253 + Interview Questions in Aircraft Systems And Aviation Overview in Aircraft Maintenance Page 2 InterviewSolution

51.	Which of the following is not true about fly by wire systems?(a) Improved safety(b) High maintenance costs(c) Lighter in weight(d) ReliableThis question was posed to me by my school principal while I was bunking the class.Query is from Overview of an Aircraft-2 topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The correct option is (b) High maintenance costs Easy explanation: FLY by wire systems offer low maintenance costs as COMPARED to conventional CONTROLS and also improve efficiency by being LIGHTER in WEIGHT.

Discussion

52.	The tail section is also referred to as __________(a) Undercarriage(b) Cockpit(c) Rudder(d) EmpennageI had been asked this question in final exam.My question is taken from Overview of an Aircraft-2 in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The correct CHOICE is (d) Empennage Easy EXPLANATION: The tail section is also referred to as empennage. It is a structure that provides stability during flying phases. The section INVOLVES both HORIZONTAL and vertical control surfaces.

Discussion

53.	A rotary wing is typically unstable in ________(a) Yaw(b) Roll(c) Pitch(d) BankThe question was posed to me in unit test.Asked question is from Overview of an Aircraft-2 in section Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The CORRECT option is (a) Yaw For explanation: A rotary wing is typically unstable in yaw. Such wings usually require a vertical stabilizer in order to balance the unstable yaw. In CASE the yaw is unbalanced, the aircraft MAY GO out of control and crash.

Discussion

54.	Avionics are generally electrical in nature.(a) True(b) FalseThis question was addressed to me in an online interview.The question is from Overview of an Aircraft-2 in division Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» Correct option is (a) True For EXPLANATION: True, avionics are GENERALLY electrical in nature. Avionic equipment’s have a VITAL role in making modern aircrafts more EFFICIENT and RELIABLE. These equipment’s are costlier as compared to other older equipments.

Discussion

55.	What is the NATO reporting name for Antonov An-225 Mriya?(a) Cossack(b) Dream lifter(c) Dreamliner(d) BelugaThis question was posed to me in class test.This intriguing question originated from Aircraft Systems and Aviation in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The correct answer is (a) Cossack To explain I would say: The NATO reporting name for ANTONOV An-225 Mriya is Cossack. NATO reporting names are CODE names assigned to MILITARY equipment from a certain SET of nations.

Discussion

56.	Which of the following engine type is used to power the Antonov An-225 Mriya?(a) Turboprop(b) Turbojet(c) Turbofan(d) TurboshaftThis question was posed to me in unit test.My enquiry is from Aircraft Systems and Aviation topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» Right choice is (c) Turbofan For EXPLANATION I would SAY: Turbofan engines are used to power the Antonov An-225 Mriya. The aircraft USES six engines and is the heaviest aircraft EVER BUILT.

Discussion

57.	Which of the following is the registration for the single example built of the Antonov An-225?(a) UA-82060(b) UK-82060(c) UR-82060(d) UU-82060I have been asked this question in an interview for job.My question is taken from Aircraft Systems and Aviation in section Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The correct OPTION is (c) UR-82060 For explanation: UR-82060 is the registration for the single example built of the ANTONOV An-225. Only ONE such aircraft has been PRODUCED till date.

Discussion

58.	When was the first Antonov An-225 completed?(a) 1998(b) 1988(c) 2005(d) 2000This question was addressed to me during an interview.The origin of the question is Aircraft Systems and Aviation topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» Right choice is (b) 1988 Easy explanation: The first Antonov An-225 AIRCRAFT was completed in the year 1988 and was produced keeping in mind freight TRANSPORT. This was the only An-225 aircraft ever produced and was BASED on the Antonov An-124.

Discussion

59.	The An-225 is used for commercial operations by __________(a) Qatar Airways(b) FedEx(c) UPS(d) Antonov AirlinesI had been asked this question during a job interview.This is a very interesting question from Aircraft Systems and Aviation topic in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The CORRECT OPTION is (d) ANTONOV Airlines For explanation: The Antonov An-225 aircraft is used for commercial OPERATIONS by Antonov Airlines. The airline is based out of Gostomel Airport in Ukraine. The aircraft is mostly used for CHARTERED freight services.

