Explore topic-wise InterviewSolutions in .

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.

Which of the following is not true about an airframe made with carbon-fiber composite?(a) Decreases drag(b) Decreases thrust(c) Higher cabin pressurization(d) Higher wing aspect ratioThe question was posed to me during a job interview.This question is from Fundamentals in division Aircraft Fundamentals of Aircraft Maintenance

Answer» RIGHT OPTION is (B) Decreases thrust

To explain: Carbon-fiber material allows for a lower-drag ALONG with higher wing aspect RATIO and higher cabin pressurization. However, these materials have no effect on thrust.
2.

Airframe of an aircraft is its __________ structure.(a) Electrical(b) Mechanical(c) Thermal(d) HydraulicI got this question in class test.I would like to ask this question from Fundamentals in chapter Aircraft Fundamentals of Aircraft Maintenance

Answer» RIGHT choice is (b) Mechanical

Easiest explanation: The airframe of an aircraft is its mechanical structure. The airframe COMPRISES of the fuselage, wings, and UNDERCARRIAGE and EXCLUDES the propulsion system.
3.

Which was the first commercial aircraft with 50% of its structure weight made of carbon-fiber composite?(a) Boeing 777(b) Boeing 787(c) Boeing 747(d) Airbus A380The question was posed to me in a job interview.I would like to ask this question from Fundamentals in section Aircraft Fundamentals of Aircraft Maintenance

Answer»

Correct CHOICE is (b) BOEING 787

Easy explanation: The Boeing 787 was the FIRST commercial aircraft with 50% of its structure weight made of carbon-fiber composites, along 20% Aluminum and 15% TITANIUM. It first flew in 2009.

4.

Why does the landing gear retract into the wings and/or fuselage during flight?(a) To decrease drag(b) To increase airspeed(c) To decrease airspeed(d) To generate more thrustThis question was posed to me in an international level competition.This interesting question is from Fundamentals topic in section Aircraft Fundamentals of Aircraft Maintenance

Answer»

Right choice is (a) To decrease DRAG

The best I can explain: Aircrafts have landing gear that retract into the wings and/or FUSELAGE to decrease drag during flight. Drag slows down the aircraft, thus increasing the FLYING time between TWO places.

5.

Which of the following is not a part of the airframe?(a) Fuselage(b) Wing(c) Stabilizing tail(d) Landing gearI got this question by my college professor while I was bunking the class.The origin of the question is Fundamentals topic in section Aircraft Fundamentals of Aircraft Maintenance

Answer»

Right OPTION is (d) LANDING gear

Explanation: The main PARTS of the airframe are the fuselage, wing, stabilizing tail and undercarriage. The landing gear is not a part of the airframe.

6.

What material is used for aircraft fuselage?(a) Aluminum alloys(b) Titanium alloys(c) Silver alloys(d) Metal alloysI have been asked this question in homework.I want to ask this question from Fundamentals in section Aircraft Fundamentals of Aircraft Maintenance

Answer»

Right option is (a) Aluminum alloys

The best EXPLANATION: The aircraft fuselage is made of aluminum alloys along with other MATERIALS such as Zn, Mg and Cu. However modern AIRCRAFTS have started using carbon fiber materials in order to decrease the aircraft WEIGHT and in turn increase performance.

7.

Wings are responsible for creating lift.(a) True(b) FalseThis question was addressed to me in my homework.My enquiry is from Fundamentals topic in portion Aircraft Fundamentals of Aircraft Maintenance

Answer»

The correct answer is (a) True

For EXPLANATION: The wings of an aircraft are responsible for PRODUCING lift. MANY different styles and ARRANGEMENTS of wings have been used on heavier than air aircrafts. Some lighter than air aircraft ALSO have wings.

8.

Landing gears are also known as __________(a) Stabilizers(b) Empennage(c) Undercarriage(d) AileronThe question was posed to me in an online quiz.Origin of the question is Fundamentals topic in portion Aircraft Fundamentals of Aircraft Maintenance

Answer»

Right CHOICE is (c) Undercarriage

Explanation: The LANDING gears are ALSO KNOWN as undercarriage. It is the structure that supports an aircraft when it is not flying and allows it to take off, land and taxi.

