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</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.</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).</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</p> Signup and view all the answers

    What is the most restrictive field length limit available from?

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

    What is V2 speed?

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

    What is the weight of the survival kit?

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

    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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