Discussion

60.	Cargo on the upper fuselage of the An-225 can be 100m long.(a) True(b) FalseThe question was asked during an internship interview.This key question is from Aircraft Systems and Aviation topic in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The correct option is (B) False The best I can explain: False, CARGO on the upper fuselage of the An-225 can be 70m, APPROXIMATELY 230 FEET long. The aircraft can carry ultra-heavy and oversize freight.

Discussion

61.	The An-225 comes with a swept-back horizontal stabilizer.(a) True(b) FalseI got this question in quiz.I want to ask this question from Aircraft Systems and Aviation in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» CORRECT choice is (a) TRUE Explanation: True. The An-225 comes with a swept-back horizontal stabilizer.The aircraft ALSO features a twin tail, which was essential to enable the plane to carry large and heavy EXTERNAL loads.

Discussion

62.	The An-225 landing gear system consists of __________(a) 50 wheels(b) 32 wheels(c) 42 wheels(d) 28 wheelsThe question was asked during an interview.The question is from Aircraft Systems and Aviation topic in section Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» Right ANSWER is (b) 32 WHEELS For explanation: The An-225 landing gear system consists of 32 wheels. The system has a number of steerable wheels which enable the aircraft to turn within a 60-metre-wide runway.

Discussion

63.	The An-225 first flew on __________(a) 21 December 2008(b) 21 December 1998(c) 21 December 1988(d) 21 December 2018I got this question by my school teacher 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» The correct answer is (c) 21 December 1988 Best explanation: The An-225 first flew on 21 December 1988. It was a 74-minute flight from Kiev. The aircraft also flew during the public days at the FARNBOROUGH AIR show in 1990.

Discussion

64.	UR-82060 is registered in Ukraine.(a) True(b) FalseI got this question by my college director while I was bunking the class.My question is from Aircraft Systems and Aviation in division Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The CORRECT choice is (a) TRUE To explain: True, the UR-82060 aircraft is registered in UKRAINE. The aircraft is owned by Antonov AIRLINES, a division of the Antonov AVIATION company.

Discussion

65.	The An-225’s pressurized cargo hold is ________ in terms of volume.(a) 1,300 m^3(b) 1,900 m^3(c) 1,000 m^3(d) 2,000 m^3I have been asked this question during an internship interview.The question is from Aircraft Systems and Aviation topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» RIGHT option is (a) 1,300 m^3 For explanation I WOULD say: The An-225’s pressurized cargo HOLD is 1,300 m^3 in terms of volume. The aircraft is heavier in comparison to the double-decker AIRBUS A380.

Discussion

66.	What is the maximum takeoff weight of the Antonov An-225 Mriya?(a) 640 tons(b) 740 tons(c) 700 tons(d) 400 tonsI have been asked this question in homework.The query is from Aircraft Systems and Aviation topic in section Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» Right answer is (a) 640 tons The best explanation: The ANTONOV An-225 MRIYA has a maximum take-off weight of 640 tons. The take-off weight may also be SPECIFIED as 710 short tons or 630 LONG tons.

Discussion

67.	What is the maximum speed of the An-225?(a) 1,000 km/h(b) 800 km/h(c) 700 km/h(d) 850 km/hThe question was posed to me during an internship interview.This interesting question is from Aircraft Systems and Aviation topic in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The correct ANSWER is (d) 850 km/h Explanation: 850 km/h is the maximum SPEED of the ANTONOV An-225 AIRCRAFT. The aircraft offers a cruise speed of 800 km/h and requires 6 crew members to operate.

Discussion

68.	The An-225 has a service ceiling of __________(a) 10,000 m(b) 15,000 m(c) 11,000 m(d) 9,000 mI have been asked this question by my college director while I was bunking the class.This is a very interesting question from Aircraft Systems and Aviation topic in section Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» RIGHT option is (c) 11,000 m To EXPLAIN I would say: The Antonov An-225 AIRCRAFT has a service ceiling of 11,000 m, which is approximately 36,000 FEET. The aircraft can fly 15,400 km with maximum fuel.

