2025 Examen limitaciones Airbus A319/A320 LATAM COLOMBIA

FLIGHT MANEUVERING LOAD LIMITS Clean configuration. -1 g to 2.5 g. 1 g to -2.5 g. -1 g to +2.0 g.

FLIGHT MANEUVERING LOAD LIMITS Other configurations. 0 g to 2 g. -1 g to +2.5 g. 0 g to +2.5 g.

MAXIMUN OPERATION ALTITUD. 39.800 FT. 41.000 FT. 39.000 FT.

MAX ALTITUD FOR FLAPS. 20.000 FT. 25.000 FT. 22.000 FT.

RUNWAY SLOPE. ±2 %. ±3 %. ±2.5 %.

NORMAL RUNWAY WIDTH. 45 m. 40 m. 35 m.

Minimal runway width. 30 m. 35 m. 40 m.

Maximum demonstrated crosswind (takeoff and landing). 38 kt (gust included). 30 kt (gust included). 38 km/h (gust included).

Maximum tailwind for takeoff A320 AND A319. 15 kt & 10Kt. 10 kt & 15Kt. 20 kt & 10Kt.

Maximum headwind for CAT II o III and autoland. 30 kt. 25 kt. 20 kt.

Maximum crosswind for CAT II o III and autoland. 20 kt. 30 kt. 15 kt.

Maximum tailwind for CAT II o III and autoland. 10 kt. 15 kt. 20 kt.

For landing with a tailwind greater than 10 kt. use FLAPS FULL only. use FLAPS 3.

The maximum wind for passenger door operation. 65 kt. 40 kt. 50 kt.

The maximum wind for FWD and AFT cargo door operation. 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). 30 kt (or 40 kt, if the aircraft nose is into the wind, or if the FWD and AFT cargo doors are on the leeward side). 35 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. 200 kt. 220 kt. 320 kt. 200 k/hr.

Max speed flaps 1. 230 kt. 215 kt. 200 kt.

Max speed flaps 1+F. 215 kt. 230 kt. 200 kt.

Max speed flaps 2. 200 kt. 230 kt. 185 kt.

Max speed flaps 3. 185 kt. 200 kt. 177 kt.

Max speed flaps FULL. 177 kt. 185 kt. 200 kt.

MAXIMUM OPERATING SPEED VMO/MMO. 350 kt / M.82. 300 kt / M.80. 350 kt / M.80.

Maximun tire speed. 195 Kt GS. 190 Kt GS. 200 Kt GS.

Maximun Wilnshield wiper use. 230 kt. 320 kt. 200 kt.

Max cockpit window open. 200 kt. 220 kt. 230 kt.

Maximun taxi speed on straight line. 30 kt. 20 kt. 40 kt.

Maximun taxi speed for turns 90º or more. 15 kt. 20 kt. 17 kt.

Max taxi speed for weight above 76.000 kg. Do not exceed a taxi speed of 20 kt during a turn. Do not exceed a taxi speed of 15 kt during a turn. Do not exceed a taxi speed of 25 kt during a turn.

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

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

Maximum taxi weight A319. 75 900 kg. 75 500 kg. 62 500 Kg.

Maximum takeoff weight (brake release) A319. 75.500 kg. 62.500 kg. 77.400 kg.

Maximum landing weight A319. 62.500 kg. 66.000 kg. 62.600 kg.

Maximun zero fuel weight A319. 58.500 kg. 58.000 kg. 35.400 kg.

Maximum taxi weight A320. 77.400 kg. 77.000 kg. 66.000 kg.

Maximum takeoff weight (brake release) A320. 77.000 kg. 66.000 kg. 77.400 kg.

Maximum landing weight A320. 66.000 kg. 77.000 kg. 65.000 kg.

Maximum zero fuel weight A320. 62.500 kg. 62.000 kg. 58.500 kg.

AVIONICS VENTILATION OAT ≤ 49 °C. No limitation. 2 h. 1 h.

AVIONICS VENTILATION 49 °C < OAT ≤ 55 °C. 2 h. 1 h. no limitation.

AVIONICS VENTILATION 55 °C < OAT ≤ 60 °C. 1 h. 2 h. 0.5 h.

AVIONICS VENTILATION 60 °C < OAT ≤ 64 °C. 0.5 h. 1 h. 2 h.

Maximum positive differential pressure. 9.0 PSI. -1.0 PSI. 8.6 PSI.

Maximum negative differential pressure. -1.0 PSI. 9.0 PSI. 8.6 PSI.

Safety relief valve setting. 8.6 PSI. 9.0 PSI. -1.0 PSI.

Altitud cabin warning. 9550 ft (±350 ft). 9500 ft (±350 ft). 9550 ft (±550 ft).

Ram air inlet only open if diff pressure is lower than: 1 psi. 1.5 psi.

