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This section includes InterviewSolutions, each offering curated multiple-choice questions to sharpen your knowledge and support exam preparation. Choose a topic below to get started.

1.

When did the Concorde enter service?(a) 21 January 2000(b) 21 January 1999(c) 21 January 1959(d) 21 January 1976I have been asked this question during an interview for a job.Asked question is from Aircraft Systems and Aviation topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Correct option is (d) 21 January 1976

To explain: The CONCORDE aircraft entered into service on 21 January 1976. The aircraft FLEW for 27 years and was withdrawn from commercial service due to VARIOUS reasons. The aircraft was capable of flying at supersonic SPEEDS.

2.

What does the word Concorde mean?(a) Flight(b) War(c) Harmony(d) SupersonicI have been asked this question in an online quiz.My question is taken from Aircraft Systems and Aviation topic in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Correct answer is (C) Harmony

Explanation: Concorde is a French word, which has an ENGLISH equivalent, concord. The AIRCRAFT has been named after this word. Both words MEAN harmony or unity.

3.

The Concorde was jointly developed and manufactured under an _________ treaty.(a) Arab-French(b) Anglo-British(c) Anglo-French(d) Arab-BritishThe question was posed to me during an online exam.This question is from Aircraft Systems and Aviation topic in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Right ANSWER is (C) Anglo-French

To explain: The Concorde was jointly DEVELOPED and MANUFACTURED under an Anglo-French treaty, by Sud Aviation and the British Aircraft Corporation.

4.

How much did the Concorde program cost?(a) £1.3 billion(b) £1.3 million(c) £70 billion(d) £70 millionThe question was posed to me in class test.Question is taken from Aircraft Systems and Aviation topic in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Right CHOICE is (a) £1.3 billion

For explanation: The Concorde program costed £1.3 billion. HOWEVER, the ORIGINAL program cost estimate was of £70 million. Huge OVERRUNS and delays resulted in such extreme costs.

5.

Apart from the Concorde, which of the following is one of only two supersonic transports that has been operated commercially?(a) Airbus A380(b) Tupolev Tu-144(c) MD 80(d) Boeing 777This question was posed to me in quiz.The origin of the question is Aircraft Systems and Aviation in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer» RIGHT answer is (b) TUPOLEV Tu-144

Explanation: The Tupolev Tu-144 and Concorde are the only two supersonic TRANSPORTS that have been OPERATED COMMERCIALLY. The Tupolev Tu-144 operated in the late 1970s.
6.

Which of the following is not an operator of the Concorde?(a) Air France(b) Air India(c) British Airways(d) Singapore AirlinesI have been asked this question during a job interview.My question is based upon Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Correct choice is (b) AIR India

Best EXPLANATION: Air India is not an operator of the Concorde. However, Air FRANCE, British Airways and Singapore Airlines were operators of the Concorde. Singapore Airlines had ONE aircraft on short TERM lease.

7.

The Concorde 001 made its first test flight from Toulouse on 2 March 1969.(a) True(b) FalseThe question was posed to me in my homework.This interesting question is from Aircraft Systems and Aviation in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Correct choice is (a) True

For EXPLANATION: True, the AIRCRAFT flew its first test flight on 2 March 1969. The aircraft flew from Toulouse in FRANCE and numerous checks were performed during the test flight.Further, the first supersonic flight by the CONCORDE was on 1 October 1969.

8.

Which of the following was not a launch customer of the Concorde?(a) Air France(b) BOAC(c) Emirates(d) Pan-AmThis question was posed to me by my college director while I was bunking the class.My question comes from Aircraft Systems and Aviation in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The correct CHOICE is (c) Emirates

The best I can explain: Emirates was not a LAUNCH customer of the CONCORDE. HOWEVER, Pan Am, BOAC, and Air France were the launch customers, with six Concorde’s each.

9.

