Limitaciones A320/321 NEO y CEO 2025

Max tire speed: 195 kt. 190 kt. 189 kt.

Max operating speed VMO/MMO: 350kt / M 0.82. 330kt / M 0.80. 350kt / M 0.76.

Max Flaps/Slats Speeds a321. Conf 1: 230kt Conf 1+f: 215kt Conf 2: 200kt Conf 3: 185kt Conf full: 177kt. Conf 1: 235kt Conf 1+f: 215kt Conf 2: 200kt Conf 3: 195kt Conf full: 190kt. Conf 1: 235kt Conf 1+f: 225kt Conf 2: 215kt Conf 3: 195kt Conf full: 190kt.

Max speeds with the landing gear extended: 270kt / M 0.64. 250kt / M 0.60. 280kt / M 0.67.

Max speed at which the landind gear may be extended (VLO). 230kt / M 0.58. 250kt / M 0.60. 220kt / M 0.54.

Max speed at which the landind gear may be retracted (VLO retraction): 220kt / M 0.54. 250kt / M 0.60. 280kt / M 0.67.

Minimum control speed for landing (VMCL) A321 NEO: 115kt. 116kt. 109kt.

Max Flaps/Slats Speeds a320. Conf 1: 230kt Conf 1+f: 215kt Conf 2: 200kt Conf 3: 185kt Conf full: 177kt. Conf 1: 230kt Conf 1+f: 215 kt Conf 2: 205kt Conf 3: 195kt Conf full: 185kt. Conf 1: 225kt Conf 1+f: 215kt Conf 2: 195kt Conf 3: 185kt Conf full: 177kt.

Minimum control speed for landing (VMCL) A320 CEO: 116kt. 109kt. 115kt.

Minimum control speed for landing (VMCL) A320 NEO: 115kt. 109kt. 116kt.

Minimum control speed for landing (VMCL) A321 CEO: 115kt. 114kt. 116kt.

Wipers max operating speed: 230kt. 220kt. 200kt.

Max taxi weight A320 CEO: 77,400kg. 77,000kg. 77,200kg.

Max takeoff weight A320 CEO: 79,000kg. 76,000kg. 77,000kg.

Max landing weight A320 CEO: 62,500kg. 66,000kg. 67,400kg.

Maximum zero fuel weight A320 CEO: 62,500kg. 66,000kg. 63,500kg.

Min weight A320 CEO: 40,000kg. 37,000kg. 37,230kg.

Max taxi weight A320 NEO: 79,400kg. 78,000kg. 77,400kg.

Max takeoff weight A320 NEO: 77,000kg. 78,000kg. 79,000kg.

Max landing weight A320 NEO: 66,000kg. 67,400kg. 68,000kg.

Min weight A320 NEO: 40,300kg. 37,230kg. 40,000kg.

Max taxi weight A321 NEO: 93,900kg. 92,000kg. 93,500kg.

Max takeoff weight A321 NEO: 93,500kg. 93,000kg. 91,000kg.

Max landing weight A321 NEO: 77,400kg. 79,000kg. 79,200kg.

Max zero fuel weight A321 NEO: 75,600kg. 75,000kg. 77,000kg.

Min weight A321 NEO: 46,300kg. 46,000kg. 47,000kg.

Max positive differential pressure: 9.0 PSI. 8.6 PSI. 9.6 PSI.

Max negative differential pressure: -1.0 PSI. -2.0 PSI. 1.0 PSI.

Safety relief valve setting: 8.0 PSI. 8.6 PSI. 9.0 PSI.

Outflow valve closure: 14,100ft. 15,000ft. 14,000ft.

Max cabin alt selection: 16,000ft. 14,000ft. 14,100ft.

Can Alt Warning: 9,550ft +-350ft. 10,000ft +-400ft. 9,300ft +-350ft.

Max norm cab alt: 8,500ft. 7,900ft. 8,000ft.

Min cabin alt selection: 1,000ft. -1,000ft. -2,000ft.

Autopilot function at takeoff: 100 ft. 200 ft and 5 seconds. 50 ft and no time.

Autopilot function in app with FINAL APP, V/S or FPA mode: 200ft. 250ft. 500ft.

Autopilot function in circling approach: 250ft. 600ft. 500ft.

Autopilot function with ILS CAT 1. At the minima for the app. 200ft. 160ft.

Autopilot function after a manual go-around: 150ft. 200ft. 100ft.

After three consecutive APU start attempts how much time may the crew must wait before a new start attempt: 30min. 45min. 60min.

What’s the APU max N speed: 161%. 150%. 107%.

Maximum EGT for APU start below 35,000ft. 1090 Celsius. 1120 Celsius. 1200 Celsius.