9.

Which of the following supports an aircraft on the ground?(a) Rudder(b) Engines(c) Aileron(d) Landing gearI got this question in an interview.Origin of the question is Fundamentals in portion Aircraft Fundamentals of Aircraft Maintenance

Answer»

Correct answer is (d) Landing gear

Explanation: Landing gear is the structure that supports an AIRCRAFT when it is not flying and ALLOWS it to MANOEUVRE on the ground. Most commonly, wheels are USED but other equipment such as floats and skids can also be used, depending on the surface.

10.

What do winglets do?(a) Increase thrust(b) Reduce turbulence at the tips of an airplane’s wings(c) Decrease thrust(d) Increase turbulence at the tips of an airplane’s wingsThis question was addressed to me in exam.My question is based upon Fundamentals in portion Aircraft Fundamentals of Aircraft Maintenance

Answer»

The CORRECT choice is (b) Reduce turbulence at the tips of an airplane’s wings

The explanation is: The purpose of winglets is to reduce turbulence at the tips of an airplane’s wings. Winglets and sharklets are SIMILAR to each other. The wingtip vortices created by a LARGE AIRCRAFT are strong enough to flip a smaller aircraft that maybe flying closely. Winglets are responsible to break these vortices thereby reducing drag on the airplane.

11.

Stabilizing tail is also known as __________(a) Rudder(b) Empennage(c) Aileron(d) WingtipThis question was addressed to me during an interview.This is a very interesting question from Fundamentals topic in section Aircraft Fundamentals of Aircraft Maintenance

Answer»

Right choice is (B) Empennage

The EXPLANATION: The stabilizing tail is also KNOWN as the empennage. It is a structure at the rear END of an aircraft that provides stability during flight, in a WAY similar to the feathers on an arrow.

12.

The fuselage of an aircraft contains the engines.(a) True(b) FalseI have been asked this question during an internship interview.This is a very interesting question from Fundamentals topic in division Aircraft Fundamentals of Aircraft Maintenance

Answer»

Correct option is (a) True

The explanation is: The fuselage is an aircraft’s MAIN body SECTION containing the cockpit or flight DECK along with the passenger cabin and CARGO hold. It also often CONTAINS the engine(s).

13.

Which was the first widely produced general aviation aircraft manufactured with all composite construction?(a) Boeing 787(b) Airbus A350(c) Cirrus SR20(d) Bombardier CRJ700This question was addressed to me in an interview.My question comes from Fundamentals in division Aircraft Fundamentals of Aircraft Maintenance

Answer»

Right choice is (c) Cirrus SR20

For explanation: The first widely produced AVIATION aircraft with all COMPOSITE construction was Cirrus SR20. It first FLEW in 1995 and has a cruise speed of 287km/h.

14.

The earliest aircraft were constructed primarily of __________(a) Steel(b) Aluminum(c) Steel(d) WoodThis question was addressed to me in an online interview.The doubt is from Fundamentals in division Aircraft Fundamentals of Aircraft Maintenance

Answer»

Right choice is (d) Wood

The best I can explain: The earliest AIRCRAFT were constructed PRIMARILY of wood. Many newly certified aircraft are BUILT from moulded composite materials, such as CARBON fiber and titanium alloys.

15.

The Rolls-Royce Trent 900 is one of the power plant options for which of the following?(a) Airbus A380(b) Boeing 747(c) Airbus A320(d) Airbus A350This question was posed to me at a job interview.The origin of the question is Fundamentals topic in portion Aircraft Fundamentals of Aircraft Maintenance

Answer» RIGHT choice is (a) Airbus A380

To explain: The Rolls-Royce Trent 900 is a turbofan ENGINE and is one of the power plant OPTIONS available for the Airbus A380. Another power plant option for the A380 is the Engine Alliance GP7000.
16.

The General Electric GE90 is a family of high-bypass __________ aircraft engines.(a) Turboshaft(b) Turboprop(c) Turbojet(d) TurbofanThe question was posed to me in class test.Query is from Fundamentals topic in chapter Aircraft Fundamentals of Aircraft Maintenance

Answer»

Right option is (d) TURBOFAN

To EXPLAIN: The General Electric GE90 is a family of high-bypass turbofan aircraft ENGINES. It is built for the Boeing 777 by GE AVIATION. The engine OFFERS thrust ratings from 81,000 to 115,000 lb.

