AVIA 305 QUIZ Aircraft Performance
• Question 1
2.5 out of 2.5 points
The power-required curves for an increase in altitude show that the
Selected Pr increases by the same amount as the velocity
Answer:
• Question 2
2.5 out of 2.5 points
The equation Ta=Q(V2-V1) shows that
Selected Both (a) and (b)
Answer:
• Question 3
2.5 out of 2.5 points
The lowest point on the Pr curve is (L/D)MAX
Selected Fals
Answer: e
• Question 4
2.5 out of 2.5 points
A gas turbine engine that uses most of its power to drive a propeller.
Selected Turboprop
Answer:
• Question 5
2.5 out of 2.5 points
(Reference Figure 7.2) Using Figure 7.2, find the velocity for best range for the airplane at
12,000 lbs.
Selected 325 knots
Answer:
• Question 6
2.5 out of 2.5 points
An engine that utilizes compressed air, via a compressor, to provide sea level performance to
approximately 18,000 feet.
Selected Supercharged
Answer:
• Question 7
2.5 out of 2.5 points
The thrust available from a jet engine at 35,000 ft altitude compared to that at sea level is
Selected Answer:
, Less
• Question 8
0 out of 2.5 points
A propeller where the pilot can adjust the pitch setting in the air. It usually is restricted to either
the takeoff setting or the cruise setting.
Selected Constant speed
Answer:
• Question 9
2.5 out of 2.5 points
• Question 1
2.5 out of 2.5 points
The power-required curves for an increase in altitude show that the
Selected Pr increases by the same amount as the velocity
Answer:
• Question 2
2.5 out of 2.5 points
The equation Ta=Q(V2-V1) shows that
Selected Both (a) and (b)
Answer:
• Question 3
2.5 out of 2.5 points
The lowest point on the Pr curve is (L/D)MAX
Selected Fals
Answer: e
• Question 4
2.5 out of 2.5 points
A gas turbine engine that uses most of its power to drive a propeller.
Selected Turboprop
Answer:
• Question 5
2.5 out of 2.5 points
(Reference Figure 7.2) Using Figure 7.2, find the velocity for best range for the airplane at
12,000 lbs.
Selected 325 knots
Answer:
• Question 6
2.5 out of 2.5 points
An engine that utilizes compressed air, via a compressor, to provide sea level performance to
approximately 18,000 feet.
Selected Supercharged
Answer:
• Question 7
2.5 out of 2.5 points
The thrust available from a jet engine at 35,000 ft altitude compared to that at sea level is
Selected Answer:
, Less
• Question 8
0 out of 2.5 points
A propeller where the pilot can adjust the pitch setting in the air. It usually is restricted to either
the takeoff setting or the cruise setting.
Selected Constant speed
Answer:
• Question 9
2.5 out of 2.5 points
