A320 LIMITATIONS

Flight maneuvering load acceleration limits for ALL on other configurations is: 0g to +2g. -1g to +2.5g. 0g to +2.5g.

Runway slope limitation for ALL is: +/- 2%. +/- 3%. +/- 4%.

Flight maneuvering load acceleration limits for ALL on clean configuration is: -1 g to +2.5g. 0 g to +2g. -1 g to +2g.

Runway altitude limitation for ALL is: 12 100 ft. 14 100 ft. 14 200 ft.

Nominal runway width limitation for ALL is: 45 m. 30 m. 40 m.

Minimal runway width limitation for ALL is: 45 m. 30 m. 40 m.

Maximum certified crosswind for takeoff on the A320 NEO is: 35 kt (gust included). 38 kt (gust included). 33 kt (gust included).

Maximum demonstrated crosswind for landing on the A319/320 is: 38 kt (gust included). 35 kt (gust included). 36 kt (gust included).

Maximum demonstrated crosswind (Takeoff and Landing) on the A319/320 is: 38 kt (gust included). 35 kt (gust included). 36 kt (gust included).

Maximum tailwind for takeoff for ALL is: 15 kt. 12 kt. 13 kt.

Maximum tailwind for landing for ALL is: 15 kt. 10 kt. 12 kt.

For landing with a tailwind greater than 10 kt on ALL: Use FLAPS FULL only. FLAPS FULL is recommended.

Airport elevation for autoland for all is: 14.100 ft. 9.200 ft. 9.500 ft.

The maximum wind for passenger door operation for ALL is: 65 kt. 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). 50 kt.

The maximum wind for FWD and AFT cargo door operation for ALL is: 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). 50 ft. 65 kt.

The FWD and AFT cargo doors for ALL must be closed before the wind speed exceeds: 65 kt. 50 kt. 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).

Cockpit window open maximum speed for ALL is: 200 kt. 215 kt. 230 kt.

Max speed on cruise for flaps lever position 0 for ALL is: VMO/MMO. 230 kt. 200 kt.

Max speed for flaps 1 is: VMO/MMO. 230 kt. 215 kt.

Max speed on Takeoff for flaps 1 + F is: 230 kt. VMO/MMO. 215 kt.

Max speed on Takeoff/Approach for flaps 2 is: 215 kt. 200 kt. 185 kt.

Max speed for flaps 3 is: 200 kt. 215 kt. 185 kt.

Max speed on flaps FULL is: 185 kt. 177 kt. 200 kt.

Maximum Operating Speed VMO/MMO for ALL is: 350 kt/ M 0.82. 315 kt/ M 0.60. 325 kt/ M 0.77.

Maximum Operating Speed MMO for ALL is: M 0.82. M 0.81. M 0.83.

Maximum speed with the landing gear extended (VLE) for ALL is: 280 kt/ M 0.67. 250 kt/ M 0.60. 220 kt/ M 0.54.

Maximum speed at which the landing gear may be extended (VLO extension) for ALL is: 280 kt/ M 0.67. 250 kt/ M 0.60. 220 kt/ M 0.54.

Maximum speed at which the landing gear may be retracted (VLO retraction) for ALL is: 280 kt/ M 0.67. 250 kt/ M 0.60. 220 kt/ M 0.54.

Maximum tire ground speed for ALL is: 113 kt. 195 kt. 190 kt.

Minimum control speed for landing (VMCL) on the A320 CEO is: 113 kt. 116 kt. 111 kt.

Minimum control speed for landing (VMCL) on the A320 NEO is: 113 kt. 116 kt. 115 kt.

When the takeoff weight is higher than 76 000 kg (167 550 lb), the taxi speed during a turn should not exceed: 20 kt. 18 kt. 15 kt.

Wipers maximum operating speed when the wipers are sweeping for ALL is: 215 kt. 230 kt. 220 kt.

Maximum take off (brake release) weight for the A320 is: 77 000 kg (169 755 lb). 77 400 kg (170 637 lb). 62 500 kg (137 788 lb).

Maximum landing weight for the A320 is: 66 000 kg (145 505 lb). 62 500 kg (137 788 lb). 37 230 kg (82 079 lb).