17.

Which of the following is not a retraction system for landing gear?(a) Hydraulic retraction system(b) Thermal retraction system(c) Manual retraction system(d) Electrical retraction systemThis question was addressed to me during an online interview.My question is taken from Fundamentals topic in portion Aircraft Fundamentals of Aircraft Maintenance

Answer»

Right answer is (b) THERMAL retraction system

The EXPLANATION: AIRCRAFT retraction systems can be manually, electrically or HYDRAULICALLY operated. HOWEVER, there are no thermal retraction systems in aircrafts. The retraction systems are required to reduce drag.

18.

An aircraft engine generates __________ power.(a) Electrical(b) Mechanical(c) Thermal(d) HydraulicThis question was addressed to me in an online quiz.Enquiry is from Fundamentals in portion Aircraft Fundamentals of Aircraft Maintenance

Answer»

The CORRECT option is (B) MECHANICAL

To ELABORATE: An aircraft engine is a COMPONENT of the propulsion system for an aircraft that generates mechanical power. The power generated is used to keep the aircraft flying high in the air.

19.

Which is the largest jet engine in the world?(a) GE90(b) Trent 800(c) PW4000(d) GE9XThis question was addressed to me during an internship interview.I'm obligated to ask this question of Fundamentals in portion Aircraft Fundamentals of Aircraft Maintenance

Answer» CORRECT choice is (d) GE9X

To explain: The GE9X is the largest jet engine in the world, it is as wide as the BODY of a Boeing 737. The engine is MANUFACTURED by General Electric for the Boeing 777X.
20.

A turboprop is very efficient when operated at cruise speed of __________(a) 200-400 mph(b) 20-40 mph(c) 10-100 mph(d) 600-800 mphThe question was asked during an interview.My query is from Fundamentals in division Aircraft Fundamentals of Aircraft Maintenance

Answer»

The correct choice is (a) 200-400 mph

Easy EXPLANATION: Turboprops are extremely efficient when operated at cruise speeds of 200 to 400 mph. This is the ideal cruise speed for such ENGINES, THUS providing such efficiency.

21.

In jet engines the oxygen necessary for fuel combustion comes from the air.(a) True(b) FalseThis question was addressed to me in class test.The above asked question is from Fundamentals topic in portion Aircraft Fundamentals of Aircraft Maintenance

Answer»

Correct option is (a) True

The explanation: True, in jet engines the OXYGEN necessary for fuel combustion comes from the air. The jet engines TAKE in required oxygen through the engine blades and the process of combustion takes PLACE.

22.

How many channels are present in the Cockpit Voice Recorder (CVR)?(a) 4(b) 2(c) 5(d) 3The question was asked at a job interview.My query is from Fundamentals topic in division Aircraft Fundamentals of Aircraft Maintenance

Answer»

The correct answer is (a) 4

The best I can EXPLAIN: There are 4 channels in a commercial type RECORDER. They are Pilot, Co-pilot, CREW, and Centre-Area. The CVR is helpful in probing details of an aircraft crash, in CASE it happens.

23.

The last airliner that used turbojets was the __________(a) Boeing 737(b) Airbus A330(c) Concorde(d) Boeing 767The question was asked during an internship interview.This intriguing question comes from Fundamentals topic in portion Aircraft Fundamentals of Aircraft Maintenance

Answer»

Correct answer is (c) Concorde

The explanation: Concorde was the LAST airliner that USED turbojet. The Mach 2 AIRSPEED offered by Concorde proved the engine to be highly efficient. Other aircrafts could not match such AIRSPEEDS.

24.

Which of the following is not an aircraft engine manufacturer?(a) BMW(b) General Electric(c) Pratt & Whitney(d) Rolls-RoyceI had been asked this question in a national level competition.This key question is from Fundamentals in division Aircraft Fundamentals of Aircraft Maintenance

Answer» RIGHT option is (a) BMW

Easiest explanation: In commercial AVIATION, the MAJOR players in the manufacturing of turbofan engines are PRATT & Whitney, General Electric, Rolls-Royce, and CFM International.
25.