Discussion

69.	What is the wingspan of the An-225?(a) 88.4m(b) 80.4m(c) 90.0m(d) 86.9mThis question was posed to me during an interview for a job.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) 88.4m The EXPLANATION: The Antonov An-225 aircraft has a wingspan of 88.4m. Further, the aircraft measures 84m in length and 18.1 in HEIGHT. It has an ASPECT ratio of 8.6.

Discussion

70.	What is the maximum landing weight of the An-124?(a) 330,000 kg(b) 430,000 kg(c) 530,000 kg(d) 130,000 kgI have been asked this question at a job interview.This intriguing question originated from Aircraft Systems and Aviation topic in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The correct CHOICE is (a) 330,000 KG To elaborate: The An-124 has a MAXIMUM LANDING weight of 330,000 kg, which is approximately 727,525lb. The aircraft has a gross weight of 214,000 kg.

Discussion

71.	The An-124 has a maximum certified altitude of _________(a) 10,000 m(b) 14,000 m(c) 12,000 m(d) 9,000 mThis question was posed to me in a national level competition.This is a very interesting question from Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» Right CHOICE is (c) 12,000 m For explanation: The An-124 has a MAXIMUM certified altitude of 12,000 m, which is approximately 39,000 FEET. The aircraft has a FERRY range of 14,000 km with maximum fuel and minimum payload.

Discussion

72.	Which of the following aircraft is based on the An-124?(a) Airbus A380(b) Boeing 747(c) Antonov An-225 Mriya(d) Airbus BelugaI have been asked this question in an interview for internship.I need to ask this question from Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The CORRECT OPTION is (c) ANTONOV An-225 Mriya Explanation: The Antonov An-225 Mriya is BASED on the An-124. The An-125 is a greatly enlarged design of the An-124 and is the heaviest operating cargo aircraft.

Discussion

73.	When did the An-124 receive civil certification?(a) 30 December 1982(b) 30 December 1992(c) 30 December 1979(d) 30 December 1995I have been asked this question at a job interview.My doubt is from Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» Right answer is (B) 30 December 1992 To elaborate: The An-124 received civil CERTIFICATION on 30 December 1992. It was developed as a heavy transport AIRCRAFT and features FOUR engines.

Discussion

74.	The Antonov An-124 aircraft first took to the skies on __________(a) 24 December 2000(b) 24 December 1909(c) 24 December 1959(d) 24 December 1982This question was addressed to me in an interview for internship.I would like to ask this question from Aircraft Systems and Aviation topic in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» Right ANSWER is (d) 24 December 1982 For EXPLANATION: The ANTONOV An-124 aircraft first took to the skies on 24 December 1982. The aircraft was developed with the motive of transporting heavy MATERIALS around the globe.

Discussion

75.	The An-124’s rear cargo door can open in flight.(a) True(b) FalseThe question was asked at a job interview.This question is from Aircraft Systems and Aviation in section Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» CORRECT answer is (a) True Easy explanation: True, the An-124’s rear cargo door can open in flight. The aircraft features a double FUSELAGE and OPENING of the rear cargo door in flight does not affect its structural integrity.

Discussion

76.	The An-124 is similar to the American Lockheed C-5 Galaxy.(a) True(b) FalseI have been asked this question in a national level competition.My question comes from Aircraft Systems and Aviation topic in section Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» Correct option is (a) True Explanation: True, the An-124 is SIMILAR to the AMERICAN LOCKHEED C-5 GALAXY. This is because both aircrafts share a similar fuselage and door DESIGN.

Discussion

77.	The military variant of the Antonov An-124 can accommodate up to _______ of cargo.(a) 200 tons(b) 100 tons(c) 150 tons(d) 300 tonsThis question was addressed to me in final exam.The query is from Aircraft Systems and Aviation in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» Correct answer is (c) 150 tons The best EXPLANATION: The military variant of the Antonov An-124 aircraft can ACCOMMODATE up to 150 tons of CARGO. The cargo limit may ALSO be specified as 150 LONG tons and 170 short tons.

