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A320 - Limitations
62問 • 1年前
  • Angelo Ortiz
    • 通報

    問題一覧

  • 1

    Flight Maneuvering Load Acceleration Limits: Clean Configuration

    -1g to +2.5g

  • 2

    Runway altitude:

    9,200 ft

  • 3

    Maximum wind for FWD and AFT cargo door operation if aircraft nose is into the wind, or if the FWD and AFT cargo doors are on the leeward side:

    50 kts

  • 4

    Wipers maximum operating speed:

    230 kts

  • 5

    Minimum weight:

    37,230 kg

  • 6

    Maximum zero fuel weight:

    61,000 kg

  • 7

    Maximum landing weight:

    64,500 kg

  • 8

    Maximum takeoff weight (brake release):

    73,500 kg

  • 9

    Maximum taxi weight:

    73,900 kg

  • 10

    Minimum control speed for landing (VMCL):

    113 kts

  • 11

    Maximum ground speed:

    195 kts

  • 12

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

    220 kts/M 0.54

  • 13

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

    250 kts/M 0.60

  • 14

    Maximum speed with the landing gear extended (VLE):

    280 kts/M 0.67

  • 15

    MMO

    M 0.82

  • 16

    VMO:

    350 kts

  • 17

    Max speed for Flaps lever configuration: CONF FULL

    177 kts

  • 18

    Max speed for Flaps lever configuration: CONF 3

    185 kts

  • 19

    Max speed for Flaps lever configuration: CONF 2

    200 kts

  • 20

    Max speed for Flaps lever configuration: CONF 1+F

    215 kts

  • 21

    Max speed for Flaps lever configuration: CONF 1

    230 kts

  • 22

    Max speed for Flaps lever configuration: CONF 0

    VM0/MMO

  • 23

    Cockpit window open maximum speed:

    200 kts

  • 24

    Maximum wind for FWD and AFT cargo door operation:

    40 kts

  • 25

    Maximum wind for passenger door operation:

    65 kts

  • 26

    Maximum tailwind (takeoff and landing):

    15 kts

  • 27

    Maximum demonstrated crosswind (takeoff and landing):

    38 kts

  • 28

    Minimal runway width:

    30 meters

  • 29

    Nominal runway width:

    45 meters

  • 30

    Runway slope (mean):

    ±2 %

  • 31

    Flight Maneuvering Load Acceleration Limits: Other Configuration

    0g to +2g

  • 32

    Electric power supply must be limited during ground operations. In normal avionics ventilation system configuration: OAT ≤ 49 °C

    No limitation

  • 33

    Electric power supply must be limited during ground operations. In normal avionics ventilation system configuration: 49 °C < OAT ≤ 55 °C

    2 h

  • 34

    Electric power supply must be limited during ground operations. In normal avionics ventilation system configuration: 55 °C < OAT ≤ 60 °C

    1 h

  • 35

    Electric power supply must be limited during ground operations. In normal avionics ventilation system configuration: 60 °C < OAT ≤ 64 °C

    0.5 h

  • 36

    Maximum positive differential pressure

    9.0 PSI

  • 37

    Maximum negative differential pressure

    -1.0 PSI

  • 38

    Safety relief valve setting

    8.6 PSI

  • 39

    Maximum wind condition for ILS/MLS (CAT II or CAT III and for GLS) CAT I: Headwind:

    30 kts

  • 40

    Maximum wind condition for ILS/MLS (CAT II or CAT III and for GLS) CAT I: Tailwind:

    10 kts

  • 41

    Maximum wind condition for ILS/MLS (CAT II or CAT III and for GLS) CAT I: Crosswind:

    20 kts

  • 42

    APU ROTOR SPEED: Maximum N speed:

    107%

  • 43

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

    1090 °C

  • 44

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

    1120 °C

  • 45

    Maximum EGT for APU running:

    675 °C

  • 46

    Thrust Setting/EGT Limits: Takeoff and Go-around - All engines operative:

    5 mins - 950°C

  • 47

    Thrust Setting/EGT Limits: Takeoff and Go-around - One engines inoperative:

    10 mins - 950°C

  • 48

    Thrust Setting/EGT Limits: Maximum Continuos Thrust (MCT)

    Not limited - 915°C

  • 49

    Thrust Setting/EGT Limits: Starting (On ground/In flight):

    725°C

  • 50

    APU BLEED: Max altitude to assist engine start:

    20 000 ft

  • 51

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

    22 500 ft

  • 52

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

    15 000 ft

  • 53

    ENGINES: Maximum N1

    104%

  • 54

    ENGINES: Maximum N2

    105%

  • 55

    OIL TEMPERATURE: Maximum continuous temperature

    140 °C

  • 56

    OIL TEMPERATURE: Maximum transient temperature (15 min)