How many types of gas turbine engines are manufactured?(a) 2(b) 4(c) 1(d) 10The question was asked in exam.Question is taken from Fundamentals in section Aircraft Fundamentals of Aircraft Maintenance

Answer»

Correct option is (B) 4

To EXPLAIN: There are FOUR types of gas TURBINE engines: the turbojet, the TURBOFAN, the turboprop, and the turboshaft.

26.

CFM56-3 is a turbofan engine.(a) True(b) FalseI had been asked this question by my college director while I was bunking the class.Origin of the question is Fundamentals topic in section Aircraft Fundamentals of Aircraft Maintenance

Answer» CORRECT OPTION is (a) True

For explanation: The CFM56 series is a family of high-bypass TURBOFAN aircraft engines MADE by CFM International. CFM International is a French-American company headquartered in CINCINNATI, Ohio, United States.
27.

High-bypass turbofans are usually most efficient when the aircraft is traveling at __________(a) 500-550 mph(b) 50-55 mph(c) 20-25 mph(d) 200-250 mphThe question was asked in an international level competition.My question is based upon Fundamentals topic in division Aircraft Fundamentals of Aircraft Maintenance

Answer» RIGHT option is (a) 500-550 mph

Easy explanation: High-bypass turbofans are USUALLY most efficient when the aircraft is traveling at 500 to 550 MILES per hour (800 to 885 km/h) i.e. the CRUISE SPEED of most large airliners.
28.

In general aviation, the dominant manufacturer of turboprop engines has been __________(a) Maserati(b) Pratt & Whitney(c) Boeing(d) AirbusI have been asked this question during an internship interview.The above asked question is from Fundamentals topic in division Aircraft Fundamentals of Aircraft Maintenance

Answer»

Right CHOICE is (b) PRATT & Whitney

Best explanation: In general AVIATION, the dominant manufacturer of turboprop engines has been Pratt & Whitney. However, General Electric in 2015 its ENTRANCE into the market.

29.

Turboshaft engines are used primarily for __________(a) UAVs(b) Commercial aircrafts(c) Cars(d) HelicoptersI had been asked this question during an online interview.This interesting question is from Fundamentals topic in portion Aircraft Fundamentals of Aircraft Maintenance

Answer»

Right answer is (d) Helicopters

For explanation: TURBOSHAFT ENGINES are used PRIMARILY for helicopter. A turboshaft engine is similar to a TURBOPROP in principle, but in turboshaft the engine does not provide any physical support to the helicopter’s rotors.

30.

What is the full form of TEL?(a) Tetraethyllead(b) Tetraethylenelead(c) Tetraethollead(d) TetraethaneleadI had been asked this question during an interview.This interesting question is from Fundamentals in chapter Aircraft Fundamentals of Aircraft Maintenance

Answer»

Correct option is (a) TETRAETHYLLEAD

The BEST I can EXPLAIN: Tetraethyllead (TEL) is blended with aviation gasoline, to be used as a fuel for AIRCRAFTS. The blend increases the fuel EFFICIENCY.

31.

Aircraft AC systems operate on which of the following frequency?(a) 4Hz(b) 40Hz(c) 400Hz(d) 4000HzThis question was posed to me in semester exam.This is a very interesting question from Fundamentals in portion Aircraft Fundamentals of Aircraft Maintenance

Answer» CORRECT ANSWER is (c) 400Hz

Explanation: All aircraft equipment’s using AC power SUPPLY, operates at a frequency of 400Hz. Such relatively HIGH frequency helps in reducing the core size of equipment’s used.
32.

What is the full form of ARINC?(a) Aeronautical Radio, Incorporated(b) Aircraft Radio, Incorporated(c) Aviation Radio, Incorporated(d) Air Radio, IncorporatedI had been asked this question in examination.Origin of the question is Fundamentals topic in chapter Aircraft Fundamentals of Aircraft Maintenance

Answer»

Right choice is (a) Aeronautical Radio, INCORPORATED

Explanation: ARINC refers to Aeronautical Radio, Incorporated. It is owned by Collins Aerospace and was FOUNDED in 1929. It PROVIDES transport communication systems for various industries LIKE AVIATION, defense and healthcare.

