This set of Aircraft Performance Multiple Choice Questions & Answers (MCQs) focuses on “Climb Gradient”. 1. What is departure path? a) A path of no obstructions b) Runway path c) Apron area d) Passenger terminal 2. The departure path in an airport is depended on _________ a) size of the runway b) size of the … Read more
This set of Aircraft Performance Multiple Choice Questions & Answers (MCQs) focuses on “Climb and Descent Performance with Mixed Power Plants”. 1. Which of the following is the correct performance equation for mixed power-plants? a) Emaxsinγ2= b) Emaxsinγ2= c) Emaxsinγ2= d) Emaxsinγ2= 2. The best gradient of climb is attained at _____________ a) airspeed below … Read more
This set of Aircraft Performance Questions and Answers for Aptitude test focuses on “Climb and Descent Performance with Power-Producing Engines”. 1. The propulsive force developed by the engine-propeller combination is given by _______ a) b) c) d) 2. The gradient of climb is given by _____________ a) =sinγ2 b) =sinγ2 c) =sinγ2 d) =sinγ2 3. … Read more
This set of Aircraft Performance Multiple Choice Questions & Answers (MCQs) focuses on “Climb and Descent Performance with Thrust-Producing Engines”. 1. Which of the following is the correct thrust balancing equation for thrust producing engines? a) FN+D=Wsinγ2+mV̇ b) FN-D=Wsinγ2+mV̇ c) FN-D=Wsinγ2-mV̇ d) FN+D=Wsinγ2-mV̇ 2. Which of the following is the correct lift balancing equation for … Read more
This set of Aircraft Performance Multiple Choice Questions & Answers (MCQs) focuses on “Cruising Performance – Aircraft with Mixed Power Plants”. 1. What is a turboprop? a) It is a combination of turbojet and ramjet b) It is a combination of turbojet and turbofan c) It is a combination of turbojet and scramjet d) It … Read more
This set of Aircraft Performance Multiple Choice Questions & Answers focuses on “Range and Endurance for Aircraft with Power Producing Engines”. 1. Which of the following is the correct performance equation for power-producing engines? a) ηV=PD b) ηD=PV c) ηP=VD d) V=ηPD 2. What is the unit of specific fuel consumption? a) kg/kW-sec b) kg/W-hr … Read more
This set of Aircraft Performance Multiple Choice Questions & Answers (MCQs) focuses on “Effect of WAT on Cruise Performance”. 1. The range factor is proportional to the square root of the initial cruising weight. a) True b) False 2. Which of the following is a correct statement? a) Increase in initial weight of aircraft implies … Read more
This set of Aircraft Performance MCQs focuses on “Cruising Performance – Effect of Alternative Fuel Flow Laws”. 1. The range and endurance are proportional to which of the following factors? a) fuel flow b) net thrust c) bypass ratio d) airspeed 2. Which of the following is a correct form of fuel flow? a) C=C2θMn … Read more
This set of Aircraft Performance Multiple Choice Questions & Answers (MCQs) focuses on “Cruise Method 3”. 1. Which factor must be reduced in cruise method 3? a) Mach number b) Angle of attack c) Altitude d) Temperature 2. Which of the following indicates the range formula in cruise method 3? a) R= b) R= c) … Read more
This set of Aircraft Performance Multiple Choice Questions & Answers (MCQs) focuses on “Cruise Method 2”. 1. Which factor must be reduced in constant angle of attack and constant altitude method? a) Mach number b) Angle of attack c) Altitude d) Temperature 2. Which of the following indicates the range formula in cruise method 2? … Read more
