AVIA 305 Quiz Maneuvering Performance
AVIA 305 Quiz Maneuvering Performance
Covers the Learn material from Module 5: Week 5 — Module 6: Week 6.
- Dynamic hydroplaning
- Directional control during a crosswind takeoff in a C172 should be maintained with coordinated use of ailerons and the rudder.
- A steep turn during level flight can be considered any bank angle above:
- If an aircraft maintaining a constant bank angle increases its airspeed while maintaining a level, coordinated turn, what will the effect be on the rate of turn (ROT)?
- In Figure 8.12, _____ is the intersection of the acceleration and deceleration proles.
- What effect does a tailwind have on takeoff performance?
- As a rule of thumb, a 5% increase in takeoff distance can be expected for every _______ of uphill slope.
- A common source for runway surface and slope information for a particular airport runway is:
- If wind shear is encountered during takeoff after V1, then:
- (Reference Figure 5.4) What will happen to an aircraft that is own to the right side of the straight vertical line on the right side of the flight envelope?
- When thrust reversers are deployed, a component of thrust now acts as drag.
- Referencing Figure 10.11, what is the indicated stall speed of an airplane with the following
conditions: Gross weight = 2200 lb Flaps = 0°Angle of blank = 40° - Calculate the new stall speed (Vs2) of an airplane when the Vs1 is 52 kts, and the airplane is experiencing a load factor of 3.2 Gs during a level altitude, banked turn.
- An aircraft in which of the following situations is most likely to create the most intense wake turbulence?
- Calculate the new stall speed (Vs2) of an airplane when the Vs1 is 43 kts, and the airplane is experiencing a bank angle of 68° during a level altitude, banked turn.
- An aircraft maintaining 150 knots TAS during a level turn with a bank angle of 22° has the following rate of turn:
- A high roundout during landing may result in:
- An airplane is making a final approach for a landing and encounters a horizontal wind shear. Which of the type of burst below is the most dangerous?
- For an aircraft to spin both wings have to be stalled.
- Takeoff thrust is primarily influenced by what factor(s)
- Angle of attack is the primary control of airspeed in steady flight.
- Calculate the new stall speed (Vs2) of an airplane when the Vs1 is 57 kts, and the airplane is experiencing a bank angle of 47° during a level altitude, banked turn.
- Which of the following is not used in the calculation of accelerate- stop distance?
- When taking off from a high density altitude airport, the ________ will be higher than at sea level.
- Acceleration is inversely proportional to the mass of the aircraft.
- When Tr exceeds Ta, the only way to go is ______________.
- The following is the maximum speed that the aircraft can obtain under normal acceleration and then stop within the predetermined accelerate-stop distance.
- According to Figure 9.11, an equivalent airfoil with aps deployed with have:
- Which statement is true with respect to Lift Coefficient (CL) and the Effect of Sweepback on Coefficient of Lift – Angle of Attack (AOA) curves.
- The no-wind takeoff distance for a turbojet airplane, at sea level on a standard day, is 3,067 ft with a takeoff velocity of 157 kt. If the same airplane departs an airport with a headwind component of 29 kt, assuming all other conditions are the same, what is the new minimum takeoff distance required?