33.

The international standards for avionics equipment are prepared by ___________(a) Aircraft Electronic Engineering Committee(b) Airlines Electronic Engineering Committee(c) Aeronautical Electronic Engineering Committee(d) Aerospace Electronic Engineering CommitteeThe question was asked during an interview for a job.My doubt stems from Fundamentals topic in division Aircraft Fundamentals of Aircraft Maintenance

Answer»

The CORRECT answer is (b) Airlines Electronic ENGINEERING Committee

Explanation: The Airlines Electronic Engineering Committee (AECC) is the organization responsible for stating the INTERNATIONAL standards for AVIONICS equipment’s. The equipment also satisfies ARINC standards.

34.

Which of the following is not a manufacturer of aircraft avionics?(a) Thales Group(b) Rockwell Collins(c) GE Aviation systems(d) Mercedes-BenzThe question was posed to me in an online interview.This intriguing question originated from Fundamentals in chapter Aircraft Fundamentals of Aircraft Maintenance

Answer» RIGHT CHOICE is (C) GE Aviation systems

The explanation: Mercedes-Benz is not a manufacturer of aircraft avionics. However, Thales Group, Rockwell Collins and GE Aviation systems all manufacture aircraft avionics. Some other avionic EQUIPMENT manufacturers are BAE systems and Panasonic Avionics CORPORATION.
35.

Radio altimeters are used up to _________(a) 2,500 feet(b) 3,000 feet(c) 250 feet(d) 300 feetThe question was posed to me during an interview for a job.Question is from Fundamentals in section Aircraft Fundamentals of Aircraft Maintenance

Answer» RIGHT option is (a) 2,500 FEET

Easiest explanation: Radio altimeters provide data to the Flight computers, which is then displayed on the Flight DISPLAYS, for the pilots. These altimeters only provide READINGS up to 2,500 feet, above which pressure systems are used to determine the flight altitude.
36.

Which of the following is not a part of avionic systems?(a) Flight Recorder(b) Weather Radars(c) Communication systems(d) EmpennageThe question was posed to me during an online interview.This key question is from Fundamentals in section Aircraft Fundamentals of Aircraft Maintenance

Answer»

Correct answer is (d) Empennage

Best explanation: The empennage acts as a stabilizer and is located on the TAIL of the AIRCRAFT. It is not a part of the avionic systems. However, flight recorders, WEATHER radars and communication systems are all part of the avionic SYSTEM.

37.

The VHF communication system works up to the maximum airband of ___________(a) 106.975 kHz(b) 136.975 kHz(c) 106.975 MHz(d) 136.975 MHzI had been asked this question in unit test.This intriguing question originated from Fundamentals topic in division Aircraft Fundamentals of Aircraft Maintenance

Answer»

The correct choice is (d) 136.975 MHZ

The explanation: Aviation systems USING VHF work between the airband from 118.000 MHz to 136.975 MHz. In Europe, ADJACENT channels are spaced by 8.33 kHz and 25 kHz elsewhere.

38.

Onboard communications on an aircraft are done through public address systems and aircraft intercoms.(a) False(b) TrueThis question was addressed to me during an online interview.The question is from Fundamentals in portion Aircraft Fundamentals of Aircraft Maintenance

Answer»

Right answer is (b) True

To ELABORATE: The onboard COMMUNICATIONS between the pilots and crew, crew and passengers and pilots and passengers are all MADE using aircraft intercoms and onboard communication systems INSTALLED on the aircraft.

39.

Autopilot was first invented by ___________(a) Lawrence Sperry(b) William Boeing(c) Nikola Tesla(d) Wright BrothersI have been asked this question in an interview for internship.My question is based upon Fundamentals in chapter Aircraft Fundamentals of Aircraft Maintenance

Answer»

Right choice is (a) Lawrence Sperry

The best I can explain: The AUTOPILOT feature was invented by Lawrence Sperry. It was introduced during the Second World War to ensue bomber planes fly STEADY enough to HIT PRECISION targets from thousands of feet in the sky.

