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Aircraft Longitudinal CG Calculation Quiz

13 Questions

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Aircraft Longitudinal CG Calculation Quiz

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Questions and Answers

What is the longitudinal CG position in meters for the given conditions?

2.91 m (correct)

2.82 m

2.97 m

2.85 m

To move the center of gravity to 40%, how much mass needs to be transferred from the forward to the aft cargo hold?

183 kg (correct)

104 kg

165 kg

110 kg

What is the correct formula for minimum take-off safety speed?

VMCG

V2 min. (correct)

None of the above

What is the moment arm of the forward cargo in meters?

$-0.50$ m (D) Signup and view all the answers

What is the length of the mean aerodynamic chord in meters?

$1$ m (D) Signup and view all the answers

What is the center of gravity position in percentage MAC to move the center of gravity to 40%?

$25%$ MAC (D) Signup and view all the answers

What is the moment arm of the aft cargo in meters?

2.50 m (C) Signup and view all the answers

What is the aircraft mass in kilograms to move the center of gravity to 40%?

2 200 kg (C) Signup and view all the answers

What is the rotation speed (VR) in relation to the minimum take-off safety speed (V2 min.)?

$VR > V2 min.$ (D) Signup and view all the answers

What is the longitudinal CG position in meters for the given conditions?

2.91 m (A) Signup and view all the answers

Aircraft Longitudinal CG Calculation Quiz

Choose a study mode

Podcast

Questions and Answers

What is the longitudinal CG position in meters for the given conditions?

To move the center of gravity to 40%, how much mass needs to be transferred from the forward to the aft cargo hold?

What is the correct formula for minimum take-off safety speed?

What is the moment arm of the forward cargo in meters?

What is the length of the mean aerodynamic chord in meters?

What is the center of gravity position in percentage MAC to move the center of gravity to 40%?

What is the moment arm of the aft cargo in meters?

What is the aircraft mass in kilograms to move the center of gravity to 40%?

What is the rotation speed (VR) in relation to the minimum take-off safety speed (V2 min.)?

What is the longitudinal CG position in meters for the given conditions?

What mass needs to be transferred from the forward to the aft cargo hold to move the center of gravity to 40%?

What is the length of the mean aerodynamic chord in meters?

What is the correct formula for minimum take-off safety speed?

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