Discussion

78.	The An-124 features __________ wheels.(a) 50(b) 24(c) 36(d) 40I got this question in an interview.This key question is from Aircraft Systems and Aviation in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» Right answer is (B) 24 Explanation: The Antonov An-124 AIRCRAFT features a TOTAL of 24 wheels. The aircraft can easily land on rough terrains as it is EQUIPPED with the oleo STRUT suspension system.

Discussion

79.	The Antonov An-124 is equipped with an overhead crane.(a) True(b) FalseI got this question in an online quiz.This interesting question is from Aircraft Systems and Aviation in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» Right choice is (a) True Explanation: True, the Antonov An-124 is EQUIPPED with an overhead crane. This onboard crane can lift and winch cargo items WEIGHING up to 30 tons and 120 tons RESPECTIVELY.

Discussion

80.	Which of the following is a proposed variant of the An-124?(a) An-124-130(b) An-124 Ruslan(c) An-124-100(d) An-124-102I got this question by my college professor while I was bunking the class.The doubt is from Aircraft Systems and Aviation topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The correct ANSWER is (a) An-124-130 The explanation: The An-124-130 is a proposed VARIANT of the An-124. An-124 Ruslan is a strategic heavy lift transport aircraft, while the An-124-100 and An-124-102 are both COMMERCIAL VARIANTS.

Discussion

81.	What is the range of the An-124 with maximum payload?(a) 3,700 km(b) 5,700 km(c) 2,000 km(d) 2,500 kmThis question was posed to me in an interview for internship.Asked question is from Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» RIGHT option is (a) 3,700 KM To explain: The An-124 can fly 3,700 km with maximum PAYLOAD. Further, it can fly 8,400 km with 80,000 kg payload or 11,500 km with 40,000 kg payload.

Discussion

82.	What is the maximum speed of the An-124?(a) 650 km/h(b) 600 km/h(c) 1,100 km/h(d) 865 km/hThis question was addressed to me in an international level competition.Question is from Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» CORRECT option is (d) 865 km/h The BEST explanation: The An-124 has a maximum speed of 865 km/h. The aircraft OFFERS cruise speed of 800–850 km/h at Flight LEVEL 328-394.

Discussion

83.	How many passengers can the An-124 carry in a palletized seating arrangement?(a) 800(b) 550(c) 350(d) 100The question was asked in quiz.Question is taken from Aircraft Systems and Aviation in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The correct option is (c) 350 The explanation is: The Antonov An-124 aircraft is CAPABLE of CARRYING about 350 pax in a palletized seating ARRANGEMENT. The aircraft can also HOLD up to 150,000 kg of CARGO.

Discussion

84.	What is the wingspan of the An-124?(a) 73.3m(b) 60.0m(c) 80.50m(d) 86.9mI got this question during an interview.My doubt stems from Aircraft Systems and Aviation topic in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The correct option is (a) 73.3m The BEST explanation: The An-124 has a wingspan of 73.3m. The AIRCRAFT requires a MINIMUM of six CREW members to operate and measures 69.1 m in length.

Discussion

85.	What is the seating layout in a one class An-148-100 aircraft?(a) 2-3(b) 3-3(c) 1-1(d) 2-2I have been asked this question in homework.I would like to ask this question from Aircraft Systems and Aviation topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» RIGHT choice is (a) 2-3 Explanation: The typical seating layout in a one class configuration is 2-3. They can also be CONFIGURED in a multiple class layout which can carry FEWER passengers, TYPICALLY with four abreast business class.

Discussion

86.	The An-148 can carry up to _________ passengers.(a) 120(b) 85(c) 360(d) 25This question was posed to me in an interview for job.I'd like to ask this question from Aircraft Systems and Aviation in section Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The correct answer is (b) 85 For explanation: The An-148 can CARRY up to 85 PASSENGERS. The seating capacity RANGES between 68 to 85 passengers, depending on the aircraft configuration.

Discussion

87.	The An-148 uses ________ engines.(a) Turboprop(b) Turbojet(c) Turbofan(d) TurbopropThis question was addressed to me in an interview for internship.My enquiry is from Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The correct option is (C) Turbofan The best I can explain: The An-148 USES turbofan ENGINES. The aircraft is equipped with two Motor SICH D-436-148 engines, mounted in PODS under the wing.

