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37 Cards in this Set
- Front
- Back
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Max tailwind - Takeoff & Landing
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10 knots
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Max Crosswind Component
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29 knots (Allegiant)
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Max takeoff and landing pressure altitude
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9200’
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Max wind for PAX door operation
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65 knots
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Max wind for CARGO door operation
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40 knots
(50 knots if the nose is oriented into the wind) |
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Max wind for PAX or Cargo door operation
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65 knots
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Max speed with flight deck window open
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200 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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Turbulent Air Penetration Speed
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Below 20,000 ft, maintain 250 knots
At or above 20,000 ft, 275 knots until intercepting 0.76 Mach |
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Ground AIR
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Do not use LP ground conditioned air simultaneously with aircraft PACK (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 (starting) air when the APU is supplying bleed air( to avoid bleed system damage)
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Maximum Altitude (Allegiant)
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39,100 feet
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Minimum Altitude For Use Of Autopilot
(Takeoff) |
May not be engaged below 100 feet AGL on Takeoff
(Allegiant) |
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Minimum Altitude For Use Of Autopilot
(Allegiant) On approach |
ILS Autolanding - The Autopilot is certified to remain engaged throughout the autolanding / rollout or automatic go around.
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Precision Approach with Manual Landing
(Allegiant) |
Disconnect the autopilot no lower than 50 feet below the DA
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Non-Precision Approaches
(Allegiant) |
Disconnect the autopilot no lower than 50 feet below the MDA
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Visual Approach (ILS APPR mode not used)
(Allegiant) |
Disconnect the Autopilot no lower than 500 feet HAA
Unless the approach capability of CAT 3 DUAL or CAT 3 single is displayed on the FMA. The autopilot must be Disconnected at 50 feet below the DDA/DA for the approach or 112 feet AGL, which ever is higher. |
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Maximum Allowed Wing Fuel Imbalance
between INNER WING TANKS |
3300 LBS
Fuel must be transferred to comply with these restrictions |
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Maximum Allowed Wing Fuel Imbalance
between OUTER WING TANKS |
1551 LBS
(One Tank empty, one Tank full, provided the total Fuel Quantity in each wing, outer + inner is approximately equal) Fuel must be transferred to comply with these restrictions |
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Center Tank Fuel
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Must not be used on Takeoff
Center Tank fuel must emptied before the wing tank fuel unless the center tank fuel is used as ballast. |
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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 Start Limitations (cycles)
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3 CONSECUTIVE starter motor duty cycles, with 1 minute cooling between attempts. After 3rd attempt, 60 min cooling period must be allowed.
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Max altitude with flaps and/or slats extended
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20,000 feet
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Max altitude with landing gear extended
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25,000 feet
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Landing Gear Tire Speed (A320)
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Ground Speed of 195 knots
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Brake Limits
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Max brake temperature for takeoff 300°C
(brake fans off) |
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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 |
9.5 quarts + est. consumption (~0.5 qt/hr)
Note: at idle, oil indications can decrease by as much as 6 quarts |
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Power plant starter limitations
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4 consecutive cycles NOT TO EXCEED 9 minutes.
Each cycle 2 minutes followed by a 20 second rest. After the 4th cycle, a Cooling period of 15 minutes. No running engagement of the starter when N2 RPM is above 20% |
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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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