Concorde is an ogival delta winged aircraft.(a) True(b) FalseI had been asked this question in an interview for job.I'd like to ask this question from Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The correct choice is (a) True

Easy explanation: True, the Concorde is an ogee delta winged aircraft. The aircraft is EQUIPPED with four OLYMPUS engines, based on those employed in RAF’s Avro Vulcan STRATEGIC BOMBER.

10.

The Concorde did not have auxiliary power unit,(a) True(b) FalseI have been asked this question during an online interview.I want to ask this question from Aircraft Systems and Aviation topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The correct answer is (a) TRUE

The explanation is: True, the Concorde did not have auxiliary POWER unit. This is because the AIRCRAFT would only VISIT large AIRPORTS where ground air start carts are available.

11.

What was the maximum speed of the Concorde?(a) Mach 2.04(b) Mach 0.24(c) Mach 1.5(d) Mach 24I got this question by my college director while I was bunking the class.Origin of the question is Aircraft Systems and Aviation in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The correct ANSWER is (a) Mach 2.04

To explain I WOULD say: The Concorde had a maximum speed of Mach 2.04, at CRUISE altitude. It OFFERED a cruise speed of Mach 2.02 for OPTIMUM fuel consumption.

12.

The Concorde had seating for up to ________ passengers.(a) 428(b) 28(c) 228(d) 128This question was addressed to me during an internship interview.This is a very interesting question from Aircraft Systems and Aviation topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Right option is (d) 128

Easy explanation: The Concorde had seating for 92 to 128 passengers. The AIRCRAFT was primarily used by WEALTHY passengers who could pay a HIGH price in RETURN for the aircraft’s speed and luxury service.

13.

Which of the following developed Concorde’s thrust-by-wire engine control system?(a) BAE Systems(b) Ultra Electronics(c) General Electronics(d) Rolls-RoyceI had been asked this question in an internship interview.I'm obligated to ask this question of Aircraft Systems and Aviation topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Correct ANSWER is (b) Ultra Electronics

The best EXPLANATION: The thrust-by-wire engine control SYSTEM used on the Concorde AIRCRAFT was developed by Ultra Electronics. All pilots flying the Concorde had to undergo rigorous trainings that LASTED for months.

14.

The Concorde airframe was designed for life off ________ flying hours.(a) 45,000(b) 4,500(c) 450(d) 4,50,000This question was addressed to me by my school teacher while I was bunking the class.My question comes from Aircraft Systems and Aviation topic in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Correct choice is (a) 45,000

To elaborate: The AIRCRAFT’s airframe was designed for life off 45,000 flying hours. The aircraft went through TWO cycles of HEATING and cooling during a flight, FIRSTLY cooling down as it gained altitude, then heating up after going SUPERSONIC.

15.

What was the maximum temperature that aluminum could sustain over the life of the aircraft?(a) 1000 ℃(b) 1270 ℃(c) 100 ℃(d) 127 ℃I have been asked this question in my homework.Origin of the question is Aircraft Systems and Aviation in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Correct option is (d) 127 ℃

Easiest explanation: Aluminium MATERIAL could sustain a maximum temperature of about 127 ℃ (Approximately 261 ℉) over the COMPLETE LIFE of the aircraft. Such temperature limitations in TURN decreased the top speed of the aircraft.

16.

When any aircraft passes the critical Mach of that particular airframe, the centre of pressure shifts ________(a) Rightwards(b) Leftwards(c) Rearwards(d) FrontwardsThis question was posed to me in a job interview.This intriguing question comes from Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The correct choice is (C) Rearwards

To EXPLAIN I would say: The centre of pressure SHIFTS rearwards when any aircraft passes the critical Mach of that particular AIRFRAME. This phenomenon causes a pitch down moment on the aircraft, if the centre of GRAVITY still remains where it was.

17.