Discussion

88.	Which of the following is a stretched version of the An-148?(a) Airbus A320(b) Antonov An-225(c) Antonov An-158(d) Airbus A319I got this question during an online interview.This key question is from Aircraft Systems and Aviation topic in section Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The correct answer is (C) Antonov An-158 Explanation: The Antonov An-158 AIRCRAFT is a STRETCHED version of the An-148, the newer An-158 features a stretched fuselage and can seat a maximum of 100 pax in a SINGLE class layout.

Discussion

89.	The An-148-300 is a business variant.(a) True(b) FalseThe question was posed to me in homework.The doubt is from Aircraft Systems and Aviation topic in section Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» Correct OPTION is (a) TRUE The explanation: True, the An-148-300 is a business variant. It was previously called An-168 and can seat up to 40 PASSENGERS, offering a range of up to 7,000 km.

Discussion

90.	The An-148 first flew on ________(a) 17 December 1995(b) 17 December 2000(c) 17 December 2014(d) 17 December 2004The question was asked in final exam.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 (d) 17 DECEMBER 2004 The explanation: The An-148 first flew on 17 December 2004. DEVELOPMENT of the aircraft started in the 1990s and it was CERTIFIED on 26 February 2007.

Discussion

91.	The An-148-100-E has a maximum takeoff weight of __________(a) 75.7 tons(b) 10.7 tons(c) 90.7 tons(d) 43.7 tonsThis question was posed to me in homework.My enquiry is from Aircraft Systems and Aviation topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» Right CHOICE is (d) 43.7 TONS The explanation is: The An-148-100-E has a maximum takeoff weight of 43.7 tons. It is an EXTENDED range VERSION of the An-148 and OFFERS a range of up to 4,400 km.

Discussion

92.	The An-148 has a service ceiling of __________(a) 35,000 feet(b) 40,000 feet(c) 30,000 feet(d) 37,000 feetI had been asked this question in an international level competition.My question is based upon Aircraft Systems and Aviation in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The correct choice is (B) 40,000 FEET For explanation I WOULD say: The An-148 has a SERVICE ceiling of 40,000 feet, which is approximately 12,200m. The aircraft has an ECON cruise altitude of 36,000 feet.

Discussion

93.	Which of the following is a cargo variant of the An-148?(a) An-148-100E(b) An-158(c) An-178(d) An-148-100BcThe question was asked in an online quiz.My question is from Aircraft Systems and Aviation in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The correct option is (C) An-178 The best explanation: The An-178 is a cargo variant of the An-148. The aircraft has a PAYLOAD capacity of 15 TONS and there is an extra pair of main-wheels on each side.

Discussion

94.	The An-148 is equipped with fly-by-wire systems.(a) True(b) FalseI have been asked this question by my school teacher while I was bunking the class.My question is taken from Aircraft Systems and Aviation in section Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» CORRECT answer is (a) True To elaborate: True, the An-148 is equipped with fly-by-wire SYSTEMS. These systems enable the aircraft to operate day and night, under IFR and VFR weather CONDITIONS on high-density air routes.

Discussion

95.	When was the first autopilot developed?(a) 1950(b) 1912(c) 1900(d) 1945The question was asked in an online interview.This question is from Aircraft Systems and Aviation topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» Right choice is (B) 1912 For explanation: The first autopilot was developed in 1912, by SPERRY CORPORATION. The SYSTEM allowed the aircraft to fly straight and level on a compass course without the pilot’s attention.

Discussion

96.	Autopilot system is used to control the __________ of an aircraft.(a) Trajectory(b) Thrust(c) Landing gear(d) Air conditioningThe question was asked in final exam.Asked question is from Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» CORRECT choice is (a) TRAJECTORY Explanation: Autopilot system is used to CONTROL the trajectory of an aircraft. The system eliminates the NEED of constant hands-on control by a human operator.

Discussion

97.	The autopilot is often used in conjunction with the __________(a) Empennage(b) Rudder(c) Auto throttle(d) FlapsThis question was addressed to me by my college director while I was bunking the class.The question is from Aircraft Systems and Aviation topic in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» CORRECT option is (c) Auto throttle To explain: The autopilot is OFTEN used in conjunction with the auto throttle. Auto throttle is the analogous SYSTEM that CONTROLS the power delivered by the engines.

