A320-251 Limitations PDF
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This document details the limitations and specifications of the A320-251 aircraft, including operational parameters, cabin pressure, and engine details. It appears to be a technical manual or training guide for aviation professionals.
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CZECH AVIATION TRAINING CENTRE A320 LIMITATIONS...
CZECH AVIATION TRAINING CENTRE A320 LIMITATIONS Page 1 of 1 SAS Connect / A320-251N Revision 0 / 04.04.2024 AIRCRAFT GENERAL AIR BLEED/COND/PRESS/VENT Maximum altitude: Flight Maneuvering and Load Acceleration limits CABIN PRESSURE Assist engine start 20000 ft Clean configuration -1 g to 2.5 g Maximum positive differential pressure 9.0 PSI Air conditioning and pressurization (single pack) 22500 ft Other configurations 0 g to 2 g Maximum negative differencial pressure -1.0 PSI Air conditioning and pressurization (dual pack) 15000 ft Operational parameters Safety relief valve setting 8.6 PSI APU bleed air for wing anti-ice is not permitted Runway Slope +2 % AUTO FLIGHT SYSTEM ENGINES (CFM LEAP-1A26) Runway Altitude 9200 ft Minimum AGL for autopilot use: Thrust Setting/EGT Limits Nominal Runway Width 45 m At take off 100 ft and at least 5 s after lift off Operating Conditions Time Limit EGT Limit Minimal Runway Width 30 m In APCH with FINAL APP, V/S, or FPA 250 ft Normal 5 min Take off and Go-around One engine 1060 oC Maximum Crosswind In circling 500 ft 10 min out Not Take off 35 kt Landing 38 kt ILS when CAT I si displayed on the FMA 160 ft MCT 1025 oC limited ILS when CAT2 or CAT3 SINGLE or DUAL dis- Maximum certified tailwind 0 ft if autoland On ground - 750 oC played on the FMA Starting Take off and landing 15 kt After manual go-around 100 ft In flight - 875 oC Maximum wind for passenger door operation 65 kt All other phases 500 ft OIL Maximum wind FWD and AFT cargo door 40kt (50kt nose into wind) ILS CAT2 manual landing 80 ft Maximum continuous temperature 140 oC Speeds CAT II and CAT III fail passive autoland approved in CONF 3 or FULL Maximum transient temperature 15 min / 155 oC Cockpit window open M 200 kt Maximum wind for ILS CAT II or CAT III Minimum starting temperature -40 oC Maximum Flaps/Slats speeds Headwind 30 kt Minimum temperature before take off 19 oC 10.6 qt or 8.9 qt + est. consumption 1 230 kt Tailwind 10 kt Minimum oil quantity highest of: (max. 0.45 qt/h) 1+F 215 Kt Crosswind 20 (15kt for automatic rollout with OEI) Minimum oil pressure 17.4 PSI 2 200 kt AUTOMATIC LANDING STARTER 60 s pause required between successive 3 185 kt approved in CONF 3 and FULL Ground starts cycles (cycle=max. 3 automatic start ILS CAT I, CAT II and CAT III autoland attempts) FULL 177 kt Glide slope angle -2.5o to 3.25o After three failed cycles 15 min cooling period required VMO 350 kt APU GA SOFT mode is prohibited with OEI MMO 0.82 M After 3 start attempts 60 min before next attempt FLIGHT CONTROLS Maximum speed with L/G extended 280 kt/0.67 M Maximum EGT for start (bellow 35000ft) 1090 oC Max. altitude with slats and/or flaps extended 20000 ft Maximum speed for L/G extension 250 kt/0.60 M Maximum EGT for start (above 35000ft) 1120 oC FUEL Maximum speed for L/G retraction 220 kt/0.54 M APU running 675 oC JET A1 min. temperature -43 oC Maximum tire speed 195 kt APU start or shutdown is permitted during refueling/defueling (see conditions in FCOM) Maximum temperature + 55 oC Wipers maximum speed 230 kt Operation (elec. power) and normal restart limit 41000 ft Minimum fuel quantity for take off 1500 kg Battery start limit 25000 ft LANDING GEAR Maximum brake temperature for take off Brake fans OFF 300 oC Brake fans ON 150 oC