The aircraft’s tires are rated to a maximum speed of ________ on the runway.(a) 50 mph(b) 25 mph(c) 250 mph(d) 500 mphThe question was asked in semester exam.The doubt is from Aircraft Systems and Aviation in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Right OPTION is (c) 250 mph

Best explanation: The aircraft’s tires are rated to a MAXIMUM speed of 250 mph, approximately 400 km/h on the runway. The UNDERCARRIAGE had to be UNUSUALLY strong because of the way Concorde’s delta wing GENERATED lift.

18.

What was Concorde’s maximum cruising altitude?(a) 50,000 feet(b) 40,000 feet(c) 30,000 feet(d) 60,000 feetI got this question in an interview for job.This intriguing question originated from Aircraft Systems and Aviation in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Right answer is (d) 60,000 feet

To EXPLAIN: The Concorde offered a significantly HIGH maximum CRUISING altitude of 60,000 feet, which is approximately 18,000 m. It may also be noted that most SUBSONIC aircrafts have cruise altitudes under 44,000 feet.

19.

When the radiation levels became a bit too high, the aircraft had to descend below __________(a) 4,700 feet(b) 47,000 feet(c) 3,700 feet(d) 37,000 feetThis question was posed to me by my college director while I was bunking the class.Question is from Aircraft Systems and Aviation topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The correct ANSWER is (b) 47,000 FEET

The best I can explain: When the radiation levels became a bit too high, the aircraft had to descend below 47,000 feet. This was done in order to silence certain speculations on the aircraft, which SAID supersonic travel may increase the chances of skin CANCER.

20.

The Concorde had livery restrictions.(a) True(b) FalseThe question was asked by my college director while I was bunking the class.This intriguing question comes from Aircraft Systems and Aviation in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer» CORRECT choice is (a) True

Best explanation: True, the aircraft had certain livery restrictions. A major portion of the aircraft was supposed to be painted white, so as to avoid over HEATING of the airframe DUE to EFFECTS of SUPERSONIC flight.
21.

What was Concorde’s normal landing speed?(a) 170 miles per hour(b) 1,700 miles per hour(c) 100 miles per hour(d) 1,000 miles per hourI have been asked this question by my college professor while I was bunking the class.My doubt is from Aircraft Systems and Aviation in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The CORRECT answer is (a) 170 miles per hour

Best explanation: Concorde’s normal landing speed was 170 miles per hour, which is approximately 274 km/h. The AIRCRAFT adopted a higher ANGLE of attack at LOW SPEEDS than conventional aircraft.

22.

When did Air France’s final Concorde flight take place?(a) 27 June 2000(b) 27 June 2003(c) 27 June 2009(d) 27 June 1998I had been asked this question by my college professor while I was bunking the class.My question is based upon Aircraft Systems and Aviation in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Correct choice is (b) 27 June 2003

For EXPLANATION: Air France’s FINAL Concorde FLIGHT took place on 27 June 2003, when F-BVFC retired to Toulouse. The airline made its final commercial Concorde landing in New York City from Paris on 30 May 2003.

23.

Which of the following developed the brakes for Concorde?(a) General Electric(b) BAE Systems(c) Boeing(d) DunlopThe question was posed to me during an interview.Asked question is from Aircraft Systems and Aviation in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer» RIGHT choice is (d) Dunlop

The EXPLANATION: Brakes for the Concorde were DEVELOPED by Dunlop, a tire manufacturer having its headquarters in the United States. Further, the Concorde was the FIRST aircraft to feature carbon based brakes.
24.

Concorde required a minimum of ________ runway length.(a) 4,000 feet(b) 6,000 feet(c) 7,000 feet(d) 5,000 feetI had been asked this question in an interview.Enquiry is from Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Correct answer is (b) 6,000 feet

The EXPLANATION is: Concorde REQUIRED a minimum of 6,000 feet runway length. Although, this was considerably LESS than the SHORTEST runway Concorde ever actually LANDED on.

25.

