Limitaciones A320 (ALL)

Question 1

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS

- Clean configuration

Answer 1

-1 g to +2.5 g

Question 2

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS

- Other Configurations

Answer 2

0 g to +2 g

Question 3

Max runway altitude to operate

Answer 3

14,100 ft

Question 4

Nominal and Minimum runway width

Answer 4

45m and 30m

Question 5

Maximum certified crosswind for TAKEOFF for A320NEO (N769AV, N775AV, N776AV, N779AV)

Answer 5

35 Kt

Question 6

Maximum certified crosswind for LANDING for A320NEO (N769AV, N775AV, N776AV, N779AV)

Answer 6

38 kt

Question 7

Maximum demonstrated crosswind (takeoff and landing)

Answer 7

38 Kt

Question 8

Maximum tailwind for takeoff

Answer 8

15 Kt

Question 9

Maximum tailwind for landing

Answer 9

15 Kt

Question 10

The maximum wind for passenger door operation

Answer 10

65 Kt

Question 11

The maximum wind for FWD and AFT cargo door operation

Answer 11

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)

Question 12

The FWD and AFT cargo doors must be closed before the wind speed exceeds

Answer 12

65 Kt

Question 13

COCKPIT WINDOW OPEN MAXIMUM SPEED

Answer 13

200 Kt

Question 14

MAXIMUM OPERATING SPEED VMO/MMO

Answer 14

350kt / M 0.82

Question 15

Max speed with Flaps 1

Answer 15

230 Kt

Question 16

Max speed with Flaps 1+F

Answer 16

215 Kt

Question 17

Max speed with Flaps 2

Answer 17

200 Kt

Question 18

Max speed with Flaps 3

Answer 18

185 Kt

Question 19

Max speed with Flaps Full

Answer 19

177 Kt

Question 20

Maximum speed with the landing gear extended (VLE)

Answer 20

280 Kt

Question 21

Maximum speed at which the landing gear may be extended (VLO extension)

Answer 21

250 Kt

Question 22

Maximum speed at which the landing gear may be retracted (VLO retraction)

Answer 22

220 Kt

Question 23

Maximum ground speed or Tire Speed

Answer 23

195 Kt

Question 24

MINIMUM CONTROL SPEED FOR LANDING (VMCL) (N492TA)

Answer 24

109 Kt

Question 25

WIPERS MAXIMUM OPERATING SPEED

Answer 25

230 Kt

Question 26

Maximum taxi weight

Answer 26

77,400 Kg

Question 27

Maximum takeoff weight (brake release)

Answer 27

77,000 Kg

Question 28

Maximum landing weight

Answer 28

66,000 Kg

Question 29

Maximum zero fuel weight

Answer 29

62,500 Kg

Question 30

Minimum weight

Answer 30

37,230 Kg

Question 31

With passengers on board, it is not recommended to exceed ____ min without air conditioning supply. The lack of fresh air supply will significantly reduce the cabin’s air quality.

Answer 31

20 Min

Question 32

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

Answer 32

High Pressure (HP)

Question 33

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, in normal avionics ventilation system configuration OAT ≤ 49 °C

Answer 33

No Limitation

Question 34

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, in normal avionics ventilation system configuration 49 °C < OAT ≤ 55 °C

Answer 34

2 Hours

Question 35

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, in normal avionics ventilation system configuration 55 °C < OAT ≤ 60 °C

Answer 35

1 Hour

Question 36

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, in normal avionics ventilation system configuration 60 °C < OAT ≤ 64 °C

Answer 36

0.5 Hour

Question 37

CABIN PRESSURE | Maximum positive differential pressure

Answer 37

9.0 PSI

Question 38

CABIN PRESSURE | Maximum negative differential pressure

Answer 38

-1.0 PSI

Question 39

CABIN PRESSURE | Safety relief valve setting

Answer 39

8.6 PSI

Question 40

The flight crew must not use conditioned air from the packs and from the **¿HP or LP?** Air Conditioning Unit at the same time, to prevent any adverse effect on the Air Conditioning system.

Answer 40

Low Pressure (LP)

Question 41

Use of AutoPilot Function | - At takeoff

Answer 41

100 ft AGL and at least 5 s after liftoff

Question 42

Use of AutoPilot Function | - In approach with F-G/S mode

Answer 42

200 ft AGL

Question 43

Use of AutoPilot Function | - In approach with FINAL APP, V/S or FPA mode

Answer 43

250 ft AGL

Question 44

Use of AutoPilot Function | - In circling approach

Answer 44

500 ft AGL for aircraft category C (600 ft AGL for | aircraft category D).

