Aircraft Performance Questions and Answers – Effect on the Take-off Distances of Flight Variables

This set of Aircraft Performance Questions and Answers for Campus interviews focuses on “Effect on the Take-off Distances of Flight Variables”. 1. There are two atmospheric effects on the take-off distances. a) True b) False 2. Which of the following is the correct formula of ground run distance with respect to aircraft weight? a) SG= … Read more

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Aircraft Performance Questions and Answers – Estimation of Take-off Distances

This set of Aircraft Performance Multiple Choice Questions & Answers (MCQs) focuses on “Estimation of Take-off Distances”. 1. What are the additional forces acting on the aircraft? a) Runway friction b) Lift c) Thrust d) Power 2. Which of the following are the correct equations for take-off run? a) FN+D-WsinγR-μrR=mV̇ b) R-L=WcosγR c) R-L=WsinγR d) … Read more

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Aircraft Performance Questions and Answers – Take-off Performance

This set of Aircraft Performance Multiple Choice Questions & Answers (MCQs) focuses on “Take-off Performance”. 1. What is meant by minimum control speed ground? a) The airspeed below which the rudder the will not be capable of producing a yawing moment b) The airspeed below which the rudder the will not be capable of producing … Read more

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Aircraft Performance Questions and Answers – Types of Take-off and Landing

This set of Aircraft Performance Multiple Choice Questions & Answers (MCQs) focuses on “Types of Take-off and Landing”. 1. What are the terminal phases of the aircraft landing? a) Take-off b) Landing c) Take-off and landing d) En-route 2. The terminal phases consist of two parts. a) True b) False 3. What is engine failure … Read more

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Aircraft Performance Questions and Answers – High Performance Climb

This set of Aircraft Performance Multiple Choice Questions & Answers (MCQs) focuses on “High Performance Climb”. 1. If ETS is 400kts, what is the acceleration associated with it? a) 40kts/min b) 4000kts/min c) 4kts/min d) 400kts/min 2. Specific total energy is ________ a) the potential energy per unit mass b) the kinetic energy per unit … Read more

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Aircraft Performance Questions and Answers – Effect of Wind on Climb Performance and Descent Performance

This set of Aircraft Performance Questions and Answers for Entrance exams focuses on “Effect of Wind on Climb Performance and Descent Performance”. 1. Wind is the relative velocity between the air mass and the ground. a) True b) False 2. The aircraft is taken to the level ground operating for ________ a) considering vertical component … Read more

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Aircraft Performance Questions and Answers – Descent Performance in Aircraft Operations – 2

This set of Aircraft Performance Question Bank focuses on “Descent Performance in Aircraft Operations – 2”. 1. The flight control cannot be alone handled by the elevator alone at the backside of drag curve. a) True b) False 2. What measures are taken to maintain precise control of flight path gradient? a) Elevator settings alone … Read more

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Aircraft Performance Questions and Answers – Descent Performance in Aircraft Operations – 1

This set of Aircraft Performance Multiple Choice Questions & Answers (MCQs) focuses on “Descent Performance in Aircraft Operations – 1”. 1. In what proportion should the propulsive thrust be so that the aircraft will decelerate? a) Thrust is less than airframe drag b) Thrust is more than airframe drag c) Greater airspeed d) Less airspeed … Read more

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Aircraft Performance Questions and Answers – Minimum Fuel Climb

This set of Aircraft Performance Multiple Choice Questions & Answers (MCQs) focuses on “Minimum Fuel Climb”. 1. Which of the following is the formula for specific climb? a) SC= b) SC= c) SC=c d) SC= 2. The unit of specific heat is ft/kg. a) True b) False 3. What is the value of specific climb … Read more

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Aircraft Performance Questions and Answers – Climb Rate

This set of Aircraft Performance Multiple Choice Questions & Answers (MCQs) focuses on “Climb Rate”. 1. Which of the following is the correct safe height of an aircraft? a) 20000m b) 15000m c) 30000m d) 40000m 2. The operating height is achieved by maximum rate climb. a) True b) False 3. The best economic flight … Read more

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Manish Bhojasia - Founder & CTO at Sanfoundry
Manish Bhojasia, a technology veteran with 20+ years @ Cisco & Wipro, is Founder and CTO at Sanfoundry. He is Linux Kernel Developer & SAN Architect and is passionate about competency developments in these areas. He lives in Bangalore and delivers focused training sessions to IT professionals in Linux Kernel, Linux Debugging, Linux Device Drivers, Linux Networking, Linux Storage, Advanced C Programming, SAN Storage Technologies, SCSI Internals & Storage Protocols such as iSCSI & Fiber Channel. Stay connected with him @ LinkedIn | Youtube | Instagram | Facebook | Twitter