Discussion

98.	Not all passenger aircraft flying today have an autopilot system.(a) True(b) FalseI have been asked this question in homework.Question is taken from Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» Correct answer is (a) True The BEST EXPLANATION: True, smaller and older general aviation AIRCRAFT are STILL HAND flown. Further, small airliner may also be flown without an autopilot as they are operated on short-haul flights with two pilots.

Discussion

99.	Autopilots in modern complex aircraft are __________ axis.(a) One(b) Two(c) Four(d) ThreeI have been asked this question in unit test.My enquiry is from Aircraft Systems and Aviation in section Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» The correct answer is (d) THREE For EXPLANATION: Autopilots in modern complex aircraft are three axis. Three axis control is ESSENTIAL to control the roll, pitch and yaw of an aircraft. The system maybe further divided into DIFFERENT PHASES.

Discussion

100.	What is the full form of CWS?(a) Control Wheel Steering(b) Control Wheel Stoppage(c) Crank Wheel Steering(d) Cross Wheel SteeringThe question was posed to me in homework.My question is based upon Aircraft Systems and Aviation in section Aircraft Systems and Aviation Overview of Aircraft Maintenance
Answer» CORRECT option is (a) Control Wheel Steering For explanation I would say: CWS refers to Control Wheel Steering. It is an option that LIES midway between FULLY automated flight and manual flying. It is STILL used as a function on MANY aircraft today.

Discussion

Explore topic-wise InterviewSolutions in .

The tail section is also referred to as __________(a) Undercarriage(b) Cockpit(c) Rudder(d) EmpennageI had been asked this question in final exam.My question is taken from Overview of an Aircraft-2 in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

A rotary wing is typically unstable in ________(a) Yaw(b) Roll(c) Pitch(d) BankThe question was posed to me in unit test.Asked question is from Overview of an Aircraft-2 in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

Avionics are generally electrical in nature.(a) True(b) FalseThis question was addressed to me in an online interview.The question is from Overview of an Aircraft-2 in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

What is the NATO reporting name for Antonov An-225 Mriya?(a) Cossack(b) Dream lifter(c) Dreamliner(d) BelugaThis question was posed to me in class test.This intriguing question originated from Aircraft Systems and Aviation in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

When was the first Antonov An-225 completed?(a) 1998(b) 1988(c) 2005(d) 2000This question was addressed to me during an interview.The origin of the question is Aircraft Systems and Aviation topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

Cargo on the upper fuselage of the An-225 can be 100m long.(a) True(b) FalseThe question was asked during an internship interview.This key question is from Aircraft Systems and Aviation topic in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

The An-225 comes with a swept-back horizontal stabilizer.(a) True(b) FalseI got this question in quiz.I want to ask this question from Aircraft Systems and Aviation in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

The An-225 landing gear system consists of __________(a) 50 wheels(b) 32 wheels(c) 42 wheels(d) 28 wheelsThe question was asked during an interview.The question is from Aircraft Systems and Aviation topic in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

UR-82060 is registered in Ukraine.(a) True(b) FalseI got this question by my college director while I was bunking the class.My question is from Aircraft Systems and Aviation in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

What is the maximum takeoff weight of the Antonov An-225 Mriya?(a) 640 tons(b) 740 tons(c) 700 tons(d) 400 tonsI have been asked this question in homework.The query is from Aircraft Systems and Aviation topic in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

What is the maximum speed of the An-225?(a) 1,000 km/h(b) 800 km/h(c) 700 km/h(d) 850 km/hThe question was posed to me during an internship interview.This interesting question is from Aircraft Systems and Aviation topic in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

What is the wingspan of the An-225?(a) 88.4m(b) 80.4m(c) 90.0m(d) 86.9mThis question was posed to me during an interview for a job.Origin of the question is Aircraft Systems and Aviation in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

The An-124’s rear cargo door can open in flight.(a) True(b) FalseThe question was asked at a job interview.This question is from Aircraft Systems and Aviation in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

The An-124 is similar to the American Lockheed C-5 Galaxy.(a) True(b) FalseI have been asked this question in a national level competition.My question comes from Aircraft Systems and Aviation topic in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

