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Questions and Answers
What is the maximum take-off weight for the 1900D?
What is the maximum take-off weight for the 1900D?
What is the maximum landing weight for the 1900D?
What is the maximum landing weight for the 1900D?
What is the maximum zero fuel weight for the 1900D?
What is the maximum zero fuel weight for the 1900D?
What is the minimum cargo door width and height for the 1900D?
What is the minimum cargo door width and height for the 1900D?
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How does humidity affect take-off performance?
How does humidity affect take-off performance?
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How does air density/density altitude affect the take-off performance?
How does air density/density altitude affect the take-off performance?
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What is the effect of increased aircraft weight on take-off distance required?
What is the effect of increased aircraft weight on take-off distance required?
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What is the most restrictive field length limit available from?
What is the most restrictive field length limit available from?
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What is the first segment of the departure profile?
What is the first segment of the departure profile?
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What is V2 speed?
What is V2 speed?
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What are the main variables that affect the aircraft take-off and landing performance?
What are the main variables that affect the aircraft take-off and landing performance?
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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?
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?
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When is an LMC (Load Manifest Check) carried out?
When is an LMC (Load Manifest Check) carried out?
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What is the minimum fuel required for a flight from OYSN to OYRN, flying overhead OYAA, using OYSY as the alternate?
What is the minimum fuel required for a flight from OYSN to OYRN, flying overhead OYAA, using OYSY as the alternate?
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What is the take-off weight with OAT of 35°C and a runway length of 1,043 meters?
What is the take-off weight with OAT of 35°C and a runway length of 1,043 meters?
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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?
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?
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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?
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?
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What is the weight of the survival kit?
What is the weight of the survival kit?
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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.