Do Not Use Ground Air Simultaneously With APU Air. True. False.

Min ALT for use AP on T.O with SRS mode. 100 ft AGL and at least 5 s after liftof. 100 ft and at least 5 s after liftof. 150 ft AGL and at least 5 s after liftof.

Non Precision APP with LOC. 200 ft. 250 ft. 300 ft.

In approach with FINAL APP, V/S or FPA mode. 250 FT. 200 FT. 150 FT.

VISUAL APP. 500 ft. 550 ft. 250 ft.

ILS CAT I. 160 ft. 150 ft. 80 ft.

ILS CAT II (without autoland). 80 ft. 100 ft. 160 ft.

FMGS logic prevent the autopilot engaging during 6 sec after lift off. False. True.

RNP acurracy En route (with AP on in NAV). 1 nm. 0.5 nm. 0.3 nm.

RNP acurracy in terminal area (with AP on in NAV). 0.5 nm. 1 nm. 0.3 nm.

RNP acurracy approach (with AP on in NAV). 0.3 nm. 1 nm. 0.5 nm.

ILS CATEGORY II Minimum decision height. 100 ft. 50 ft. 100 AH.

ILS CATEGORY III FAIL PASSIVE (SINGLE) Minimum decision height. 50 ft. 100 AH. 100 ft.

ILS CATEGORY III FAIL OPERATIONAL (DUAL) Alert height. 100 ft. 75 ft. 50 ft.

ILS CATEGORY III DUAL without DH - Min RVR. 75 m. 100 m. 20 m.

AUTOLAND Max airport elevation. 9.200 ft. 9.000 ft. 5.750 ft.

Starter cycle APU. 3 int. x 60 min off. 4 int. x 60 min off. 2 int. x 60 min off.

APU Maximum N speed. 107 %. 100 %. 106 %.

Maximum EGT for APU start (below 25 000 ft). 900 °C. 982 °C. 682 °C.

Maximum EGT for APU start (above 25 000 ft). 982 °C. 900 °C. 682 °C.

Maximum EGT for APU running. 682 °C. 900 °C. 685 °C.

APU Max altitude for electrical power. 41.000 ft. 39.000 ft. 40.000 ft.

APU Max altitude for 100% of load con ISA +35 or below. 25.000 ft. 20.000 ft.

APU Max altitude for bleed engine start assist. 20.000 ft. 25.000 ft. 15.000 ft.

APU Elec + Bleed (1 pack) (load reduced depending on ISA). hasta 20.000 ft. hasta 15.000 ft.

APU Elec + Bleed (2 packs) (load reduced depending on ISA). hasta 15.000 ft. hasta 20.000 ft.

APU Battery Restart Limit (Emergency electrical configuration). 25.000 ft. 20.000 ft. 15.000 ft.

Use of APU bleed air for wing anti-ice is permitted. True. False.

If the APU Advisory appears LOW OIL LEVEL Maintenance actions in required within next. 10h of APU operation. 8h of APU operation. 12h of APU operation.

Engines Maximum N1 in normal operation CFM. 104 %. 100 %. 105 %.

Engines Maximum N2 in normal operation CFM. 105%. 104%. 100%.

Maximum EGT during starting CFM On ground & In flight. 725 ºC. 635 ºC. 950 ºC.

Maximun EGT T.O & G.o Around (2 engines) CFM. 950 °C (5 min). 900 °C (5 min). 915 °C (5 min).

Maximun EGT T.O & G.o Around (1 engine) CFM. 950 ºC (10 min). 900 ºC (10 min). 915 ºC (10 min).

Maximun EGT for MCT CFM. 915 ºC. 900 ºC. 950 ºC.

Engines Maximum N1 in normal operation IAE. 100%. 104%. 101%.

Engines Maximum N2 in normal operation IAE. 100%. 101%. 104%.

Maximum EGT during starting IAE. 635 ºC. 600 ºC. 610 ºC.

Maximun EGT T.O & G.o Around (2 engines) IAE. 635 ºC. 632 ºC. 615 ºC.

Maximun EGT T.O & G.o Around (1 engines) IAE. 635 ºC. 635 ºF. 615 ºC.

Maximun EGT for MCT IAE. 610 ºC. 635 ºC. 630 ºC.

Maximun engines Reverser Normal Cond. 70 kt. 70 k/hr. 60 kt.

OIL Maximum continuous temperature CFM. 140 °C. 155 °C. 145 ºC.

OIL Maximum transient temperature (15 min) CFM. 155 °C. 150 ºC. 145 ºC.

OIL Minimum starting temperature CFM. -40 °C. -35 °C. -10 ºC.

OIL Minimum temperature before takeoff CFM. -10 °. -40 º. 40 º.

Minimun OIL Quantity CFM. 9.5 q + 0.5 por Hr de vuelo. 9.0 q + 0.5 por Hr de vuelo.