    155 °C

  • 57

    OIL TEMPERATURE: Minimum starting temperature

    -40 °C

  • 58

    OIL TEMPERATURE: Minimum temperature before takeoff

    -10 °C

  • 59

    OIL QUANTITY: Minimum oil quantity

    9.5 qt + estimated consumption

  • 60

    Maximum operating altitude with slats and/or flaps extended

    20 000 ft

  • 61

    Minimum fuel quantity for takeoff

    1 500 kg

  • 62

    Maximum brake temperature for takeoff

    300 °C

    • B777 - Part 8

    B777 - Part 8

    Angelo Ortiz · 50問 · 3年前

    B777 - Part 8

    B777 - Part 8

    50問 • 3年前
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    B777 - Part 3

    B777 - Part 3

    Angelo Ortiz · 50問 · 3年前

    B777 - Part 3

    B777 - Part 3

    50問 • 3年前
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    B777 - Part 6

    B777 - Part 6

    Angelo Ortiz · 50問 · 3年前

    B777 - Part 6

    B777 - Part 6

    50問 • 3年前
    Angelo Ortiz

    B777 - Part 4

    B777 - Part 4

    Angelo Ortiz · 50問 · 3年前

    B777 - Part 4

    B777 - Part 4

    50問 • 3年前
    Angelo Ortiz

    B777 - Part 1

    B777 - Part 1

    Angelo Ortiz · 50問 · 3年前

    B777 - Part 1

    B777 - Part 1

    50問 • 3年前
    Angelo Ortiz

    B777 - Part 7

    B777 - Part 7

    Angelo Ortiz · 50問 · 3年前

    B777 - Part 7

    B777 - Part 7

    50問 • 3年前
    Angelo Ortiz

    B777 - Part 9

    B777 - Part 9

    Angelo Ortiz · 28問 · 3年前

    B777 - Part 9

    B777 - Part 9

    28問 • 3年前
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    B777 - Part 2

    B777 - Part 2

    Angelo Ortiz · 50問 · 3年前

    B777 - Part 2

    B777 - Part 2

    50問 • 3年前
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    B777 - Part 5

    B777 - Part 5

    Angelo Ortiz · 50問 · 3年前

    B777 - Part 5

    B777 - Part 5

    50問 • 3年前
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    AIA - VUL

    AIA - VUL

    Angelo Ortiz · 100問 · 2年前

    AIA - VUL

    AIA - VUL

    100問 • 2年前
    Angelo Ortiz

    Underwriting

    Underwriting

    Angelo Ortiz · 66問 · 2年前

    Underwriting

    Underwriting

    66問 • 2年前
    Angelo Ortiz

    Airplanes and Aerodynamics

    Airplanes and Aerodynamics

    Angelo Ortiz · 49問 · 2年前

    Airplanes and Aerodynamics

    Airplanes and Aerodynamics

    49問 • 2年前
    Angelo Ortiz

    Airplane Instruments, Engines and Systems

    Airplane Instruments, Engines and Systems

    Angelo Ortiz · 77問 · 2年前

    Airplane Instruments, Engines and Systems

    Airplane Instruments, Engines and Systems

    77問 • 2年前
    Angelo Ortiz

    Airport, ATC and Airspace

    Airport, ATC and Airspace

    Angelo Ortiz · 88問 · 2年前

    Airport, ATC and Airspace

    Airport, ATC and Airspace

    88問 • 2年前
    Angelo Ortiz

    Federal Aviation Regulations - Part 1

    Federal Aviation Regulations - Part 1

    Angelo Ortiz · 100問 · 2年前

    Federal Aviation Regulations - Part 1

    Federal Aviation Regulations - Part 1

    100問 • 2年前
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    Federal Aviation Regulations - Part 2

    Federal Aviation Regulations - Part 2

    Angelo Ortiz · 89問 · 2年前

    Federal Aviation Regulations - Part 2

    Federal Aviation Regulations - Part 2

    89問 • 2年前
    Angelo Ortiz

    Airplane Weight and Balance

    Airplane Weight and Balance

    Angelo Ortiz · 10問 · 2年前

    Airplane Weight and Balance

    Airplane Weight and Balance

    10問 • 2年前
    Angelo Ortiz

    Medical Factors and Decision Making

    Medical Factors and Decision Making

    Angelo Ortiz · 25問 · 2年前

    Medical Factors and Decision Making

    Medical Factors and Decision Making

    25問 • 2年前
    Angelo Ortiz

    Weather and Services

    Weather and Services

    Angelo Ortiz · 87問 · 2年前

    Weather and Services

    Weather and Services

    87問 • 2年前
    Angelo Ortiz

    Navigation

    Navigation

    Angelo Ortiz · 30問 · 2年前

    Navigation

    Navigation

    30問 • 2年前
    Angelo Ortiz

    問題一覧

  • 1

    Flight Maneuvering Load Acceleration Limits: Clean Configuration

    -1g to +2.5g

  • 2

    Runway altitude:

    9,200 ft

  • 3

    Maximum wind for FWD and AFT cargo door operation if aircraft nose is into the wind, or if the FWD and AFT cargo doors are on the leeward side:

