AVIA 305 Test 2
AVIA 305 Test 2
Answered
User
Course 202040 Fall 2020 AVIA 305-D01
LUO
Test Test 2
Status Completed
Attempt Score 67.5 out of 75
points
• Question 1
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 2
2.5 out of 2.5 points
If the weight of a jet airplane is increased then
Selected Induced drag increases more than parasite drag
Answer:
• Question 3
2.5 out of 2.5 points
An example of a power-producing aircraft is a
Selected King Air 90 turboprop
Answer:
• Question 4
2.5 out of 2.5 points
Which horsepower is the usable horsepower for reciprocating engines?
Selected
Answer: Thrust horsepower
• Question 5
2.5 out of 2.5 points
(Reference Figure 7.2) Using Figure 7.2, find the velocity for maximum endurance for the
airplane at 12,000 lbs.
Selected
Answer: 255 knots
, AVIA 305 Test 2
• Question 6
AVIA 305 Test 2
Answered
User
Course 202040 Fall 2020 AVIA 305-D01
LUO
Test Test 2
Status Completed
Attempt Score 67.5 out of 75
points
• Question 1
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 2
2.5 out of 2.5 points
If the weight of a jet airplane is increased then
Selected Induced drag increases more than parasite drag
Answer:
• Question 3
2.5 out of 2.5 points
An example of a power-producing aircraft is a
Selected King Air 90 turboprop
Answer:
• Question 4
2.5 out of 2.5 points
Which horsepower is the usable horsepower for reciprocating engines?
Selected
Answer: Thrust horsepower
• Question 5
2.5 out of 2.5 points
(Reference Figure 7.2) Using Figure 7.2, find the velocity for maximum endurance for the
airplane at 12,000 lbs.
Selected
Answer: 255 knots
, AVIA 305 Test 2
• Question 6