Minimum OIL Pressure CFM. 13 PSI. 15 PSI. 10 PSI.

OIL Maximum continuous temperature IAE. 155 °C. 150 °C. 165 °C.

OIL Maximum transient temperature IAE. 165 ºC. 155 ºC. 160 ºC.

OIL Minimum starting temperature IAE. -40 ºC. -50 ºC. -60 ºC.

OIL Minimum temperature before takeoff IAE. 50 ºC. 40 ºC.

Minimum OIL temperature before IDLE is exceeded IAE. -10 ºC. -20 ºC.

Minimun OIL Quantity IAE. 11 q + 0.3 por hr de vuelo. 10 q + 0.3 por hr de vuelo. 9.5 q + 0.3 por hr de vuelo.

Minimum OIL Pressure IAE. 60 psi. 13 psi.

HYD normal operation pressure. 3000 psi ± 200. 3000 psi ± 300. 2500 psi ± 200.

TFLEX cannot be ‐ Higher than TMAXFLEX, equal to ISA + 53 °C. ‐ Lower than the flat temperature (TREF). ‐ Lower than the actual OAT. TRUE. False.

No se puede asumir FLEX cuando: Runway contaminated Antiskid Inoperative Windshear suspected. True. False.

Starting duty cycle CFM. 4 de 2 min con 20 seg off, after 4, 15 min off. 2 de 2 min con 20 seg off, after 4, 15 min off.

Starting duty cycle IAE. 2 de 2 min y 1 de 1 min con 15 seg off, after 3, 30 min off. 4 de 2 min y 1 de 1 min con 15 seg off, after 3, 30 min off.

Turbulence speed 0 to FL200. 250 kt. 275 kt. 255 kt.

Turbulence speed FL200 to FL320. 275 kt. 250 kt. M.76.

Turbulence speed FL320 and above. M.76. 250 kt. 275 kt.

Min temp JET A. -36ºC. -43ºC. -54ºC.

Min temp JET A1. -43ºc. -36ºc. -40ºc.

Max temp JET A1 / JET A. 54ºC. 50ºC. 54ºF.

If one tire is deflated on one or more gear (max 3 tires) the max taxi speed should be. 7 kt. 3 kt. 10 kt.

If two tires are deflated on the same gear (other main gear tires not being deflated) the max taxi speed should be ___ and the nose wheel steering angle limited to ____. 3 kt and 30º. 7 kt and 30º. 3 kt and 25º.

Max angle using handwheels. 75º. 85º.

Max degrees with Towbarless car. 85º. 75º.

Maximum brake temperature for takeoff (brake fans off). 300ºC. 250ºC. 150ºC.

Max continuous load per GER. 100% (90 kva). 101% (90 kva). 110% (90 kva).

Maximum brake temperature for takeoff (brake fans ON). 150ºC. 300ºC. 250ºC. 150 ºF.

Max continuous load per TR. 200 A. 230 A. 210 A.

Minimum Equipment for RVSM. -2 ADR + 2 DMC -1 TRANSPONDER -1 AP CHANNEL KEEP CAPABILITY -2 PFD -1 FCU CHANNEL -1 FWC ------------------------------------------------------------. -2 ADR + 2 DMC -1 TRANSPONDER -2 AP CHANNEL KEEP CAPABILITY -2 PFD -1 FCU CHANNEL -1 FWC -------------------------------------------------------------.

Maintenance action is due in the following cases: ------------------------------------------------------------ • The temperature difference between two brakes of a gear is more than 150 °C, and the temperature of one of these brakes is above or equal to 600 °C, or • The temperature difference between two brakes of a gear is more than 150 °C, and the temperature of one of these brakes is below or equal to 60 °C, or • The difference between the average temperature of the left gear brakes and right brakes is above or equal to 200 °C, or • The temperature of one brake exceeds 900 °C. ----------------------------------------------------------------------------------------------------------------------------------------------------------------------. ----------------------------------------------------------------------------------------- • The temperature difference between two brakes of a gear is more than 150 °C, and the temperature of one of these brakes is above or equal to 650 °C, or • The temperature difference between two brakes of a gear is more than 150 °C, and the temperature of one of these brakes is below or equal to 60 °C, or • The difference between the average temperature of the left gear brakes and right brakes is above or equal to 200 °C, or • The temperature of one brake exceeds 950 °C. -----------------------------------------------------------------------------------------------------------------------------------------------------------------------.

MINIMUM CONTROL SPEED FOR LANDING (VMCL) A320 - 214. 113 kt. 110 kt. 111 kt.

Instrument RVSM check. ±75 ft between each PFDs and the airport elevation. ±20 ft between both PFDs / 200 ft RVSM. And depending on the aircraft configuration: ±100 ft between ISIS and PFDs. ±300 ft btween mechanical standby altimeters and PFDs. N/A.