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Limitaciones Airbus > Limitaciones A320 (ALL) > Flashcards

Limitaciones A320 (ALL) Flashcards

1
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS

- Clean configuration

A

-1 g to +2.5 g

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2
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS

- Other Configurations

A

0 g to +2 g

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3
Q

Max runway altitude to operate

A

14,100 ft

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4
Q

Nominal and Minimum runway width

A

45m and 30m

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5
Q

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

A

35 Kt

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6
Q

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

A

38 kt

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7
Q

Maximum demonstrated crosswind (takeoff and landing)

A

38 Kt

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8
Q

Maximum tailwind for takeoff

A

15 Kt

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9
Q

Maximum tailwind for landing

A

15 Kt

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10
Q

The maximum wind for passenger door operation

A

65 Kt

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11
Q

The maximum wind for FWD and AFT cargo door operation

A 
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)
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12
Q

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

A

65 Kt

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13
Q

COCKPIT WINDOW OPEN MAXIMUM SPEED

A

200 Kt

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14
Q

MAXIMUM OPERATING SPEED VMO/MMO

A

350kt / M 0.82

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15
Q

Max speed with Flaps 1

A

230 Kt

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16
Q

Max speed with Flaps 1+F

A

215 Kt

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17
Q

Max speed with Flaps 2

A

200 Kt

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18
Q

Max speed with Flaps 3

A

185 Kt

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19
Q

Max speed with Flaps Full

A

177 Kt

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20
Q

Maximum speed with the landing gear extended (VLE)

A

280 Kt

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21
Q

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

A

250 Kt

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22
Q

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

A

220 Kt

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23
Q

Maximum ground speed or Tire Speed

A

195 Kt

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24
Q

MINIMUM CONTROL SPEED FOR LANDING (VMCL) (N492TA)

A

109 Kt

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25
Q

WIPERS MAXIMUM OPERATING SPEED

A

230 Kt

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26
Q

Maximum taxi weight

A

77,400 Kg

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27
Q

Maximum takeoff weight (brake release)

A

77,000 Kg

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28
Q

Maximum landing weight

A

66,000 Kg

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29
Q

Maximum zero fuel weight

A

62,500 Kg

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30
Q

Minimum weight

A

37,230 Kg

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31
Q

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.

A

20 Min

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32
Q

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.

A

High Pressure (HP)

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33
Q

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

A

No Limitation

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34
Q

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

A

2 Hours

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35
Q

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

A

1 Hour

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36
Q

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

A

0.5 Hour

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37
Q

CABIN PRESSURE

Maximum positive differential pressure

A

9.0 PSI

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38
Q

CABIN PRESSURE

Maximum negative differential pressure

A

-1.0 PSI

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39
Q

CABIN PRESSURE

Safety relief valve setting

A

8.6 PSI

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40
Q

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.

A

Low Pressure (LP)

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41
Q

Use of AutoPilot Function

- At takeoff

A

100 ft AGL and at least 5 s after liftoff

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42
Q

Use of AutoPilot Function

- In approach with F-G/S mode

A

200 ft AGL

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43
Q

Use of AutoPilot Function

- In approach with FINAL APP, V/S or FPA mode

A

250 ft AGL

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44
Q

Use of AutoPilot Function

- In circling approach

A

500 ft AGL for aircraft category C (600 ft AGL for

aircraft category D).

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45
Q

Use of AutoPilot Function

- ILS/MLS approach when CAT1 is displayed on the FMA

A

160 ft AGL

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46
Q

Use of AutoPilot Function

- ILS/MLS approach when CAT2 or CAT3 (single or dual) is displayed on the FMA

A

0 ft AGL if autoland

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47
Q

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

A

1 NM

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48
Q

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

A

0.5 NM

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49
Q

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

A

0.3 NM

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50
Q

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:

A

‐ 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.

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51
Q

NAVIGATION PERFORMANCE

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

A

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.

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52
Q

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

Cierto o Falso?

A

Cierto

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53
Q

ILS CATEGORY II

Minimum decision height

A

100 ft

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54
Q

ILS CATEGORY II

For manual landing, AP should be disconnected no later than

A

80 ft AGL

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55
Q

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?