Question 45

Use of AutoPilot Function | - ILS/MLS approach when CAT1 is displayed on the FMA

Answer 45

160 ft AGL

Question 46

Use of AutoPilot Function | - ILS/MLS approach when CAT2 or CAT3 (single or dual) is displayed on the FMA

Answer 46

0 ft AGL if autoland

Question 47

NAVIGATION PERFORMANCE RNP accuracy with GPS PRIMARY is: - En route:

Answer 47

1 NM

Question 48

NAVIGATION PERFORMANCE RNP accuracy with GPS PRIMARY is: - In terminal area:

Answer 48

0.5 NM

Question 49

NAVIGATION PERFORMANCE RNP accuracy with GPS PRIMARY is: - In approach:

Answer 49

0.3 NM

Question 50

RNP AR: The aircraft is capable of conducting RNP AR operations when operated in accordance with the recommendations provided in the Airbus Airworthiness Compliance Document (ACD). The achieved RNP AR level could be below 0.3 NM and depends on the type of RNP AR application. Refer to ACD for maximum achievable RNP values. RNP AR capability has been demonstrated with AP ON for the following modes:

Answer 50

‐ Departure in NAV mode ‐ Initial and Intermediate approach in NAV or APP NAV modes ‐ Final approach in FINAL APP mode ‐ Missed approach in NAV mode.

Question 51

NAVIGATION PERFORMANCE | Se puede realizar una aproximacion RNAV(RNP) sin GPS PRIMARY disponible, solo si....

Answer 51

la cobertura de la ayuda a la navegación por radio (radioayuda) es compatible con el valor RNP y se muestra HIGH accuracy en la MCDU con el RNP especificado, y se obtiene una aprobación operacional.

Question 52

NAVIGATION PERFORMANCE Se puede realizar una aproximacion RNAV (GNSS) siempre que esté disponible GPS PRIMARY. Cierto o Falso?

Answer 52

Cierto

Question 53

ILS CATEGORY II | Minimum decision height

Answer 53

100 ft

Question 54

ILS CATEGORY II | For manual landing, AP should be disconnected no later than

Answer 54

80 ft AGL

Question 55

ILS CATEGORY II At least one autopilot must be engaged in APPR mode, and CAT 2 or CAT 3 SINGLE or CAT 3 DUAL must be displayed on the FMA. Cierto o Falso?

Answer 55

Cierto

Question 56

ILS CATEGORY III FAIL PASSIVE ( CAT III SINGLE) | Minimum decision height

Answer 56

50 ft

Question 57

ILS CATEGORY III FAIL PASSIVE (SINGLE) At least one autopilot must be engaged in APPR mode, and CAT 3 SINGLE or CAT 3 DUAL must be displayed on the FMA. Cierto o Falso?

Answer 57

Cierto

Question 58

ILS CATEGORY III FAIL OPERATIONAL (CAT III DUAL) | Alert height

Answer 58

100 ft AGL

Question 59

ILS CATEGORY III FAIL OPERATIONAL (CAT III DUAL) CAT III without DH: Minimum Runway Visual Range

Answer 59

75 m

Question 60

ILS CATEGORY III FAIL OPERATIONAL (CAT III DUAL) A/THR must be used in selected or managed speed. Both autopilots must be engaged in APPR mode, and CAT 3 DUAL must be displayed on the FMA. Cierto o Falso?

Answer 60

Cierto

Question 61

MAXIMUM WIND CONDITIONS ILS CAT II y III | Headwind

Answer 61

30 kt

Question 62

MAXIMUM WIND CONDITIONS ILS CAT II y III | Tailwind

Answer 62

10 Kt

Question 63

MAXIMUM WIND CONDITIONS ILS CAT II y III | Crosswind

Answer 63

20 Kt

Question 64

APU After ___ consecutive APU start attempts, the flight crew must wait ___ min before a new start attempt.

Answer 64

3 attempts - 60min

Question 65

APU | Maximum N speed

Answer 65

107 %

Question 66

APU | Maximum EGT for APU start (below 35 000 ft)

Answer 66

1,090 °C

Question 67

APU | Maximum EGT for APU start (above 35 000 ft)

Answer 67

1,120 °C

Question 68

APU | Maximum EGT for APU running

Answer 68

675 °C

Question 69

APU | During refuel/defuel procedures, APU starts or shutdown are permitted with the following restrictions:

Answer 69

‐ If the APU failed to start or following an automatic APU shutdown, do not start the APU ‐ If a fuel spill occurs, perform a normal APU shutdown.

