Related InterviewSolutions

• An airliner with take-off gross weight of 2100kg is cruising with fuel weight fraction of 0.280. Then, what will be the weight of fuel (Wf)?(a) 588kg(b) 588lb(c) 90kg(d) 28lbI got this question during an interview for a job.The doubt is from Conceptual Sketch Sizing in portion Conceptual Sketch Sizing of Aircraft Design
• According to FAA, general aviation aircraft requires reserved fuel in terms of _____(a) additional cruise fuel of half hour(b) additional climb fuel(c) no provision is mentioned in FAA(d) additional taxi-way fuel of three hoursI got this question at a job interview.Origin of the question is Conceptual Sketch Sizing topic in portion Conceptual Sketch Sizing of Aircraft Design
• Avionics systems are an example of ____ weight.(a) empty(b) crew(c) passenger(d) payloadThe question was posed to me in a job interview.My query is from Conceptual Sketch Sizing topic in division Conceptual Sketch Sizing of Aircraft Design
• What will be the weight fraction of the aircraft at final mission segment w.r.t. W0?(a) Multiplication of individual weight fraction(b) Division of individual weight fraction(c) Addition of individual weight fraction(d) Subtraction of individual weight fractionThis question was posed to me in an interview.The origin of the question is Conceptual Sketch Sizing in division Conceptual Sketch Sizing of Aircraft Design
• Mission leg fuel fraction is defined by _____(a) weight at end of the phase to that of at the begin(b) weight at end of the phase to that of at the begin(c) weight of phase at the begin(d) weight at end of the phaseI had been asked this question in an interview.I want to ask this question from Conceptual Sketch Sizing in division Conceptual Sketch Sizing of Aircraft Design
• The “Design take-off gross weight” and “maximum take-off weight” are always interchangeable.(a) True(b) FalseThis question was posed to me in an international level competition.This key question is from Conceptual Sketch Sizing topic in section Conceptual Sketch Sizing of Aircraft Design
• Total fuel weight of aircraft is ______(a) mission fuel only(b) sum of mission fuel, reserve fuel and trapped fuel(c) sum of trapped and mission fuel(d) reserved fuel onlyI had been asked this question in an international level competition.This interesting question is from Conceptual Sketch Sizing in portion Conceptual Sketch Sizing of Aircraft Design
• Which of the following is the correct pair?(a) Empty weight fraction is similar to gross weight of the aircraft(b) Empty weight fraction is inversely proportion to gross weight of the aircraft(c) Empty weight fraction is directly proportion to gross weight of the aircraft(d) Empty weight fraction is not related with the gross weight of the aircraftThe question was asked during an interview for a job.The above asked question is from Conceptual Sketch Sizing in chapter Conceptual Sketch Sizing of Aircraft Design
• A Jet transport aircraft is flying with crew load of 175kg, payload of 1400kg and fuel weight of 500kg. Find out Fuel to empty weight fraction, if design take-off gross weight of the aircraft is 5600lb.(a) 1.076(b) 0.1831(c) 0.196(d) 0.1418I got this question during an interview.Question is from Conceptual Sketch Sizing topic in portion Conceptual Sketch Sizing of Aircraft Design
• A prop-driven aircraft having fuel weight of 650kg. Now, aircraft is taxing on runway, after which it has fuel fraction of 0.975. Determine fuel used during taxing of aircraft, if W0 = 5000kg.(a) 225kg(b) 125kg(c) 221kg(d) 125.65lbThe question was posed to me by my college professor while I was bunking the class.This intriguing question comes from Conceptual Sketch Sizing in division Conceptual Sketch Sizing of Aircraft Design