A320 LIMITATIONS

Load acceleration limit in other CONF than clean. 0g - +2g. -1g - +2.5g. -1g - +2g. 0g - +2.5g.

Maximum taxi weight. 77.400 kg. 77.000 kg. 77.200 kg. 64.500 kg.

Maximum takeoff weight. 77.000 kg. 77.400 kg. 64.500 kg. 76.000 kg.

Load acceleration limit in clean configuration. -1g - +2.5g. 0g - +2g. -1g - +2g. 0g - +2.5g.

Maximum landing weight. 64.500 kg. 65.600 kg. 65.500 kg. 64.000 kg.

Maximum ZFW. 61.000 kg. 64.500 kg. 63.000 kg. 65.000 kg.

Minimum weight. 37.230 kg. 37.250 kg. 38.000 kg. 37.500 kg.

Techo de operación. 39.800 ft. 41.000 ft. 40.000 ft. 39.500 ft.

Runway slope. -+2%. -+2.5%. -+1%. -+1.5%.

Minimum runway altitude. -2000 ft. 2000 ft. 1000 ft. -1000 ft.

Maximum runway altitude. 9.200 ft. 9.000 ft. 9.500 ft. 8.500 ft.

Nominal runway width. 45 m. 30 m. 35 m. 48 m.

Minimum runway width. 30 m. 45 m. 35 m. 38 m.

Maximum crosswind. 38 kt. 36 kt. 40 kt. 35 kt.

Maximum tailwind takeoffs and landings. Some MSN 15 kt, Some MSN 10 kt. Some MSN 15 kt, Some MSN 20 kt. Some MSN 10 kt, Some MSN 20 kt. Some MSN 15 kt, Some MSN 19 kt.

Maximum headwind-crosswind-tailwind on an engine out landing. 30 kt - 20kt - 10kt. 10 kt - 20 kt - 30 kt. 30 kt - 38kt - 15 kt. 30 kt - 20 kt - 15 kt.

Maximum wind for PAX door operation. 65 kt. 50 kt. 40 kt. 55 kt.

Maximum wind for cargo door operation. 40 kt (50 kt si la nariz esta enfrentada al viento o la puerta ubicada en sotavento). 40 kt (50 kt si la nariz esta enfrentada al viento o la puerta ubicada en barlovento). 50 kt (40 kt si la nariz esta enfrentada al viento o la puerta ubicada en sotavento). 50 kt (40 kt si la nariz esta enfrentada al viento o la puerta ubicada en barlovento).

Velocidades para turbulencia. Hasta FL200: 250kt / >FL200: 275kt - 0.76M. Hasta FL200: 275kt / >FL200: 250kt - 0.76M. Hasta FL200: 200kt / >FL200: 280kt - 0.76M. Hasta FL200: 250kt / >FL200: 275kt - 0.82M.

NWS maximum angle. 85°. 75°. 80°. 70°.

Maximum NWS angle with rudder. 6°. 15°. 10°. 85°.

Maximum NWS angle with deflated tires. 30°. 75°. 85°. 6°.

Maximum positive differential pressure. 9 PSI. 8 PSI. 8.6 PSI. 9.6 PSI.

Maximum negative differential pressure. -1 PSI. 1 PSI. 0 PSI. -2 PSI.

Safety relief valve setting. 8.6 PSI. 9 PSI. 9.6 PSI. 8 PSI.

Cabin altitude warning. 9.550 ft (+-350 ft). 9.550 ft (+-300 ft). 9.500 ft (+-350 ft). 9.550 ft (+-250 ft).

Maximum normal cabin altitude. 8.000 ft. 8.500 ft. 9.000 ft. 9.550 ft.

Maximum cabin altitude selection. 14.000 ft. 12.000 ft. 13.500 ft. 9.550 ft.

Taxi speed rect line. 30 kt. 25 kt. 10 kt. 20 kt.

I taxi weight >76.000 kg, Maximum taxi speed on turns: 20 kt. 10 kt. 7 kt. 3 kt.

If maximum one tire per gear is deflated (consider three gears) , Maximum taxi speed during turn: 7 kt. 3 kt. 5 kt. 10 kt.

If two tires are deflated on the same main gear (maximum one main gear), Maximum taxi speed: 3 kt. 7 kt. 5 kt. 10 kt.

Maximum operating speed VMO/MMO. 350 kt / 0.82 M. 350 kt / 0.85 M. 360 kt / 0.82 M. 350 kt / 0.80 M.

Maximum tire speed. 195 kt GS. 200 kt IAS. 200 kt GS. 195 kt IAS.

Minimum control speed for landing. 113 kt. 110 kt. 115 kt. 120 kt.

Wipers maximum operating speed. 230 kt. 210 kt. 200 kt. 235 kt.

Cockpit window open maximum speed. 200 kt. 230 kt. 210 kt. 195 kt.

Maximum speed with landing gear extended VLE. 280 kt / 0.67 M. 250 kt / 0.60 M. 220 kt / 0.54 M. 270 kt / 0.67 M.