    50 kts

  • 4

    Wipers maximum operating speed:

    230 kts

  • 5

    Minimum weight:

    37,230 kg

  • 6

    Maximum zero fuel weight:

    61,000 kg

  • 7

    Maximum landing weight:

    64,500 kg

  • 8

    Maximum takeoff weight (brake release):

    73,500 kg

  • 9

    Maximum taxi weight:

    73,900 kg

  • 10

    Minimum control speed for landing (VMCL):

    113 kts

  • 11

    Maximum ground speed:

    195 kts

  • 12

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

    220 kts/M 0.54

  • 13

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

    250 kts/M 0.60

  • 14

    Maximum speed with the landing gear extended (VLE):

    280 kts/M 0.67

  • 15

    MMO

    M 0.82

  • 16

    VMO:

    350 kts

  • 17

    Max speed for Flaps lever configuration: CONF FULL

    177 kts

  • 18

    Max speed for Flaps lever configuration: CONF 3

    185 kts

  • 19

    Max speed for Flaps lever configuration: CONF 2

    200 kts

  • 20

    Max speed for Flaps lever configuration: CONF 1+F

    215 kts

  • 21

    Max speed for Flaps lever configuration: CONF 1

    230 kts

  • 22

    Max speed for Flaps lever configuration: CONF 0

    VM0/MMO

  • 23

    Cockpit window open maximum speed:

    200 kts

  • 24

    Maximum wind for FWD and AFT cargo door operation:

    40 kts

  • 25

    Maximum wind for passenger door operation:

    65 kts

  • 26

    Maximum tailwind (takeoff and landing):

    15 kts

  • 27

    Maximum demonstrated crosswind (takeoff and landing):

    38 kts

  • 28

    Minimal runway width:

    30 meters

  • 29

    Nominal runway width:

    45 meters

  • 30

    Runway slope (mean):

    ±2 %

  • 31

    Flight Maneuvering Load Acceleration Limits: Other Configuration

    0g to +2g

  • 32

    Electric power supply must be limited during ground operations. In normal avionics ventilation system configuration: OAT ≤ 49 °C

    No limitation

  • 33

    Electric power supply must be limited during ground operations. In normal avionics ventilation system configuration: 49 °C < OAT ≤ 55 °C

    2 h

  • 34

    Electric power supply must be limited during ground operations. In normal avionics ventilation system configuration: 55 °C < OAT ≤ 60 °C

    1 h

  • 35

    Electric power supply must be limited during ground operations. In normal avionics ventilation system configuration: 60 °C < OAT ≤ 64 °C

    0.5 h

  • 36

    Maximum positive differential pressure

    9.0 PSI

  • 37

    Maximum negative differential pressure

    -1.0 PSI

  • 38

    Safety relief valve setting

    8.6 PSI

  • 39

    Maximum wind condition for ILS/MLS (CAT II or CAT III and for GLS) CAT I: Headwind:

    30 kts

  • 40

    Maximum wind condition for ILS/MLS (CAT II or CAT III and for GLS) CAT I: Tailwind:

    10 kts

  • 41

    Maximum wind condition for ILS/MLS (CAT II or CAT III and for GLS) CAT I: Crosswind:

    20 kts

  • 42

    APU ROTOR SPEED: Maximum N speed:

    107%

  • 43

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

    1090 °C

  • 44

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

    1120 °C

  • 45

    Maximum EGT for APU running:

    675 °C

  • 46

    Thrust Setting/EGT Limits: Takeoff and Go-around - All engines operative:

    5 mins - 950°C

  • 47

    Thrust Setting/EGT Limits: Takeoff and Go-around - One engines inoperative:

    10 mins - 950°C

  • 48

    Thrust Setting/EGT Limits: Maximum Continuos Thrust (MCT)

    Not limited - 915°C

  • 49

    Thrust Setting/EGT Limits: Starting (On ground/In flight):

    725°C

  • 50

    APU BLEED: Max altitude to assist engine start:

    20 000 ft

  • 51

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

    22 500 ft

  • 52

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

    15 000 ft

  • 53

    ENGINES: Maximum N1

    104%

  • 54

    ENGINES: Maximum N2

    105%

  • 55

    OIL TEMPERATURE: Maximum continuous temperature

    140 °C

  • 56

    OIL TEMPERATURE: Maximum transient temperature (15 min)

    155 °C

  • 57

    OIL TEMPERATURE: Minimum starting temperature

    -40 °C

  • 58

    OIL TEMPERATURE: Minimum temperature before takeoff

    -10 °C

  • 59

    OIL QUANTITY: Minimum oil quantity

    9.5 qt + estimated consumption

  • 60

    Maximum operating altitude with slats and/or flaps extended

    20 000 ft

  • 61

    Minimum fuel quantity for takeoff

    1 500 kg

  • 62

    Maximum brake temperature for takeoff

    300 °C