FAA Written Flashcards
(193 cards)
The load factor for an a/c in a 60 degree bank turn is:
2 Gs
During a LEFT side-slip, an over-the-top spin would most likely occur if the stick is held ___ and ___ rudder was applied during a left side slip
- Too far back
2. Full right rudder
While holding the angle of bank constant in a level turn, if the rate of TURN is varied, the load factor would:
Remain CONSTANT regardless of air density and the resultant lift vector
As airspeed decreases in level flight below that speed for maximum lift/drag ratio, total drag of an airplane:
Increases because of increased INDUCED drag
If the airspeed is INCREASED during a coordinates level 45 degree bank turn, the load factor will:
Remain the same, but the radius of turn will increase
What changes must be made in a/c longitudinal control to maintain altitude while decreasing airspeed?
Increase AOA to compensate for DECREASING LIFT
Some a/c are fitted with wing spoilers to decrease:
Lift (during landing)
A rectangular wing, as compared to other wing planforms, has a tendency to stall first at the:
Wing ROOT, with the stall progression toward the wingtip
The angle of attack of a wing directly controls the:
Distribution of pressures acting on the wing
By changing the AOA of a wing, the pilot can control:
Lift, airspeed and drag
The critical AOA is exceeded when:
A stall occurs
The AOA at which a wing stalls remains constant:
ALWAYS!! Regardless of weight, dynamic pressure, bank angle or pitch attitude
The design maneuvering speed (Va) is:
A figure for recently designed a/c that defines the max. speed an airplane can safely stall
Is stall SPEED affected by AOA?
NO! By weight, load factor and power
In a rapid recovery from a dive, the effects of Load Factor would cause the stall speed to:
Increase!
recovery from a stall in any a/c becomes more difficult when the center of gravity moves ___;
AFT!
In a spin, what is the rotation centered around?
CG! (Not longitudinal axis)
Increasing AOA will:
Increase Drag
To generate the same amount of lift as altitude is increased, an a/c must be flown at:
A higher TAS for any given AOA
A pilot who intends to maintain level flight must coordinate AOA with what force of flight?
Thrust
In a stead state descent, the sum of all FORWARD forces is ____ to the sum of all REWARD forces
EQUAL
What is true regarding the force of life in stead, accelerated flight?
There is a corresponding indicated airspeed required for every AOA to generate sufficient life to maintain alititude
A changing AOA affects which 2 forces of flight?
Lift and WEIGHT!
In theory, if airspeed is doubled while in level flight, parasite drag AND lift produced will become:
four times greater