The final flight of a Concorde worldwide took place on 26 November 2003.(a) True(b) FalseThis question was posed to me by my college professor while I was bunking the class.I want to ask this question from Aircraft Systems and Aviation in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Right option is (a) True

The explanation: True, the final FLIGHT of a CONCORDE, worldwide TOOK place on 26 NOVEMBER 2003. The aircraft landed at Filton, Bristol in the United Kingdom.

26.

Concorde offered a range of ___________(a) 5,900 nautical miles(b) 300 nautical miles(c) 3,900 nautical miles(d) 500 nautical milesThis question was posed to me during a job interview.I want to ask this question from Aircraft Systems and Aviation in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Right answer is (C) 3,900 NAUTICAL MILES

To explain I WOULD say: Concorde offered a range of 3,900 nautical miles, which is approximately 7,223 kilometres. The aircraft had a service ceiling of 60,000 feet.

27.

The soviet Tupolev Tu-144 was nicknamed Concordski.(a) True(b) FalseThe question was posed to me in examination.This interesting question is from Aircraft Systems and Aviation in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The correct CHOICE is (a) True

To explain: True, the soviet Tupolev Tu-144 was NICKNAMED CONCORDSKI. It was NAMED as such by western European JOURNALISTS, due to its outward similarity to Concorde.

28.

How long was the wing span of Concorde?(a) 84 feet(b) 80 feet(c) 70 feet(d) 100 feetI have been asked this question in my homework.This intriguing question originated from Aircraft Systems and Aviation topic in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Correct CHOICE is (a) 84 feet

To EXPLAIN: The wing span of Concorde was 84 feet long. The aircraft had a HEIGHT of 40 feet and measured 202 feet 4 INCHES in length.

29.

Which of the following is the most extensive check to be performed on an aircraft?(a) Category A-Check(b) Category B-Check(c) Category D-Check(d) Category C-CheckThis question was addressed to me in an internship interview.The doubt is from Overview of an Aircraft-1 in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Correct choice is (c) CATEGORY D-CHECK

To explain: Category-D check is the most extensive check to be performed on an AIRCRAFT, it may also be referred to as Heavy Maintenance Visit. Such checks are performed every 5 to 6 YEARS and require a tremendous amount of manpower.

30.

Flight Data Recorder is also known as __________(a) Orange Box(b) Black Box(c) Red Box(d) Green BoxThe question was posed to me during an online exam.This key question is from Overview of an Aircraft-1 topic in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The correct option is (b) Black Box

Best explanation: FLIGHT data recorder or commercial aircraft cockpit data RECORDERS are also COMMONLY referred as a black box. These recorders store flight information and AUDIO from the aircraft cockpit.

31.

What is the full form of MRO?(a) Maintenance, repair and overhaul(b) Maintenance, repair and organization(c) Maintain, repair and overhaul(d) Maintain, repair and organizationThis question was addressed to me in an interview for internship.This intriguing question originated from Overview of an Aircraft-1 topic in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The correct choice is (a) MAINTENANCE, repair and OVERHAUL

For explanation: AIRCRAFT maintenance, repair and overhaul (MRO) is an ESSENTIAL requirement to ensure that AIRCRAFTS are maintained in pre-determined conditions of airworthiness in order to safely fly around the globe.

32.

Which of the following is the most frequently conducted check on an aircraft?(a) Category C-Check(b) Category A-Check(c) Category B-Check(d) Category D-CheckThis question was posed to me in an online interview.The doubt is from Overview of an Aircraft-1 in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer» CORRECT OPTION is (B) Category A-Check

To elaborate: Category A-check is performed approximately every 500 – 800 flight hours. The check NEEDS about 20 man hours and is usually performed overnight at an airport gate. All other category checks are more extensive.
33.

Aircraft equipment’s operate at _________(a) 350Hz(b) 450Hz(c) 400Hz(d) 40HzI had been asked this question in a job interview.This interesting question is from Overview of an Aircraft-1 topic in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The correct option is (c) 400Hz

Best explanation: Aircraft equipment’s operate at 400Hz. The equipment operates at high FREQUENCY in ORDER to reduce their core size, THUS being lighter and more EFFICIENT.

