Question 1: What is the maximum flaps-extended speed?

• 65 KTS.
• 100 KTS.
• 165 KTS.

The correct answer for this question is not provided, therefore an explanation cannot be given.

Question 2: The acute angle A is the angle of

• dihedral.
• attack (Correct answer)
• incidence

Correct answer: attack

The angle of attack is defined as the acute angle between the chord line of an airfoil (such as a wing) and the relative wind. This angle is fundamental in aerodynamics, as it directly determines the amount of lift and drag generated by the wing, influencing the aircraft's performance.

Question 3: Which V-speed represents maneuvering speed?

• VA. (Correct answer)
• VLO.
• VNE.

Correct answer: VA.

VA, or maneuvering speed, is the maximum speed at which an aircraft can be subjected to full or abrupt control inputs without exceeding its structural limits. Below VA, the aircraft will stall before its airframe experiences excessive G-loads, making it a critical speed for safe operation in turbulent conditions or during aggressive maneuvers.

Question 4: An airplane said to be inherently stable will

• be difficult to stall.
• require less effort to control.
• not spin. (Correct answer)

Correct answer: not spin.

An inherently stable airplane is designed to resist deviations from its trimmed flight path and to return to that path after being disturbed. While stability helps prevent unintentional spins by resisting uncontrolled rotations, it does not make an aircraft immune to spinning if mishandled. However, it significantly reduces the aircraft's tendency to enter or sustain a spin compared to an unstable aircraft.

Question 5: The greatest vortex strength occurs when the generating aircraft is

• light, dirty, and fast.
• heavy, dirty, and fast.
• heavy, clean, and slow.V (Correct answer)

Correct answer: heavy, clean, and slow.V

Wingtip vortices, or wake turbulence, are strongest when the generating aircraft is heavy, clean (flaps and landing gear retracted), and flying at a slow airspeed. This combination requires a high angle of attack to produce sufficient lift, resulting in the greatest pressure differential over the wing and thus the most intense vortices.

Question 6: When departing behind a heavy aircraft, the pilot should avoid wake turbulence by maneuvering the aircraft

• below and downwind from the heavy aircraft.
• above and upwind from the heavy aircraft. (Correct answer)
• below and upwind from the heavy aircraft.

Correct answer: above and upwind from the heavy aircraft.

To avoid wake turbulence, which sinks and moves with the wind, a pilot should maneuver their aircraft above and upwind from the heavy aircraft's flight path. This strategy places the aircraft clear of the descending and drifting vortices, minimizing the risk of encountering hazardous turbulence.

Question 7: One of the main functions of flaps during approach and landing is to

• decrease the angle of descent without increasing the airspeed.
• permit a touchdown at a higher indicated airspeed.
• increase the angle of descent without increasing the airspeed. (Correct answer)

Correct answer: increase the angle of descent without increasing the airspeed.

One of the main functions of flaps during approach and landing is to increase both lift and drag. By extending flaps, the aircraft can maintain a slower airspeed while achieving a steeper angle of descent, allowing for a more controlled and precise approach without increasing the aircraft's speed.

Question 8: If an airplane weighs 3,300 pounds, what approximate weight would the airplane structure be required to support during a 30° banked turn while maintaining altitude?

• 1,200 pounds.
• 3,100 pounds.
• 3,960 pounds. (Correct answer)

Correct answer: 3,960 pounds.

In a banked turn, the load factor increases, meaning the wings must support more than the aircraft's actual weight. For a 30° banked turn, the load factor is approximately 1.154 (1 / cos(30°)). Therefore, the aircraft structure must support 3,300 pounds * 1.154 = 3,808.2 pounds, with 3,960 pounds being the closest available option.

Question 9: What is the definition of load factor?

• Angle of bank relative to an increase in stall speed.
• Angle of bank relative to the power-off stall speed in a specified configuration.
• Additional weight carried by the wings divided by the weight of the aircraft. (Correct answer)

Correct answer: Additional weight carried by the wings divided by the weight of the aircraft.

Load factor is defined as the ratio of the total load supported by the aircraft's wings to the actual weight of the aircraft. It quantifies the stress placed on the aircraft structure, expressed in 'G' units, and increases during maneuvers like turns, climbs, and turbulence.

Question 10: The condition that requires maximum caution when avoiding wake turbulence on landing is a

• light, quartering headwind.
• light, quartering tailwind. (Correct answer)
• strong headwind.

Correct answer: light, quartering tailwind.

A light, quartering tailwind is the most hazardous condition for wake turbulence on landing because it can push the vortices ahead of the generating aircraft, potentially placing them directly on the runway or in the approach path for an extended period. The light wind also prevents the vortices from dissipating quickly, increasing the risk to following aircraft.

Question 11: Which color identifies the power-off stalling speed with wing flaps and landing gear in the landing configuration?

• Upper limit of the green arc.
• Upper limit of the white arc.
• Lower limit of the white arc. (Correct answer)

Correct answer: Lower limit of the white arc.