Maximum take off (brake release) weight for the A320 NEO is: 79 000 kg. 73 900 kg. 77 000 kg.

Maximum landing weight for the A320 NEO is: 67 400 kg. 66 000 kg. 66 300 kg.

Maximum takeoff weight (brake release) for the A319 is: 75 500 kg. 77 000 kg. 77 400 kg.

Maximum landing weight for the A319 is: 66 300 kg. 62 500 kg. 67 400 kg.

With passengers on board, it is not recommended to exceed ____ min without air conditioning supply.

The flight crew must not use bleed air from the ___ and from the HP Air start unit at the same time, to prevent any adverse effect on the Bleed Air System.

Maximum positive differential pressure for ALL is: 9.0 PSI. 8.6 PSI. -1.0 PSI.

Maximum negative differential pressure for ALL is: -1.0 PSI. 9.0 PSI. 8.6 PSI.

Safety relief valve setting for ALL is: 8.6 PSI. 8.7 PSI. 9.0 PSI.

The flight crew must not use conditioned air from the packs and from the ___ Air conditioning unit at the same time, to prevent any adverse effect on the conditioning system.

for ALL, the autopilot at takeoff should be engaged: at 100 ft AGL and at least 5 s after liftoff. at 200 ft AGL and at least 5 s after liftoff. at 250 ft AGL.

For ALL, in a non-precision approach, the autopilot should be disengage: at 200 ft AGL. at 250 ft AGL. at 160 ft AGL.

For ALL, in circling approach, the autopilot should be disengage: at 500 ft AGL for aircraft category C (600 ft AGL for aircraft category D). at 500 ft AGL for aircraft category D (600 ft AGL for aircraft category C). at 500 ft AGL.

For ALL, on ILS/MLS approach when CAT1 is displayed on the FMA, the autopilot should be disengage: at 160 ft AGL. at 200 ft AGL. at 250 ft AGL.

For ALL, on ILS/MLS approach when CAT2 or CAT3 (single or dual) is displayed on the FMA, the autopilot should be disengage: at 0 ft AGL if autoland. at 160 ft AGL. at 200 ft AGL.

For ALL, after a manual go-around, the autopilot should be engaged: at 100 ft AGL. at 200 ft AGL. at 250 ft AGL.

For ALL, if GPS PRIMARY LOST is displayed on the ND and MCDU, the navigation accuracy remains sufficient for RNP operations provided that: the RNP value is checked or entered on the MCDU. the RNP value is checked or entered on the MCDU and HIGH ACCURACY is displayed. HIGH ACCURACY is displayed.

On other fases, the autopilot should be engaged at: 250 ft AGL. 500 ft AGL. 300 ft AGL.

The minimum decision height of an ILS category II, for ALL is: 100 ft. 150 ft. 200 ft.

The minimum decision height of a Special Authorization CAT II, for ALL is: 100 ft. 150 ft. 200 ft.

A320, CAT II and CAT III fail passive Autoland are only approved in configuration ____, and if engine-out procedures are completed before reaching _____ in approach. FULL - 1000 ft. FULL - 1500 ft.

The maximum wind conditions for ILS/MLS CAT II or CAT III and for GLS CAT I, for ALL is: Headwind: 30 kt, Tailwind: 10 kt, Crosswind: 20 kt. Headwind: 30 kt, Tailwind: 10 kt, Crosswind: 10 kt. Headwind: 30 kt, Tailwind: 20 kt, Crosswind: 20 kt.

Automatic can be done with an airport elevation at or below: 9 200 ft. 2 500 ft. 9 100 ft.

Taxi speed in straight line is: 30 kt. 20 kt. 25 kt.

Max Taxi speed turns of more than 90° is: 10 kt. 20 kt. 15 kt.

For ALL, after three consecutive APU start attempts, the flight crew must wait ____ min before a new start attempt.