34.

Which of the following indicates an aircraft’s rotation about its longitudinal axis?(a) Turn Indicator(b) Pitch Indicator(c) Yaw Indicator(d) Bank indicatorThis question was posed to me in semester exam.Question is taken from Overview of an Aircraft-1 in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer» CORRECT choice is (a) TURN Indicator

The best explanation: The turn indicator INDICATES an AIRCRAFT’s rotation about its longitudinal axis. The instrument INCLUDES Turn-and-Slip Indicator and the Turn Coordinator.
35.

What is the frequency range of VHF?(a) 30 MHz to 300 MHz(b) 30 Hz to 300 Hz(c) 30 KHz to 300 KHz(d) 30 mHz to 300 mHzI got this question during a job interview.This intriguing question comes from Overview of an Aircraft-1 in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer» CORRECT answer is (a) 30 MHz to 300 MHz

To ELABORATE: Very high FREQUENCY (VHF) is the radio frequency range from 30 MHz to 300 MHz.Frequencies immediately below VHF are denoted high frequency and the next higher frequencies are known as ultra-high frequency.
36.

Which of the following bodies regulates civil aviation in India?(a) DGCA(b) EASA(c) FAA(d) CASAThis question was posed to me by my school teacher while I was bunking the class.I'd like to ask this question from Overview of an Aircraft-1 topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer» RIGHT answer is (a) DGCA

The best I can EXPLAIN: DGCA is the flight regulation authority in India. FAA, EASA and CASA are the flight regulation authorities in the USA, EUROPE and Australia respectively.
37.

Radio altimeters are used only up to _________(a) 2500 feet(b) 3000 feet(c) 250 feet(d) 300 feetI got this question in final exam.My query is from Overview of an Aircraft-1 in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The correct choice is (a) 2500 FEET

Easy explanation: Radio altimeters are capable of determining the flight altitude only up to 2,500 feet above ground level. These DEVICES send DATA to the auto throttle, which in turn processes by MEANS of flight COMPUTERS.

38.

The Airbus A380 is equipped with three engines.(a) False(b) TrueI had been asked this question in an interview.I need to ask this question from Overview of an Aircraft-1 in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The CORRECT option is (b) True

For EXPLANATION: False, the AIRBUS A380 is equipped with four engines. It is a wide body, double decker aircraft that is mainly OPERATED on long haul routes.

39.

Which of the following is not a part of the “big five” instruments?(a) Altimeter(b) Airspeed indicator(c) Head up display(d) Artificial HorizonThe question was asked in a national level competition.This intriguing question originated from Overview of an Aircraft-1 topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer» CORRECT choice is (c) HEAD up display

For explanation: The head up display is not a part of the “big five” instruments. The five instruments in the “big five” are ALTIMETER, Airspeed indicator, vertical speed indicator, ARTIFICIAL horizon and HEADING indicator.
40.

Which of the following is a part of the tail assembly of an aircraft?(a) Spoilers(b) Edge flaps(c) Slats(d) StabilizerThis question was addressed to me during an internship interview.My enquiry is from Overview of an Aircraft-1 topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The correct option is (d) STABILIZER

The best explanation: The stabilizer are a part of the tail assembly of an aircraft. Spoilers, edge FLAPS and SLATS are located on the wing of an aircraft.

41.

Radar systems use which of the following waves?(a) Ultrasonic(b) Radio(c) Nuclear(d) ElectronicI had been asked this question in exam.Question is from Overview of an Aircraft-1 in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Correct choice is (b) RADIO

To explain: The RADAR SYSTEMS use radio waves. These are systems designed to DETERMINE parameters like the RANGE, angle, or velocity of different objects.

42.

