What are the two main types of stability in aircraft
The two main types of stability are static stability and dynamic stability.
What is the primary source of lift for rotorcraft?
The primary source of lift for rotorcraft is the rotating blades (rotors).
What are the three primary flight controls of an aircraft?
The three primary flight controls are ailerons, elevators, and rudders.
What is a bank angle in relation to turning flight?
A bank angle is the angle at which an aircraft is tilted during a turn, affecting the direction and rate of the turn.
What would be the weight in pounds of a 180-pound person when subjected to a force of 3 g's?
540 pounds
What do you call an aircrafts tendency to return to its original attitude when diplaced?
Positive Stability
How does rotor blade pitch affect lift in a helicopter?
Rotor blade pitch affects lift by changing the angle of attack; increasing pitch increases lift, while decreasing pitch reduces lift.
What are the three axes of flight?
Longitudinal Axis
Lateral Axis
Vertical Axis
Why does an airplane tend to descend in a turn?
The vertical component of lift decreases.
What should a pilot do to minimize dangers from turbulence?
- Fly at maneuvering speed or slower
-avoid areas of rough conditions
Pitch stability refers to the movement of an aircraftʻs nose up and down around its...
lateral axis
Describe how rotor speed influences stability in rotorcraft.
Rotor speed influences stability as higher rotor speeds can provide more lift and stability, while lower speeds can lead to less control.
Name three ways a control input can be transmitted to a control surface
Hydraulic Pressure
Electronic Signals
Cable and Pulley
Propper rudder use can help you...
avoid a skidding turn.
During an approach to stall, an aircraft will stall at a higher speed when
the load factor is increased.
What happens to an aircraft if the center of gravity moves aft?
The aircraft becomes progressively more difficult to control.
Explain the concept of translational lift in rotorcraft.
Translational lift is the increase in lift experienced by rotorcraft when moving forward, due to the effect of increased airflow over the rotor blades.
What role do flaps play in flight?
-They increase lift
- They are retracted at cruising altitude
- They are extended during landing
An airplaneʻs rate of turn and itʻs airspeed are...
inversely proportional.
The amount of load that can be safely imposed on an airplane is dependent upon...
The speed of the airplane
What is the importance of the wing design in aircraft stability?
Wing design is crucial for stability as it affects the aircraft's lift characteristics, stall behavior, and overall aerodynamic performance.
What is the effect of wind on rotorcraft stability during flight?
Wind can affect rotorcraft stability by causing turbulence and altering the airflow around the rotors, which can lead to loss of control if not managed properly.
Describe how lift changes in a turn.
An airplane requires a sideward force to change its lateral flight path. This force is generated by banking the airplane’s wings and forcing some of the upward lifting force to act sideways. The vertical component of lift in flight, which originally acted to balance the aircraft’s weight in straight-and-level flight, is broken into vertical and horizontal components in a turn. The horizontal component of lift acts in the intended direction of the turn and is responsible for “pulling” the airplane into the turn.
When entering a turn, the rising wing produces more lift than the descending wing. The
increased lift causes more drag, which pulls the nose of the aircraft in a direction opposite the turn.
How should a pilot operate an aircraft to avoid overstressing its structure?
Pilots should...
- never operate an aircrarft outside of its acceptable weight and balance limitations
- should slow to maneuvering or slower to help reduce stresses on airframe during moderate or greater turbulence.
- should always stay clear of thunderstorms or other violent weather.
- should only perform maneuvers for which the aircraft is rated.
- should always operate within airspeed limitations
-should use smooth control inputs especially when fully deflecting control surfaces