Question 70

APU | Max altitude operation

Answer 70

41,000 ft

Question 71

APU BLEED | Max altitude to assist engine start

Answer 71

20,000 ft

Question 72

APU BLEED | Max altitude for air conditioning and pressurization (single pack operation)

Answer 72

22,500 ft

Question 73

APU BLEED | Max altitude for air conditioning and pressurization (dual pack operation)

Answer 73

15,000 ft

Question 74

APU BLEED Use of APU bleed air for wing anti-ice is not permitted. Cierto o Falso?

Answer 74

Cierto

Question 75

ENGINES | Max time with TOGA and All engines operative

Answer 75

5 min

Question 76

ENGINES | Max time with TOGA and One engine operative

Answer 76

10 min

Question 77

ENGINES (NEO CFM LEAP 1A Engine) | Max EGT with TOGA

Answer 77

1,060 °C

Question 78

ENGINES (NEO CFM LEAP 1A Engine) | Max EGT with MCT

Answer 78

1,025 °C

Question 79

ENGINES (NEO CFM LEAP 1A Engine) | Max EGT at START in Ground

Answer 79

750 °C

Question 80

ENGINES (NEO CFM LEAP 1A Engine) | Max EGT at START in Flight

Answer 80

875 °C

Question 81

ENGINES (CFM Engine) | Max EGT with TOGA

Answer 81

950 °C

Question 82

ENGINES (CFM Engine) | Max EGT with MCT

Answer 82

915 °C

Question 83

ENGINES (CFM Engine) | Max EGT at START

Answer 83

725 °C

Question 84

ENGINES (IAE Engine) | Max EGT with TOGA

Answer 84

635 °C y (650 °C CA321)

Question 85

ENGINES (IAE Engine) | Max EGT with MCT

Answer 85

610 °C

Question 86

ENGINES (IAE Engine) | Max EGT at START

Answer 86

635 °C

Question 87

ENGINES (NEO CFM LEAP 1A Engine) | Max N1

Answer 87

101 %

Question 88

ENGINES (NEO CFM LEAP 1A Engine) | Max N2

Answer 88

116.5 % (117 %)

Question 89

ENGINES (CFM Engine) | Max N1

Answer 89

104 %

Question 90

ENGINES (CFM Engine) | Max N2

Answer 90

105 %

Question 91

ENGINES (IAE Engine) | Max N1

Answer 91

100 %

Question 92

ENGINES (IAE Engine) | Max N2

Answer 92

100 %

Question 93

ENGINES (NEO CFM LEAP 1A Engine) | Minimum OIL quantity and consumption per hour

Answer 93

10.6qt and 0.45qt per hour

Question 94

ENGINES (NEO CFM LEAP 1A Engine) | Maximum Temperature

Answer 94

140 °C

Question 95

ENGINES (NEO CFM LEAP 1A Engine) | Maximum transient temperature (15 min)

Answer 95

155 °C

Question 96

ENGINES (NEO CFM LEAP 1A Engine) | Minimum starting temperature

Answer 96

-40 °C

Question 97

ENGINES (NEO CFM LEAP 1A Engine) | Minimum temperature before takeoff

Answer 97

19 °C

Question 98

ENGINES (NEO CFM LEAP 1A Engine) | Minimum oil pressure

Answer 98

17.4 psi

Question 99

ENGINES (CFM) | Maximum Temperature

Answer 99

140 °C

Question 100

ENGINES (CFM) | Maximum transient temperature (15 min)

Answer 100

155 °C

Question 101

ENGINES (CFM) | Minimum starting temperature

Answer 101

-40 °C

Question 102

ENGINES (CFM) | Minimum temperature before takeoff

Answer 102

-10 °C

Question 103

ENGINES (CFM) | Minimum OIL quantity and consumption per hour

Answer 103

9.5qt and 0.5qt per hour

Question 104

ENGINES (CFM) | Minimum oil pressure

Answer 104

13 PSI

Question 105

ENGINES (IAE) | Minimum OIL quantity and consumption per hour

Answer 105

11.0qt abd 0.3qt per hour

Question 106

ENGINES (IAE) | Maximum temperature

Answer 106

155 °C

Question 107

ENGINES (IAE) | Maximum transient temperature (15 min)