How are the electronic signals transmitted in a FBW system?(a) Manually(b) Using radars(c) Using sensors(d) Using wiresI had been asked this question in exam.My question comes from Overview of an Aircraft-2 in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The CORRECT OPTION is (d) Using WIRES

To explain I would say: The electronic signals are transmitted using wires, in a FBW system. In order to transmit these flight CONTROLS, they need to be first converted into electronic signals.

43.

Which of the following aircraft holds the record for the fastest recorded powered aircraft flight?(a) Lockheed SR-71 Blackbird(b) Sukhoi 30(c) Concorde(d) NASA X-43A PegasusThis question was posed to me during an interview.My query is from Overview of an Aircraft-2 in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The correct option is (d) NASA X-43A Pegasus

Easy explanation: The NASA X-43A Pegasus aircraft HOLDS the record for the FASTEST recorded powered aircraft flight. The aircraft broke its own world record of Mach 6.3 set in March 2004.

44.

Conventional flight control systems require pilot’s involvement.(a) True(b) FalseThis question was posed to me during an interview.My doubt is from Overview of an Aircraft-2 in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The correct choice is (a) True

Explanation: True, the CONVENTIONAL flight CONTROL systems require pilot’s involvement. HOWEVER, modern FLY by wire systems do not require the pilot’s involvement, and hence reduce workload.

45.

Which of the following is the world’s largest airliner?(a) Airbus A350(b) Airbus A320(c) Airbus A380(d) Airbus A340The question was posed to me in a job interview.I'm obligated to ask this question of Overview of an Aircraft-2 topic in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer» RIGHT OPTION is (c) AIRBUS A380

The best I can explain: The Airbus A380 is the world’s largest airliner. The first A380 prototype was unveiled in Toulouse, France on 18 JANUARY 2005, with its first flight on 27 April 2005.
46.

Which of the following is the largest aircraft by weight?(a) Boeing 777(b) Antonov An-225 Mriya(c) Airbus A380(d) MD 80I had been asked this question by my school teacher while I was bunking the class.Query is from Overview of an Aircraft-2 topic in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The CORRECT choice is (b) Antonov An-225 Mriya

The best EXPLANATION: The Antonov An-225 Mriya is the LARGEST aircraft by weight. It is ALSO the largest regular fixed-wing aircraft ever built. The aircraft is equipped with six engines.

47.

Engine fuel is usually stored in the wings but some aircraft have additional fuel tanks in the ________(a) Undercarriage(b) Tail(c) Fuselage(d) NoseThe question was asked by my school principal while I was bunking the class.My question is taken from Overview of an Aircraft-2 in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

The CORRECT choice is (c) Fuselage

The best EXPLANATION: Engine fuel is USUALLY STORED in the wings but some aircraft have additional fuel TANKS in the fuselage. Generally, larger aircrafts, like the A380 have these additional fuel tanks.

48.

Control systems are sometimes also used to increase or decrease ________(a) Altitude(b) Airspeed(c) Drag(d) ThrustI have been asked this question in final exam.My question is from Overview of an Aircraft-2 topic in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Right option is (c) DRAG

For explanation: The control systems are SOMETIMES also used to increase or decrease drag. ONE such application is SLOWING the aircraft to a SAFE speed for landing.

49.

Yaw is a rotation about the ________ axis.(a) Vertical(b) Longitudinal(c) Horizontal(d) DiagonalThe question was posed to me in an online interview.Question is taken from Overview of an Aircraft-2 topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer» CORRECT answer is (a) VERTICAL

The explanation: Yaw is a rotation about the vertical axis. It GIVES a side-to-side movement of the NOSE KNOWN as sideslip. The yaw axis is one of the three principle axes of an aircraft.
50.

Pitch of an aircraft is based on its angle of attack.(a) True(b) FalseI got this question by my college professor while I was bunking the class.My doubt is from Overview of an Aircraft-2 in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

Answer»

Correct answer is (a) TRUE

Easiest explanation: True, the pitch of an AIRCRAFT is based on its angle of attack. It gives an up down MOVEMENT of the aircraft NOSE measured by the angle of attack.