6/29/2023 0 Comments Airbus a320 cockpit trainer![]() ![]() All references to altitude relate to Pressure Altitude, unless otherwise noted.Īutoland Autoland is permitted using full flaps only.Īutoland - Maximum Winds Headwind - 25 kts Tailwind - 10 ktsĬrosswind other than CAT II/III - 15 kts Crosswind CAT II/III (AFM) - 10 ktsĪutopilot Engaged - Minimum Altitude After Takeoff/Go-Around - 30' AGL Enroute - 500' AGL Non-Precision Approaches - 50' Below MDA Coupled Approaches - 50' AGL Autoland (One or Two Autopilots) - Touchdown Max continuous load on generator 90 KVA Max continuous load on TRU 200 A Max brake temp for takeoff 300° CĪll references to airspeed or Mach Number relate to Indicated Airspeed or Indicated Mach Number, unless otherwise noted. Max windshield wiper operations speed (VWW) 230 kts. Max window open speed (who is going to open it?) 200 kts. Max taxi speed in turn when greater than 167,550 lbs. AGL Autoland max winds: Tailwind: 10 knots Crosswind other than CAT II/III: 20 knots Headwind: 30 knots Non-memory limits: Max tire speed 195 kts. Autopilot / Autoland After Takeoff (if SRS is indicated) 100 ft. Flaps/Slats Max operating altitude w/ slats and/or flaps extended: 20,000 ft. ![]() Landing Gear Max landing gear extension altitude: 25,000 ft. Minimum Alternate Fuel 1200 Holding Fuel Per Hour 5000 Minimum Hold for Contingencies (AFM Limit) 1000 Minimum for Dispatch (not including taxi fuel) 6800 Taxi Fuel Per Minute (not included in takeoff weight) 25 Minimum Desired Landing Fuel: Ensures sufficient fuel on board at the threshold in a worst case scenario with max fuel quantity indicator error.įuel At Touchdown 400 To Execute Go-Around 800 Fuel Quantity Indicator Error 400 Minimum Desired Landing Fuel (Indicated) 1600 To Execute Go-Around: The required amount of fuel to execute go-around at runway threshold to 1000' AGL, fly a VFR pattern, intercept a 3° glideslope at approx 2 1/2 miles from the runway and continue to landing.įuel Quantity Indicator Error: The maximum design quantity error for all tanks. Landing Fuel - Minimum (Pounds) Fuel At Touchdown: Ensures adequate fuel boost pump coverage during reverse thrust and landing roll. Outer Wing Tanks 3,100 Inner Wing Tanks 25,000 Center Tank 14,900 Total 43,000įuel Imbalance - Maximum Maximum difference between wing tanks for takeoff and landing - 4410 lbs.įuel Temperature Maximum: 54☌ Minimum: -36☌ If fuel temperature is below minimum temp limit, change to a warmer altitude.įuel Usage Takeoff with center tank supplying the engines is prohibited. Use of APU bleed air for wing anti-ice is not permitted. Wing anti-ice is not permitted on the ground (AFM), or in flight when TAT exceeds 10☌.Engine anti-ice must be ON prior to and during descent in icing conditions, including temperatures below -40☌ SAT.Engine anti-ice must be ON during all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise when temperature is below -40☌ SAT.Icing conditions exist on ground: OAT 10° C (50° F) or below Icing conditions exist in flight: TAT 10° C (50° F) or below Ice & Rain Protection Engine anti-ice must be on during all ground and flight operations when icing conditions exist except during climb and cruise when the temperature is below: -40° C SAT. ![]() 82M Max gear extension (VLO): 250 KIAS Max gear retraction (VLO): 220 KIAS Max gear extended (VLE): 280 KIAS /. Speed Limits Max operating speed (VMO): 350 KIAS Max operating speed (MMO). Operation Limits Max 90° crosswind component (including gusts) for Takeoff and Landing: 29 knots Max 90° crosswind component (including gusts) For CAT II/III: 15 knots Limiting tailwind component for takeoff and landing: 10 knots Max operating altitude: 39,000 ft. ![]()
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