The military variant of the Antonov An-124 can accommodate up to _______ of cargo.(a) 200 tons(b) 100 tons(c) 150 tons(d) 300 tonsThis question was addressed to me in final exam.The query is from Aircraft Systems and Aviation in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

The An-124 features __________ wheels.(a) 50(b) 24(c) 36(d) 40I got this question in an interview.This key question is from Aircraft Systems and Aviation in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

The Antonov An-124 is equipped with an overhead crane.(a) True(b) FalseI got this question in an online quiz.This interesting question is from Aircraft Systems and Aviation in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

What is the range of the An-124 with maximum payload?(a) 3,700 km(b) 5,700 km(c) 2,000 km(d) 2,500 kmThis question was posed to me in an interview for internship.Asked question is from Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

What is the maximum speed of the An-124?(a) 650 km/h(b) 600 km/h(c) 1,100 km/h(d) 865 km/hThis question was addressed to me in an international level competition.Question is from Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

How many passengers can the An-124 carry in a palletized seating arrangement?(a) 800(b) 550(c) 350(d) 100The question was asked in quiz.Question is taken from Aircraft Systems and Aviation in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

What is the wingspan of the An-124?(a) 73.3m(b) 60.0m(c) 80.50m(d) 86.9mI got this question during an interview.My doubt stems from Aircraft Systems and Aviation topic in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

What is the seating layout in a one class An-148-100 aircraft?(a) 2-3(b) 3-3(c) 1-1(d) 2-2I have been asked this question in homework.I would like to ask this question from Aircraft Systems and Aviation topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

The An-148 can carry up to _________ passengers.(a) 120(b) 85(c) 360(d) 25This question was posed to me in an interview for job.I'd like to ask this question from Aircraft Systems and Aviation in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

The An-148 uses ________ engines.(a) Turboprop(b) Turbojet(c) Turbofan(d) TurbopropThis question was addressed to me in an interview for internship.My enquiry is from Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

The An-148-300 is a business variant.(a) True(b) FalseThe question was posed to me in homework.The doubt is from Aircraft Systems and Aviation topic in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

The An-148 first flew on ________(a) 17 December 1995(b) 17 December 2000(c) 17 December 2014(d) 17 December 2004The question was asked in final exam.This intriguing question comes from Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

The An-148-100-E has a maximum takeoff weight of __________(a) 75.7 tons(b) 10.7 tons(c) 90.7 tons(d) 43.7 tonsThis question was posed to me in homework.My enquiry is from Aircraft Systems and Aviation topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

Which of the following is a cargo variant of the An-148?(a) An-148-100E(b) An-158(c) An-178(d) An-148-100BcThe question was asked in an online quiz.My question is from Aircraft Systems and Aviation in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

The An-148 is equipped with fly-by-wire systems.(a) True(b) FalseI have been asked this question by my school teacher while I was bunking the class.My question is taken from Aircraft Systems and Aviation in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

When was the first autopilot developed?(a) 1950(b) 1912(c) 1900(d) 1945The question was asked in an online interview.This question is from Aircraft Systems and Aviation topic in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

Autopilot system is used to control the __________ of an aircraft.(a) Trajectory(b) Thrust(c) Landing gear(d) Air conditioningThe question was asked in final exam.Asked question is from Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

Not all passenger aircraft flying today have an autopilot system.(a) True(b) FalseI have been asked this question in homework.Question is taken from Aircraft Systems and Aviation topic in portion Aircraft Systems and Aviation Overview of Aircraft Maintenance

Autopilots in modern complex aircraft are __________ axis.(a) One(b) Two(c) Four(d) ThreeI have been asked this question in unit test.My enquiry is from Aircraft Systems and Aviation in section Aircraft Systems and Aviation Overview of Aircraft Maintenance

What is the full form of CWS?(a) Control Wheel Steering(b) Control Wheel Stoppage(c) Crank Wheel Steering(d) Cross Wheel SteeringThe question was posed to me in homework.My question is based upon Aircraft Systems and Aviation in section Aircraft Systems and Aviation Overview of Aircraft Maintenance