Maximum speed to extend gear VLO. 250 kt / 0.60 M. 220 kt / 0.54 M. 250 kt / 0.54 M. 220 kt / 0.60 M.

Maximum speed to retract gear VLO. 220 kt / 0.54 M. 250 kt / 0.54 M. 250 kt / 0.60 M. 220 kt / 0.60 M.

Maximum speeds CONF 1 / 1+F / 2 / 3 / FULL. 230 kt / 215 kt / 200 kt / 185 kt / 177 kt. 230 kt / 215 kt / 200 kt / 185 kt / 170 kt. 230 kt / 225 kt / 200 kt / 185 kt / 180 kt. 250 kt / 225 kt / 200 kt / 185 kt / 177 kt.

Maximum altitude flaps/slats extended: 20.000 ft. 22.500 ft. 25.000 ft. 20.500 ft.

Maximum brake temperature. 300° (150° if brake fans on). 150° (300° if brake fans on). 300° (350° if brake fans on). 300° (100° if brake fans on).

Maximum engines N1 and N2. 104% - 105%. 105% - 104%. 104% - 104%. 100% - 105%.

Maximum engine EGT during start. 725°C. 625°C. 675°C. 765°C.

Maximum time and EGT in TOGA. 5 min (10 min 1 ENG out) - 950°C. 10 min (5 min 1 ENG out) - 950°C. No time limitation - 950°C. No time limitation - 915°C.

Maximum time and EGT in MCT. 5 min (10 min 1 ENG out) - 950°C. 10 min (5 min 1 ENG out) - 950°C. No time limitation - 950°C. No time limitation - 915°C.

Maximum speed for MAX reverser. 70 kt. 20 kt. 65 kt. 72 kt.

Dont run the engine starter if N2: >20%. >15%. <20%. <15%.

Maximum oil continuous temperature. 140°C. 155°C. 145°C. 150°C.

Maximum oil transient temperature. 155°C (15 min). 155°C (10 min). 140°C (15 min). 145°C (15 min).

Minimum oil temperature for starting. -40°C. 40°C. -45°C. 45°C.

Minimum oil temperature before takeoff. -10°C. 10°C. -20°C. 20°C.

Minimum oil quantity for flight. 9.5 qt + estimated consumption (0.5 qt/h). 9.5 qt + estimated consumption (0.3 qt/h). 8.5 qt + estimated consumption (0.5 qt/h). 8.5 qt + estimated consumption (0.8 qt/h).

Minimum oil pressure. 13 PSI. 30 PSI. 15 PSI. 20 PSI.

Minimum normal ground oil pressure. 30 PSI. 13 PSI. 15 PSI. 20 PSI.

Maximum normal oil pressure. 90 PSI. 30 PSI. 60 PSI. 70 PSI.

APU maximum N. 107%. 105%. 104%. 100%.

APU maximum EGT for start <FL350. 1090°C. 1120°C. 675°C. 725°C.

APU maximum EGT for start >FL350. 1090°C. 1120°C. 675°C. 725°C.

APU maximum EGT running. 675°C. 725°C. 755°C. 625°C.

APU provides bleed up to: 15.000 ft (dual pack) - 22.500 ft (single pack). 15.000 ft (single pack) - 22.500 ft (dual pack). 15.000 ft (dual pack) - 22.000 ft (single pack). 15.000 ft (dual pack) - 20.000ft (single pack).

APU provides electrical power up to: 39.800 ft. 22.500 ft. 15.000 ft. 25.000 ft.

APU maximum altitude to assist an engine start: 20.000 ft. 25.000 ft. 22.000 ft. 22.500 ft.

Maximum altitude to start APU on batteries. 25.000 ft. 20.000 ft. 22.500 ft. 39.800 ft.

It is permitted to use APU bleed for wing anti ice operation. False. True.

AP connection after takeoff. 100 ft and 5 sec. 100 ft and 3 sec. 150 ft and 3 sec. 250 ft and 5 sec.

AP in approach with FINAL APP, V/S or FPA. 250 ft. 500 ft. 150 ft. 100 ft.

AP in circling approach. 500 ft. 250 ft. 100 ft. 250 ft.

AP ILS CAT 1 FMA. 160 ft. 150 ft. 250 ft. 100 ft.

The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time, to prevent any adverse effect on the Bleed Air System. True. False.

During ground operations and depending on the Outside Air Temperature (OAT), the flight crew must limit the time that the aircraft electric power supply is used. <49°C: No limit / 49°C-55°C: 2h / 55°C-60°C: 1h / 60°C-64°C: 0.5h. <49°C: No limit / 49°C-55°C: 2.5h / 55°C-60°C: 2h / 60°C-64°C: 1h. <49°C: No limit / 49°C-55°C: 2h / 55°C-60°C: 1.5h / 60°C-64°C: 0.5h. <49°C: No limit / 49°C-55°C: 2h / 55°C-60°C: 1h / 60°C-64°C: not allowed.

The flight crew must not use conditioned air from the packs and from the LP Air Conditioning Unit at the same time,. True. False.