Lecture Notes Flashcards
Takeoff mass is
Complete mass minus start and taxi fuel
Landing mass is
complete mass minus start, taxi and trip fuel
The pitch stability with forward/aft CG
forward - stable, aft - unstable
The range with forawrd/aft CG
Forward - decreased
Since forward CG has more stability, the trim
More trim drag
The stalling speed with forward CG is
increased
The fuel consumption with forward CG i
increased
Final reserve fuel should be
45 minutes
Alternate fuel meaning
Alternative fuel for mised approach, landing at altenate, etc.
Trip fuel contains
Takeoff, climb, cruise, descent, approach and landing
Grass factor
1.2
Long grass factor
1.3
How to calculate runway slope
(Difference in height / runway length) * 100
Vx
best angle of climb speed (greated altitude is shortest horizontal distance)
Vy
best rate of climb speed (greatest altitude in shortest time)