Answer 107

165 °C

Question 108

ENGINES (IAE) | Minimum starting temperature

Answer 108

-40 °C

Question 109

ENGINES (IAE) | Minimum temperature before IDLE is exceeded

Answer 109

-10 °C

Question 110

ENGINES (IAE) | Minimum temperature before takeoff

Answer 110

50 °C

Question 111

ENGINES (IAE) | Minimum oil pressure

Answer 111

60 psi

Question 112

ENGINES (CFM) | STARTER Cycles Explain

Answer 112

- 3 START = 1 CYCLE - 20s Pause between cycle - 15 min Pause after 4 cycles - Starter not above 20%

Question 113

ENGINES (IAE) | STARTER Cycles Explain

Answer 113

- 1 START = 1 CYCLE - 15s Pause between cycles - 30 min Pause after 3 cycles or 5 min crank - 5 min Maximum Crank - Starter not above 10% on ground 18% in flight

Question 114

REVERSE THRUST LIMITATIONS - Selection of reverse is Prohibited in ______ - Backing the aircraft with Reverse is _______ - Maximum Reverse should not be used below ___kt

Answer 114

Flight - Prohibited - 70kt

Question 115

ENGINES WIND LIMITATIONS - Engine is able to start with __kt crosswind - Engine crosswind takeoff is __kt - Soft GA in not permited with ________ inop

Answer 115

45kt - 35Kt - One Engine

Question 116

Maximum operating altitude with slats and/or flaps extended

Answer 116

20,000 ft

Question 117

ICE AND RAIN PROTECTION Icing conditions exist when OAT or TAT is at or below __℃ and visible moisture is visible. (cloud,fog, with less than __ sm rain snoiw or ice cristals).

Answer 117

10°C - 1sm (1600m)

Question 118

ICE AND RAIN PROTECTION | Severe ice accreation is when a layer of ice is __mm or greater.

Answer 118

5mm

Question 119

RAIN REPELENT | Use only with ______ to ______ rain

Answer 119

moderate - heavy

Question 120

NAVIGATION | Ground aligement or IRS between...

Answer 120

73ºN and 73ºS

Question 121

FUEL | Certified Fuel

Answer 121

JETA JETA1 JETB JP4 JP5 JP8 Nº3 JET RT TS-1

Question 122

FUEL JET A1 | Fuel Temp Limits

Answer 122

-43°C - 54°C

Question 123

FUEL JET A | Fuel Temp Limits

Answer 123

-36°C - 54°C

Question 124

FUEL IMBALANCE TakeOff Tank Fuel QTY.... Full Max Asymetry..... ___

Answer 124

500 kg

Question 125

FUEL IMBALANCE TakeOff Tank Fuel QTY.... 3000kg Max Asymetry..... ___

Answer 125

1050 Kg

Question 126

FUEL IMBALANCE TakeOff Tank Fuel QTY.... 1450kg Max Asymetry..... ___

Answer 126

1450 Kg

Question 127

FUEL IMBALANCE TakeOff Outer Tanks

Answer 127

370 Kg

Question 128

FUEL IMBALANCE Landing Tank Fuel QTY.... Full Max Asymetry..... ___

Answer 128

1500 kg

Question 129

FUEL IMBALANCE Landing Tank Fuel QTY.... 4300 kg Max Asymetry..... ___

Answer 129

1600 kg

Question 130

FUEL IMBALANCE Landing Tank Fuel QTY.... 2250 kg Max Asymetry..... ___

Answer 130

2250 kg

Question 131

FUEL IMBALANCE Landing Outer Tanks

Answer 131

690 Kg

Question 132

FUEL | Minimum fuel qty for TakeOff

Answer 132

1500 Kg

Question 133

ON-BOARD AIRPORT NAVIGATION SYSTEM (OANS) TAXI: The use of OANS is authorized on __________

Answer 133

PF and PM displays

Question 134

ON-BOARD AIRPORT NAVIGATION SYSTEM (OANS) TAKEOFF: The use of OANS is authorized on __________

Answer 134

PM display only

Question 135

LANDING GEAR | Brake Temp Brake Fan off

Answer 135

300 °C

Question 136

LANDING GEAR | Brake Temp Brake Fan on

Answer 136

150 °C

Question 137

NWS | Maximum nws angle

Answer 137

85 °

Question 138

Taxi with deflated tires | Max speed 1 tire per gear in turn

Answer 138

7 kt

Question 139

Taxi with deflated tires | Max speed 2 tires deflated on same gear

Answer 139

3 kt

Question 140

Taxi with deflated tires | Max WS

Answer 140

30 °