The APU maximum N rotor speed, for ALL, is: 107 %. 105 %. 106 %.

maximum EGT for APU start (below 35 000 ft), for 2328-2575,5056-8096 is: 1 090 C. 1 120 C. 900 C.

maximum EGT for APU start (Above 35 000 ft), for 2328-2575,5057-8096 is: 1 120 C. 1 090 C. 982 C.

maximum EGT for APU running, for 2328-2575,5057-8096 is: 675 C. 682 C. 742 C.

Maximum EGT for APU start (below 25 000 ft), for 3647-4939 is: 900 C. 1 090 C. 982 C.

Maximum EGT for APU start (above 25 000 ft), for 3647-4939 is: 982 C. 900 C. 1 120 C.

Maximum EGT for APU running (with 5 s confirmation for shutdown), for 3647-4939 is: 682 C. 675 C. 700 C.

Maximum EGT for APU running (for immediate shutdown), for 3647-4939 is: 700 C to 742 C. 682 C to 700 C. 682 C to 742 C.

Max altitude to assist engine start, for ALL, is: 20 000 ft. 22 500 ft. 12 000 ft.

Max altitude for air conditioning and pressurization (single pack operation), for 2328-2575,5057-8096 is: 22 500 ft. 15 000 ft. 20 000 ft.

Max altitude for air conditioning and pressurization (dual pack operation), for ALL, is: 15 000 ft. 22 500 ft. 20 000 ft.

APU battery start limit for all is: 25 000 ft. 21 000 ft. 20 000 ft.

Max altitude for air conditioning and pressurization (single pack operation), for 3646-4939 is: 20 000ft. 18 000 ft. 21 000 ft.

The EGT limit for maximum continuous thrust (MCT), for LEAP 1A NEO, is: 1 025 C. 750 C. 875 C.

The EGT limit when starting on ground, for LEAP 1A NEO, is: 750 C. 875 C. 725 C.

The EGT limit when starting in flight, for LEAP 1A NEO, is: 875 C. 915 C. 950 C.

The EGT limit during Takeoff and Go-around with all engines operative, for CFM, is: 950 C. 1 060 C. 915 C.

The EGT limit during Takeoff and Go-around, for LEAP 1A NEO, is: 1 060 C. 1 025 C. 915 C.

The EGT limit for maximum continuous thrust (MCT), for CFM, is: 915 C. 1 025 C. 950 C.

The EGT limit when starting on ground, for the CFM, is: 750 C. 725 C. 875 C.

The EGT limit when starting in flight, for CFM, is: 725 C. 915 C. 875 C.

Maximum Engine N1, for LEAP 1A NEO, is: 101%. 116.5%. 104 %.

Maximum Engine N2, for LEAP 1A NEO, is: 116.5%. 101%. 105%.

Maximum Engine N1, for CFM, is: 104%. 105%. 101%.

Maximum Engine N2, for MSN CFM, is: 105%. 104%. 116.5%.

Maximum Engine oil continuous temperature, for both, is: 140 C. 155 C. 145 C.

Maximum Engine oil transient temperature (15 min), for both, is: 155 C. 140 C. 150 C.

Minimum Engine oil starting temperature, for both, is: -40 C. 19 C. -10 C.

Minimum Engine oil temperature before takeoff, for LEAP 1A NEO, is: 19 C. -10 C. -40 C.

The minimum oil quantity, for the LEAP 1A NEO, is the highest value of: 10.6 qt, or 8.9 qt + estimated consumption. 8.9 qt, or 10.6 qt + estimated consumption. 0.45 qt/h.

The minimum oil pressure, for LEAP 1A NEO, is: 17.4 PSI. 16 PSI. 17.2 PSI.

The maximum oil pressure (when oil temperature is above 50 C), for LEAP 1A NEO, is: 130.5 PSI. 145 PSI. 17 PSI.

The maximum oil pressure (when oil temperature is below 50 C), for LEAP 1A NEO, is: 145 PSI. 130.5 PSI. 150 PSI.

Minimum Engine oil temperature before takeoff, for CFM, is: -10 C. -40 C. -15 C.

Minimum oil quantity, for CFM, is: 9.5 qt + estimated consumption. 8.9 qt + estimated consumption. 10.6 qt + estimated consumption.

A standard automatic start that includes up to three start attempts, is considered.