Max EGT for APU start above 35,000: 1130 Celsius. 1090 Celsius. 1120 Celsius.

Max EGT for APU running: 675 Celsius. 1120 Celsius. 635 Celsius.

What’s the APU battery restart limit: 22,500ft. 25,000ft. 15,000ft.

Between which altitude would you have only electrical power from the APU?. 25,000 and 39,800 ft. 20,000 and 39,800 ft. 22,500 and 41,000 ft.

Between which altitude would the APU be able to supply Bleed air and Elec power to the aircraft: -2000 and 22,500 ft. -1000 and 25,000 ft. 0 and 39,800 ft.

Max altitude for the APU BLEED to assist engine start: 20,000 ft. 22,500 ft. 25,000 ft.

Max altitude for air conditioning and pressurization single pack operation: 15,000 ft. 25,000 ft. 22,500 ft.

Max altitude for air conditioning and pressurization dual pack operation. 22,500 ft. 15,000 ft. 20,000 ft.

Flight maneuvering load acceleration limits clean configuration... 0 g to 2.0g. -1g to +2.5g. -1g to +2.0g.

Flight maneuvering load acceleration limits other configurations... 0 g to +2g. -1g to +2g. 0g to +2.5g.

Max runway altitude... 15,000ft. 14,000 ft. 14,100 ft.

Maximum demonstrated crosswind (takeoff and landing)... 30 kt. 38 kt gust included. 40 kt.

Maximum wind for passenger door operation: 65 kt. 45 kt. 50 kt.

Maximum wind for FWD and AFT cargo door operation: 45 kt (or 50 kt if the aircraft nose is into the wind or if the FWD and AFT cargo doors are on the leeward side). 40 kt (or 60 kt if the aircraft nose is into the wind or if the FWD and AFT cargo doors are on the leeward side). 40 kt (or 50 kt if the aircraft nose is into the wind or if the FWD and AFT cargo doors are on the leeward side).

Maximum crosswind for takeoff and landing (gust included) with braking action good to medium (4): 38 kt. 29 kt. 30 kt.

Maximum crosswind for takeoff and landing (gust included) with braking action good (5): 38 kt. 35 kt. 40 kt.

Maximum crosswind for takeoff and landing (gust included) with braking action medium (3): 29 kt. 25 kt. 30 kt.

Maximum crosswind for takeoff and landing (gust included) with braking action medium to poor (2): 29 kt. 25 kt. 20 kt.

Maximum crosswind for takeoff and landing (gust included) with braking action poor (1): 15 kt. 20 kt. 10 kt.

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

Maximum Flaps/Slats speeds a321 NX. 1 243 kt 1+F 225 kt 2 215 kt 3 195 kt FULL 186 kt. 1 243 kt 1+F 225 kt 2 215 kt 3 190 kt FULL 186 kt. 1 234 kt 1+F 225 kt 2 210 kt 3 190 kt FULL 186 kt.

During preliminary cockpit preparation if battery voltage below 25.5 how much time of charging cycle is required?. 30 min. 20 min. 10 min.

If the aircraft hasn´t been electrically supplied for ____ hrs or more you must have to do the check for battery voltage?. 6 hrs. 5 hrs. 3 hrs.

Having more than 25.5 V on batteries, how much percentage of charge is ensured?. 50%. 40%. 60%.

If the APU is started on batteries only, it must be started within how long after the selection batteries to auto?. 30 min. 40 min. 15 min.

What would be the percentage of battery charge after battery selection to AUTO after 35 minutes?. Less than 50% of its maximum capacity. Less than 30% of its maximum capacity. Less than 25% of its maximum capacity.

What´s the full range temperature of the cockpit and cabin rotary selectors?. 26 +- 8 celsius. 24 +- 6 celsius. 18 +- 6 celsius.

(NEO) Time and thrust setting limitation in TOGA all engines operative: 5 min and 1083 C EGT. 10 min and 1083 C EGT. 5 min and 1043 C EGT.

(NEO) Time and thrust setting limitation in TOGA one engine inoperative: 10 min and 1043 C EGT. 10 min and 1083 C EGT. 5 min and 1083 C EGT.

(NEO) Time and thrust setting limitation in MCT: Not limited on time and 1083 C EGT. 10 min and 1043 C EGT. Not limited on time and 1043 C EGT.

(NEO) EGT limitation at starting on ground and in flight: 1090 C EGT. 1043 C EGT. 1083 C EGT.

(NEO) Maximum oil temperature: 150 c. 151 c. 140 c.

(NEO) Minimum starting oil temperature: -40 c. -10 c. 52 c.

(NEO) Minimum oil temperature before takeoff: -10 c. 50 c. 52 c.

(NEO) Minimum oil quantity with OAT at or above -30ºC. 14 qt. 15 qt. 16.5 qt.