A

Cierto

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56
Q

ILS CATEGORY III FAIL PASSIVE ( CAT III SINGLE)

Minimum decision height

A

50 ft

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57
Q

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?

A

Cierto

58
Q

ILS CATEGORY III FAIL OPERATIONAL (CAT III DUAL)

Alert height

A

100 ft AGL

59
Q

ILS CATEGORY III FAIL OPERATIONAL (CAT III DUAL)

CAT III without DH:
Minimum Runway Visual Range

A

75 m

60
Q

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?

A

Cierto

61
Q

MAXIMUM WIND CONDITIONS ILS CAT II y III

Headwind

A

30 kt

62
Q

MAXIMUM WIND CONDITIONS ILS CAT II y III

Tailwind

A

10 Kt

63
Q

MAXIMUM WIND CONDITIONS ILS CAT II y III

Crosswind

A

20 Kt

64
Q

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

A

3 attempts - 60min

65
Q

APU

Maximum N speed

A

107 %

66
Q

APU

Maximum EGT for APU start (below 35 000 ft)

A

1,090 °C

67
Q

APU

Maximum EGT for APU start (above 35 000 ft)

A

1,120 °C

68
Q

APU

Maximum EGT for APU running

A

675 °C

69
Q

APU

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

A

‐ 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.

70
Q

APU

Max altitude operation

A

41,000 ft

71
Q

APU BLEED

Max altitude to assist engine start

A

20,000 ft

72
Q

APU BLEED

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

A

22,500 ft

73
Q

APU BLEED

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

A

15,000 ft

74
Q

APU BLEED
Use of APU bleed air for wing anti-ice is not permitted.

Cierto o Falso?

A

Cierto

75
Q

ENGINES

Max time with TOGA and All engines operative

A

5 min

76
Q

ENGINES

Max time with TOGA and One engine operative

A

10 min

77
Q

ENGINES (NEO CFM LEAP 1A Engine)

Max EGT with TOGA

A

1,060 °C

78
Q

ENGINES (NEO CFM LEAP 1A Engine)

Max EGT with MCT

A

1,025 °C

79
Q

ENGINES (NEO CFM LEAP 1A Engine)

Max EGT at START in Ground

A

750 °C

80
Q

ENGINES (NEO CFM LEAP 1A Engine)

Max EGT at START in Flight

A

875 °C

81
Q

ENGINES (CFM Engine)

Max EGT with TOGA

A

950 °C

82
Q

ENGINES (CFM Engine)

Max EGT with MCT

A

915 °C

83
Q

ENGINES (CFM Engine)

Max EGT at START

A

725 °C

84
Q

ENGINES (IAE Engine)

Max EGT with TOGA

A

635 °C y (650 °C CA321)

85
Q

ENGINES (IAE Engine)

Max EGT with MCT

A

610 °C

86
Q

ENGINES (IAE Engine)

Max EGT at START

A

635 °C

87
Q

ENGINES (NEO CFM LEAP 1A Engine)

Max N1

A

101 %

88
Q

ENGINES (NEO CFM LEAP 1A Engine)

Max N2

A

116.5 % (117 %)

89
Q

ENGINES (CFM Engine)

Max N1

A

104 %

90
Q

ENGINES (CFM Engine)

Max N2

A

105 %

91
Q

ENGINES (IAE Engine)

Max N1

A

100 %

92
Q

ENGINES (IAE Engine)

Max N2

A

100 %

93
Q

ENGINES (NEO CFM LEAP 1A Engine)

Minimum OIL quantity and consumption per hour

A

10.6qt and 0.45qt per hour

94
Q

ENGINES (NEO CFM LEAP 1A Engine)

Maximum Temperature

A

140 °C

95
Q

ENGINES (NEO CFM LEAP 1A Engine)

Maximum transient temperature (15 min)

A

155 °C

96
Q

ENGINES (NEO CFM LEAP 1A Engine)

Minimum starting temperature

A

-40 °C

97
Q

ENGINES (NEO CFM LEAP 1A Engine)

Minimum temperature before takeoff

A

19 °C

98
Q

ENGINES (NEO CFM LEAP 1A Engine)