For the LEAP 1A NEO,For ground starts (automatic or manual), a ___ s pause is required between successive cycles.

For the CFM, For ground starts (automatic or manual), a ___ s pause is required between successive cycles.

For the LEAP 1A NEO, a 15 min cooling period is required, subsequent to ___ failed cycles.

For the CFM, a 15 min cooling period is required, subsequent to ___ failed cycles.

For the LEAP 1A NEO, the starter must not be run when N2 is above ___ %.

For the CFM, the starter must not be run when N2 is above ___ %.

for ALL, selection of the reverse thrust is _______ in flight. prohibited. permitted. should not be used.

for ALL, backing the aircraft with reverse thrust is: not permitted. permitted. should not be used.

Maximum reverse should not be used below ___ kt. Idle reverse is permitted down to aircraft stop.

Takeoff at reduced thrust, so-called as FLEX takeoff, is permitted only if the airplane meets all performance requirements at the takeoff weight, with the operating engines at the thrust available for the flexible temperature (TFLEX). Takeoff at reduce thrust is permitted with any inoperative item affecting the performance only if the associated performance shortfall has been applied to meet the above requirements. True. False.

FLEX takeoff is permitted on contaminated runways. False. True.

For engine start, the engine is able to start in crosswind up to: 45 kt. 35 kt. 30 kt.

Engine crosswind limit at takeoff is: 45 kt (gust included). 35 kt (gust included). 35 kt.

The maximum operating altitude with slats and/or flaps extended, for ALL, is: 20 000 ft. 25 000 ft. 15 000 ft.

The maximum asymmetry allowed at takeoff on the inner tanks (outer tanks balanced) when the tank fuel quantity (heavier tank) is FULL, for ALL, is: 500 kg (1 102 lb). 1 050 kg (2 314 lb). 1 450 kg (3 196 lb).

The maximum asymmetry allowed at takeoff on the outer tanks (inner tanks balanced) for ALL, is: 370 kg (815 lb). 690 kg (1 521lb). 500 kg (1 102 lb).

The maximum asymmetry allowed in flight and at landing on the inner tanks (outer tanks balanced) when the tank fuel quantity (heavier tank) is FULL, for ALL, is: 1 500 kg (3 306 lb). 1 600 kg (3 527 lb). 500 kg (1 1021 lb).

The maximum asymmetry allowed in flight and at landing on the outer tanks, for ALL, is: 690 kg ( 1 521 lb). 370 kg (815 lb). 500 kg (1 102 lb).

The minimum fuel quantity for takeoff, for ALL, is: 1 500 kg (3 307 lb). 1 600 kg (3 527 lb). 1 450 kg ( 3 196 lb).

The maximum brake temperature for takeoff, for ALL, is: 300 C. 200 C. 400 C.

The maximum NWS angle, for ALL, is: +/- 85. +/- 80. +/- 75.

for ALL, If maximum one tire per gear is deflated (consider three gears), the maximum taxi speed during turn is: 7 kt. 3 kt. 6 kt.

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

For ALL, for the nosewheel steering (NWS) angle, the maximum NWS angle is: 30. 35. 40.

Minimum control speed for landing on A319 is: 113 kt. 109 kt. 110 kt.

Oxygen REF temperature in ground is: REF Temperature = (OAT + Cockpit TEMP) / 2. REF Temperature = CAB TEMP (°C) - 10 °C.

Oxygen REF temperature in flight is: REF Temperature = (OAT + Cockpit TEMP) / 2. REF Temperature = CAB TEMP (°C) - 10 °C.

Minimum oil pressure for CFM is: 13 psi. 17 psi. 14 psi.

Max estimated oil consumption for LEAP 1A NEO is: 0.45 qt/hr. 0.30 qt/hr. 0.50 qt/hr.

Averaged estimated oil consumption for CFM is: 0.4 qt/hr. 0.3 qt/hr. 0.5 qt/hr.

Min temperature of JET A1 for all is: -43 c. -41 c.

Max temperature of JET A1 for CFM is: 54 c. 52 c.

Max temperature of JET A1 for LEAP 1A NEO is: 55 c. 53 c.