Lecture Notes Flashcards

1
Q

Takeoff mass is

A

Complete mass minus start and taxi fuel

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2
Q

Landing mass is

A

complete mass minus start, taxi and trip fuel

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3
Q

The pitch stability with forward/aft CG

A

forward - stable, aft - unstable

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4
Q

The range with forawrd/aft CG

A

Forward - decreased

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5
Q

Since forward CG has more stability, the trim

A

More trim drag

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6
Q

The stalling speed with forward CG is

A

increased

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7
Q

The fuel consumption with forward CG i

A

increased

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8
Q

Final reserve fuel should be

A

45 minutes

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9
Q

Alternate fuel meaning

A

Alternative fuel for mised approach, landing at altenate, etc.

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10
Q

Trip fuel contains

A

Takeoff, climb, cruise, descent, approach and landing

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11
Q

Grass factor

A

1.2

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12
Q

Long grass factor

A

1.3

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13
Q

How to calculate runway slope

A

(Difference in height / runway length) * 100

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14
Q

Vx

A

best angle of climb speed (greated altitude is shortest horizontal distance)

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15
Q

Vy

A

best rate of climb speed (greatest altitude in shortest time)

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16
Q

Wind affects gliding endurance?

A

No, affects only flight path over the groud

17
Q

How to calculate ground distance over a climb?

A

NAM / TAS * GS
NAM = Nautical air miles (the distance flown)

18
Q

How to calculate distance flown by climb gradient percentage

A

(Height difference (ft) * 100) / Gradient