Minimum oil pressure

A

17.4 psi

99
Q

ENGINES (CFM)

Maximum Temperature

A

140 °C

100
Q

ENGINES (CFM)

Maximum transient temperature (15 min)

A

155 °C

101
Q

ENGINES (CFM)

Minimum starting temperature

A

-40 °C

102
Q

ENGINES (CFM)

Minimum temperature before takeoff

A

-10 °C

103
Q

ENGINES (CFM)

Minimum OIL quantity and consumption per hour

A

9.5qt and 0.5qt per hour

104
Q

ENGINES (CFM)

Minimum oil pressure

A

13 PSI

105
Q

ENGINES (IAE)

Minimum OIL quantity and consumption per hour

A

11.0qt abd 0.3qt per hour

106
Q

ENGINES (IAE)

Maximum temperature

A

155 °C

107
Q

ENGINES (IAE)

Maximum transient temperature (15 min)

A

165 °C

108
Q

ENGINES (IAE)

Minimum starting temperature

A

-40 °C

109
Q

ENGINES (IAE)

Minimum temperature before IDLE is exceeded

A

-10 °C

110
Q

ENGINES (IAE)

Minimum temperature before takeoff

A

50 °C

111
Q

ENGINES (IAE)

Minimum oil pressure

A

60 psi

112
Q

ENGINES (CFM)

STARTER Cycles Explain

A
  • 3 START = 1 CYCLE
  • 20s Pause between cycle
  • 15 min Pause after 4 cycles
  • Starter not above 20%
113
Q

ENGINES (IAE)

STARTER Cycles Explain

A
  • 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
114
Q

REVERSE THRUST LIMITATIONS

  • Selection of reverse is Prohibited in ______
  • Backing the aircraft with Reverse is _______
  • Maximum Reverse should not be used below ___kt
A

Flight - Prohibited - 70kt

115
Q

ENGINES WIND LIMITATIONS

  • Engine is able to start with __kt crosswind
  • Engine crosswind takeoff is __kt
  • Soft GA in not permited with ________ inop
A

45kt - 35Kt - One Engine

116
Q

Maximum operating altitude with slats and/or flaps extended

A

20,000 ft

117
Q

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).

A

10°C - 1sm (1600m)

118
Q

ICE AND RAIN PROTECTION

Severe ice accreation is when a layer of ice is __mm or greater.

A

5mm

119
Q

RAIN REPELENT

Use only with ______ to ______ rain

A

moderate - heavy

120
Q

NAVIGATION

Ground aligement or IRS between…

A

73ºN and 73ºS

121
Q

FUEL

Certified Fuel

A

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

122
Q

FUEL JET A1

Fuel Temp Limits

A

-43°C - 54°C

123
Q

FUEL JET A

Fuel Temp Limits

A

-36°C - 54°C

124
Q

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

A

500 kg

125
Q

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

A

1050 Kg

126
Q

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

A

1450 Kg

127
Q

FUEL IMBALANCE
TakeOff
Outer Tanks

A

370 Kg

128
Q

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

A

1500 kg

129
Q

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

A

1600 kg

130
Q

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

A

2250 kg

131
Q

FUEL IMBALANCE
Landing
Outer Tanks

A

690 Kg

132
Q

FUEL

Minimum fuel qty for TakeOff

A

1500 Kg

133
Q

ON-BOARD AIRPORT NAVIGATION SYSTEM (OANS)

TAXI:
The use of OANS is authorized on __________

A

PF and PM displays

134
Q

ON-BOARD AIRPORT NAVIGATION SYSTEM (OANS)

TAKEOFF:
The use of OANS is authorized on __________

A

PM display only

135
Q

LANDING GEAR

Brake Temp Brake Fan off

A

300 °C

136
Q

LANDING GEAR

Brake Temp Brake Fan on

A

150 °C

137
Q

NWS

Maximum nws angle

A

85 °

138
Q

Taxi with deflated tires

Max speed 1 tire per gear in turn

A

7 kt

139
Q

Taxi with deflated tires

Max speed 2 tires deflated on same gear

A

3 kt

140
Q

Taxi with deflated tires

Max WS

A

30 °

Limitaciones Airbus (1 decks)

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