption 0.3 qt/hr NEO: 15.5 quarts (what temp?) 16.5 quarts with OAT => -30°C 19.0 quarts with OAT < -30°C + est. consumption of 0.22 qt/h |
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Power plant starter limitations A319/A320/A321 |
3 consecutive cycles: |
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Power plant starter limitations A320NEO |
3 consecutive start attempts, 35 seconds between each cycle. After 3 cycles, or after 15 min of continuous or cumulative cranking: A 15 min cooling is needed before a new start motoring cycle is attempted. No running engagement of the starter, when N2 is above 20% on ground. |
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Reverse Thrust Limitations |
Max reverse should not be used below 70 knots or when airspeed starts to fluctuate. |
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Reduced Thrust Takeoff Limitations |
Takeoff at reduced thrust is not permitted on contaminated runways. |
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Powerplant |
Engine is capable of starting in crosswinds up to 35 knots. |