(NEO) Minimum oil quantity with OAT below -30ºC. 16.5 qt. 14 qt. 16 qt.

(NEO) Minimum oil pressure: 62 PSI. 65 PSI. 50 PSI.

(NEO) Maximum oil pressure: 275 PSI. 260 PSI. 270 PSI.

(NEO) Regarding the starter: what is considered to be one cycle: A standard automatic start that includes up to two start attempts. A standard automatic start that includes one start attempt. A standard automatic start that includes up to three start attempts.

(NEO) For ground starts (automatic or manual) how much time is required between successive cycles: 35 s pause. 40 s pause. 1 min pause.

(NEO) For how long of cooling period and after how many subsequent of failed cycles is required for the starter: A 15 min subsequent to three failed cycles. A 10 min subsequent to four failed cycles. A 15 min subsequent to two failed cycles.

(NEO) How much time of continuous or cumulated crank is required subsequent to three failed cycles: 60 min. 15 min. 10 min.

(NEO) The starter must not be run when N2 is above: 15 %. 20 %. 18 %.

(NEO) The engine is able to start in crosswind up to: 35 kt. 38 kt. 30 kt.

The use of GA SOFT mode is prohibited with one engine inoperative: True. False.

(NEO) Minimum and maximum fuel temperature JET A: -36ºc and 55ºc. -34ºc and 55ºc. -30ºc and 52ºc.

Maximum altitude Flaps/Slats extended: 20 000 ft. 25 000 ft. 15 000 ft.

Minimum fuel quantity for takeoff: 1,500 kg. 1,000 kg. 1,800 kg.

Maximum brake temperature for takeoff (brake fans off). 300°C. 150°C. 350°C.

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

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

Maximum NWS angle with tire(s) deflated (not damaged): 30°. 45°. 25°.

Runway Slope (mean): +-2%. +-1%. +-3%.

Minimal runway width: 45m. 30m. 60m.

Nominal runway width: 45m. 30m. 60m.

Maximum tailwind for takeoff: 15 kt. 10 kt. 18 kt.

Maximum tailwind for landing: 20 kt. 10 kt. 15 kt.

Autopilot function during ILS approach when CAT II or CAT III single or CAT III dual displayed on the FMA: 0 ft AGL if autoland. 80 ft AGL. 160 ft AGL.

Minimum decision height ILS CAT II: 50 ft. 100 ft. NO DH.

ILS CAT II approach, for manual landing, AP should be disconnected no later than: 160 ft AGL. 100 ft AGL. 80 ft AGL.

Minimum decision height ILS CAT III Fail Passive (single): 100 ft. 50 ft. NO DH.

One engine inoperative approach CAT II and CAT III fail passive autoland, are approved in config 3 and Full if engine-out procedures are completed before reaching 1000 ft in approach. False. True.

Maximum headwind for ILS CAT II or CAT III: 30 kt. 15 kt. 20 kt.

Maximum tailwind for ILS CAT II or CAT III: 15 kt. 10 kt. 20 kt.

Maximum crosswind for ILS CAT II or CAT III: 15 kt (or 10 kt with OEI). 30 kt (or 20 kt with OEI). 20 kt (or 15 kt with OEI).

Automatic landing is demonstrated with a glide slope between: -2.0° and -3.35°. -2.5° and -3.15°. -2.5° and -3.45°.

Alert height ILS CAT III Fail Operational (Dual): 50 ft. 100 ft. 20 ft.

Automatic landing is demonstrated with an airport elevation at or below: 8,500 ft. 14,100 ft. 9,200 ft.

(CEO) Time and EGT limit with thrust setting in TOGA all engines operative: 10 min and 635 °C. 5 min and 635 °C. 10 min and 675 °C.

(CEO) Time and EGT limit with thrust setting in TOGA one engine inoperative: 10 min and 675 °C. 5 min and 635 °C. 10 min and 635 °C.

(CEO) Time and EGT limit with MCT: 10 min and 610 °C. Not limited on time and 610 °C. Not limited on time and 635 °C.

(CEO) EGT limit starting on ground or in flight: 610 °C. 635 °C. 1083 °C.

(CEO) Oil maximum continuous temperature: 151 °C. 165 °C. 155 °C.

(CEO) Oil maximum transient temperature (15 min): 165 °C. 155 °C. 151 °C.

(CEO) Oil minimum starting temperature: 50 °C. -40 °C. -10 °C.

(CEO) Oil minimum temperature before IDLE is exceeded: -10 °C. -40 °C. 50 °C.

(CEO) Oil minimum temperature before takeoff: -10 °C. 52 °C. 50 °C.

(CEO) Minimum oil pressure: 65 PSI. 60 PSI. 270 PSI.