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: 54C Minimum: -36C 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 10C. Icing conditions exist on ground: OAT 10 C (50 F) or below Icing conditions exist in flight: TAT 10 C (50 F) or belowĮngine 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 -40C SAT.Įngine anti-ice must be ON prior to and during descent in icing conditions, including temperatures below -40C SAT. 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. TAXI 63 TAKEOFF 63 APPROACHES 64 ILS APPROACHES 67 CAT II/III APPROACHES 67 RNAV APPROACHES 68 LDA APPROACHES 69 ASR APPROACHES 69 ENGINE-OUT APPROACHES 70 VISUAL APPROACHES 70 GO AROUND 71 LANDING 71 WINDSHEAR 72 EGPWS 72 A TO Z - ABBREVIATIONS & ACRONYMS 72 FOM STUFF 76 LOGBOOK STUFF 84 LINE FIXES 85 Training Notes by Eric Parks Copyright 1999 - 2001 Eric Parks Used with the expres Permission of ERIC PARKSĪ319 A320 A321 Max Ramp: 167,400 lbs. ICE & RAIN PROTECTION 5 ELECTRICAL X FIRE PROTECTION 16 FUEL 18 PNEUMATICS, AIR CONDITIONING & PRESSURIZATION 21PRESSURIZATION 23 HYDRAULICS, BRAKES & LANDING GEAR 25 FLIGHT CONTROLS 29 INSTRUMENT / NAV / COMM 34 AUTO FLIGHT SYSTEM 42 FMA - FLIGHT MODE ANNUNCIATOR 48 OXYGEN 49 POWERPLANT XX APU 51FMS 52 REROUTES 61