Which of the following is correct according to power producing engines?(a) Airspeed for climb is high than for optimum climb gradient(b) Airspeed for climb is less than for optimum climb gradient(c) Airspeed for climb is equal to optimum climb gradient(d) Airspeed for climb is equal to maximum climb gradientThis question was posed to me by my school teacher while I was bunking the class.My doubt stems from Climb Gradient in division Climb and Descent Performance of Aircraft Performance

Which of the following is correct according to power producing engines

1.	Which of the following is correct according to power producing engines?(a) Airspeed for climb is high than for optimum climb gradient(b) Airspeed for climb is less than for optimum climb gradient(c) Airspeed for climb is equal to optimum climb gradient(d) Airspeed for climb is equal to maximum climb gradientThis question was posed to me by my school teacher while I was bunking the class.My doubt stems from Climb Gradient in division Climb and Descent Performance of Aircraft Performance
Answer» RIGHT answer is (a) Airspeed for climb is high than for optimum climb gradient Easy EXPLANATION: The airspeed for climb is high than for optimum climb gradient in the CASE of power producing engines. The airspeed chosen for after take-off climb should be same as for that of maximum gradient. The safeguard path has a gradient of 2%. The safeguard DISTANCE extends from the take-off distance AVAILABLE on the runway to a distance of 15000m.

Discussion

No Comment Found

Related InterviewSolutions

What is the benefit of flying at minimum power speed?(a) Increases gliding flight time(b) Decreases gliding flight time(c) Does not change the gliding flight time(d) Decreases the aircraft performanceThis question was addressed to me in unit test.My doubt is from Climb and Descent Performance with Thrust-Producing Engines topic in portion Climb and Descent Performance of Aircraft Performance
What is the value that maintains minimum power speed of the aircraft?(a) u/\(\sqrt[4]{3}\)(b) u/\(\sqrt[3]{3}\)(c) u^2/\(\sqrt[4]{3}\)(d) u^2/\(\sqrt[3]{3}\)The question was asked in unit test.My question is based upon Climb and Descent Performance with Thrust-Producing Engines topic in chapter Climb and Descent Performance of Aircraft Performance
Level accelerated is best suitable for thrust producing engines.(a) True(b) FalseI have been asked this question by my college professor while I was bunking the class.This intriguing question comes from Climb and Descent Performance with Mixed Power Plants topic in section Climb and Descent Performance of Aircraft Performance
There are two ways of aircraft descend of an aircraft.(a) True(b) FalseThe question was asked in semester exam.This is a very interesting question from Descent Performance in Aircraft Operations in chapter Climb and Descent Performance of Aircraft Performance
At the back side of the drag curve the rate of change of drag is negative.(a) True(b) FalseI have been asked this question in semester exam.Question is from Descent Performance in Aircraft Operations in chapter Climb and Descent Performance of Aircraft Performance
In practical the climb takes place in three ways.(a) True(b) FalseI have been asked this question in semester exam.Question is taken from Climb Gradient in chapter Climb and Descent Performance of Aircraft Performance
Wind is the relative velocity between the air mass and the ground.(a) True(b) FalseThis question was addressed to me during an interview.The doubt is from Effect of Wind on Climb Performance and Descent Performance topic in section Climb and Descent Performance of Aircraft Performance
The best economic flight is achieved by _________(a) maximum drag(b) minimum speed(c) minimum drag(d) maximum fuel consumptionThis question was addressed to me at a job interview.My question is based upon Climb Rate topic in portion Climb and Descent Performance of Aircraft Performance
What is climb rate?(a) The rate at which the flight take-off the ground(b) Speed at which the flight takes-off(c) Distance required for flight to take-off(d) Fuel required for the take-off of flightThis question was posed to me in homework.My question comes from Climb Rate in section Climb and Descent Performance of Aircraft Performance
What are the factors that affect the economic benefits of fuel climb?(a) Indirect operating costs(b) Direct operating costs(c) Annual pay to the airport(d) Tax payThe question was asked in quiz.This interesting question is from Minimum Fuel Climb topic in portion Climb and Descent Performance of Aircraft Performance

Discussion

No Comment Found

Related InterviewSolutions

Reply to Comment