On an airspeed indicator, the white arc represents the flap operating range. The lower limit of this white arc (VS0) specifically identifies the power-off stalling speed with the wing flaps and landing gear in the landing configuration, indicating the slowest safe airspeed for landing.

Question 12: Which marking identifies the never-exceed speed?

• Upper limit of the green arc.
• Upper limit of the white arc.
• The red radial line. (Correct answer)

Correct answer: The red radial line.

The red radial line on an airspeed indicator marks the VNE, or Never-Exceed Speed. This is the absolute maximum speed at which the aircraft may be operated under any circumstances, as exceeding it can lead to structural damage or failure due to excessive aerodynamic stress.

Question 13: What is the caution range of the airplane?

• 0 to 60 KTS.
• 100 to 165 KTS.
• 165 to 208 KTS. (Correct answer)

Correct answer: 165 to 208 KTS.

The caution range on an airspeed indicator is typically depicted by the yellow arc. This range indicates speeds where flight is permissible only in smooth air and with caution, as encountering turbulence at these speeds could lead to structural damage. The specific values (165 to 208 KTS) correspond to this yellow arc for a particular aircraft.

Question 14: During an approach to a stall, an increased load factor will cause the airplane to

• stall at a higher airspeed. (Correct answer)
• have a tendency to spin.
• be more difficult to control.

Correct answer: stall at a higher airspeed.

During an approach to a stall, an increased load factor (due to maneuvers like turns or turbulence) effectively increases the aircraft's weight relative to its wings. To support this greater load, the wings must generate more lift, which requires a higher angle of attack. Since the critical angle of attack (where a stall occurs) remains constant, the aircraft will reach this critical angle at a higher indicated airspeed when under an increased load.

Question 15: When taking off or landing at an airport where heavy aircraft are operating, one should be particularly alert to the hazards of wingtip vortices because this turbulence tends to

• rise from a crossing runway into the takeoff or landing path.
• rise into the traffic pattern area surrounding the airport.
• sink into the flightpath of aircraft operating below the aircraft generating the turbulence. (Correct answer)

Correct answer: sink into the flightpath of aircraft operating below the aircraft generating the turbulence.

Wingtip vortices are generated by the pressure differential over the wing and descend at a rate of several hundred feet per minute while spreading outwards. This means they sink into the flight path of aircraft operating below the aircraft that generated the turbulence, posing a significant hazard during takeoff and landing operations.

Question 16: Which would provide the greatest gain in altitude in the shortest distance during climb after takeoff?

• VY.
• VA.
• VX. (Correct answer)

Correct answer: VX.

VX is the best angle-of-climb speed, which provides the greatest gain in altitude over a given horizontal distance. This speed is crucial when clearing obstacles after takeoff, as it maximizes the climb gradient. In contrast, VY is the best rate-of-climb speed, which provides the greatest gain in altitude over a given period of time.

Question 17: The angle of attack for a propeller is defined as

• The angle between the propeller chord line and the relative wind. (Correct answer)
• The angle between the propeller chord line and the thrust vector.
• The pitch angle of the blade to the propeller hub.

Correct answer: The angle between the propeller chord line and the relative wind.

The angle of attack for any airfoil, including a propeller blade, is fundamentally defined as the angle between its chord line and the relative wind. This angle dictates how efficiently the blade generates thrust by interacting with the oncoming air. A higher angle of attack generally produces more thrust up to a critical point.

Question 18: Which V-speed represents best-angle-of-climb speed?

• VA.
• VX. (Correct answer)
• VY.

Correct answer: VX.

Vx represents the best-angle-of-climb speed, which allows the aircraft to gain the most altitude over a given horizontal distance. This speed is crucial for clearing obstacles immediately after takeoff, as it maximizes the climb gradient. It is typically a lower airspeed than Vy (best rate of climb).

Question 19: Floating caused by the phenomenon of ground effect will be most realized during an approach to land when at

• less than the length of the wingspan above the surface. (Correct answer)
• twice the length of the wingspan above the surface.
• a higher-than-normal angle of attack.

Correct answer: less than the length of the wingspan above the surface.

Ground effect is a phenomenon where the airflow around the wing is altered when an aircraft is flying very close to the ground, typically within one wingspan's length. This effect reduces induced drag and increases lift, causing the aircraft to 'float' or remain airborne longer than expected during an approach to land.

Question 20: The angle of attack at which an airplane wing stalls will

• increase if the CG is moved forward.
• change with an increase in gross weight.
• remain the same regardless of gross weight. (Correct answer)

Correct answer: remain the same regardless of gross weight.

An airplane wing always stalls at the same critical angle of attack, regardless of factors like gross weight, airspeed, or load factor. While changes in gross weight will affect the airspeed at which this critical angle of attack is reached, the angle itself remains constant. The wing's aerodynamic properties determine this critical angle.