Beechcraft 1900D Aircraft Performance Quiz
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Questions and Answers

What is the maximum take-off weight for the 1900D?

  • 17,120 Ibs
  • 15,165 kgs
  • 17,120 kgs (correct)
  • 7,200 Ibs

    • What is the maximum landing weight for the 1900D?

  • 16,765 kgs (correct)
  • 15,165 lbs
  • 14,120 kgs
  • 16,765 lbs

    • What is the maximum zero fuel weight for the 1900D?

  • 6,878 lbs (correct)
  • 15,165 lbs
  • 7,200 kg
  • 15,165 kg

    • What is the minimum cargo door width and height for the 1900D?

    <p>49 cm + 54 cm (D)</p> Signup and view all the answers

    How does humidity affect take-off performance?

    <p>High humidity increases air density, which increases aircraft aerodynamic and engine performance. (A)</p> Signup and view all the answers

    How does air density/density altitude affect the take-off performance?

    <p>An increase in density altitude (decreases in air density) increases the take-off distance required (TODR). (D)</p> Signup and view all the answers

    What is the effect of increased aircraft weight on take-off distance required?

    <p>It increases the take-off distance required (D)</p> Signup and view all the answers

    What is the most restrictive field length limit available from?

    <p>Both A and B are correct (A)</p> Signup and view all the answers

    What is the first segment of the departure profile?

    <p>Extends from the reference point (60 ft length) to the point where the landing gear is retracted at a constant V2 speed (D)</p> Signup and view all the answers

    What is V2 speed?

    <p>The all engine operating take-off climb (B)</p> Signup and view all the answers

    What are the main variables that affect the aircraft take-off and landing performance?

    <p>Both A and B are correct (B)</p> Signup and view all the answers

    What is the max take-off weight if the flap is 17, bleeds off, engine anti-ice off, and temp is 35ºC, pressure altitude is 7000 ft?

    <p>16,100 kgs (B)</p> Signup and view all the answers

    When is an LMC (Load Manifest Check) carried out?

    <p>If the total of the LMC’s excluding fuel exceeds 2% of the MTOW (A)</p> Signup and view all the answers

    What is the minimum fuel required for a flight from OYSN to OYRN, flying overhead OYAA, using OYSY as the alternate?

    <p>16,599 lbs (C)</p> Signup and view all the answers

    What is the take-off weight with OAT of 35°C and a runway length of 1,043 meters?

    <p>16,500 lbs (C)</p> Signup and view all the answers

    What is the field length when the flap is 17°, bleeds are off, engine anti-ice is off, and the pressure altitude is 3,500ft?

    <p>1,043 meters (A)</p> Signup and view all the answers

    What is the maximum payload out of Djibouti for a flight to Aden with a temperature of 35°C and a runway length of 3,800ft x 17ft?

    <p>6,000 kg (A)</p> Signup and view all the answers

    What is the weight of the survival kit?

    <p>45 kg (D)</p> Signup and view all the answers

    Flashcards

    Maximum Take-Off Weight (MTOW)

    The maximum weight an aircraft can have at takeoff, considering all factors including fuel, passengers, and cargo.

    Zero Fuel Weight (ZFW)

    The total weight of the aircraft excluding fuel.

    Load Manifest Calculation (LMC)

    A calculation that determines if the total weight of the aircraft, excluding fuel, exceeds a certain percentage of the MTOW.

    Humidity's effect on air density

    The decrease in air density caused by high humidity, leading to reduced aerodynamic and engine performance.

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    Density Altitude

    The altitude corrected for air density, affecting take-off performance.

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    Take-off Distance Required (TODR)

    The distance required for an aircraft to take off, influenced by weight, altitude, temperature, and configuration.

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    V2 Speed

    The speed at which an aircraft climbs during takeoff, critical if an engine fails.

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    First Segment of Departure

    The first segment of a departure after takeoff, extending from the reference point to the landing gear retraction point at a constant V2 speed.

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    Minimum Fuel Required

    The minimum amount of fuel required for a flight, considering factors like route, weather, and alternate airports.

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    Maximum Payload

    The maximum cargo weight that an aircraft can carry, which is limited by the aircraft's design and the runway's capabilities.

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    Take-off Configuration

    The specific set of aircraft configuration settings used for taking off, such as flaps, bleeds, and anti-ice.

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    Cargo Door Dimensions

    The dimensions of the cargo door, which determine the size of cargo that can be loaded.

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    Maximum Baggage Weight

    The maximum weight allowed in the aft baggage compartment.

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    Passenger Weight Calculation

    The calculation of passenger weight, taking into account factors like age and gender.

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    Low Humidity's Impact on Density

    The effect of low humidity on air density, decreasing performance.

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    High Humidity's Impact on Density

    The effect of high humidity on air density, decreasing performance.

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    Study Notes

    Aircraft Weight Management

    • LMC (Load Manifest Calculation) carried out if:
      • Total of LMC’s, excluding fuel, exceeds 2%, 5%, or 10% of MTOW (Maximum Take-Off Weight).
    • Maximum Take-Off Weight for 1900D:
      • 17,120 lbs (7,700 kgs).
    • Maximum Landing Weight for 1900D:
      • 16,765 lbs (7,600 kgs).
    • Maximum Zero Fuel Weight for 1900D:
      • 15,165 lbs (6,878 kg).

    Performance Factors

    • Humidity effects:
      • Low humidity decreases air density, negatively impacting aerodynamic and engine performance.
      • High humidity also decreases air density.
    • Air density and density altitude influence take-off performance:
      • Increased density altitude leads to increased take-off distance required (TODR).
      • Decreased density altitude results in shorter TODR.
    • Aircraft weight and take-off performance:
      • Increased weight results in a greater TODR and reduced net take-off climb gradient.

    Flight Planning Considerations

    • Flight from OYSN to OYRN:
      • Calculate minimum fuel required flying over OYAA and using OYSY as alternate (specific aircraft: 5Y-BVP).
    • In Djibouti:
      • Assess max payload based on a runway of 3800 ft x 17 ft under the temperature of 35ºC.
    • Plan includes approach from 3,500 ft at 30ºC with specific take-off configuration (flap 17, bleeds off, anti-ice off).

    Take-Off Profiles

    • Take-off Field Length:
      • Influenced by weight, altitude, temperature, and configuration.
    • First segment of departure:
      • Extends from the reference point to the landing gear retraction point at a constant V2 speed, height varies per operation (options include 60 ft, 45 ft, and 35 ft).
    • V2 Speed Definition:
      • All-engine operating take-off climb speed, critical for safety in case of engine failure.

    Cargo and Seating Capacity

    • Cargo door dimensions:
      • Minimum width 125 inches, height 132 inches.
    • Maximum baggage weight in AFT compartment:
      • 1,000 lbs (454 kgs).
    • Passenger weight calculation includes differentiation based on age and gender across designated seats.

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    Description

    Test your knowledge of the Beechcraft 1900D aircraft's performance specifications, including maximum take-off weight, maximum landing weight, and maximum zero fuel weight. This quiz is designed for aviation professionals and students.

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