40.

What is the full form of WAAS?(a) Wide Area Aircraft System(b) Wide Area Augmentation System(c) Wide Aircraft Augmentation System(d) Wide Air Augmentation SystemI have been asked this question by my college director while I was bunking the class.I want to ask this question from Fundamentals topic in chapter Aircraft Fundamentals of Aircraft Maintenance

Answer»

Right CHOICE is (B) Wide Area Augmentation System

The best explanation: WAAS refers to Wide Area Augmentation System. It is an air NAVIGATION system developed by the FAA, DESIGNED to improve the precision of GPS.

41.

Which of the following is not true about LORAN?(a) Expensive(b) Stands for Long Range Navigation(c) Operated at higher frequencies(d) Range up to 1,500 milesThe question was asked in an online quiz.My question comes from Fundamentals topic in division Aircraft Fundamentals of Aircraft Maintenance

Answer»

The CORRECT answer is (c) Operated at higher frequencies

The best I can explain: LORAN refers to Long Range NAVIGATION. It was a system developed during the Second WORLD War in the USA. It was operated at lower frequencies and offered a range up to 1,500 MILES.

42.

Which of the following organizations regulates the safety and reliability standards of avionic and other aircraft equipment, in the USA?(a) DGCA(b) FBI(c) NASA(d) FAAI got this question in homework.Question is from Fundamentals topic in portion Aircraft Fundamentals of Aircraft Maintenance

Answer»

Correct CHOICE is (b) FBI

Easy explanation: The Federal AVIATION Administration regulates the safety and reliability STANDARDS of avionic and other AIRCRAFT EQUIPMENT, in the USA. The regulating authorities are different for other countries in the world. For example, DGCA regulates the safety and reliability standards of avionic and other aircraft equipment in India.

43.

ARINC 708 is a type of ___________(a) Weather radar(b) Satellite(c) Sensor(d) AltimeterI have been asked this question during an internship interview.My question is based upon Fundamentals topic in chapter Aircraft Fundamentals of Aircraft Maintenance

Answer»

Correct option is (a) Weather RADAR

Best explanation: The ARINC 708 is a weather radar USED in commercial AIRCRAFTS. It is not the sole radar used to determine weather conditions around the aircraft, it is supplemented by various other ground SENSING and proximity radars.

44.

Which of the following is used to help pilots fly at low altitudes?(a) Forward looking infrared(b) Terrain-following radar(c) Head-up display(d) ARINC 629This question was addressed to me during an internship interview.This interesting question is from Fundamentals topic in division Aircraft Fundamentals of Aircraft Maintenance

Answer»

Correct option is (B) Terrain-following radar

For explanation I would SAY: Terrain-following radar (TFR) help aircrafts fly at low altitudes. These are FITTED into aircrafts which fly relatively close to the ground at a constant flight level. Such FLIGHTS are SOMETIMES referred to as terrain hugging flights.

45.

Which of the following is a data transfer standard for aircraft avionics?(a) IEEE 1394b(b) ARINC 664(c) MIL-STD-1760(d) ARINC 429The question was posed to me during an online interview.This question is from Fundamentals topic in portion Aircraft Fundamentals of Aircraft Maintenance

Answer»

The CORRECT answer is (d) ARINC 429

To explain I would SAY: The ARINC 429 is a data transfer standard for aircraft avionics. It is an alternative to MIL-STD-1553. It has a self-synchronizing and self-clocking data bus protocol. It has a 32 bit data word.

46.

FMS refers to ___________(a) Fuel management systems(b) Fare management systems(c) Flight management systems(d) Flight managing systemsI have been asked this question during an interview.The doubt is from Fundamentals topic in section Aircraft Fundamentals of Aircraft Maintenance

Answer»

The correct option is (c) Flight management SYSTEMS

Easiest explanation: FMS is an abbreviation for flight management systems. Most commercial aircrafts with autopilot USE FMS, so that the aircraft can KEEP flying without the PILOT’s intervention in some CERTAIN phases of the flight.

47.

A sonobuoy is used to determine the location of enemy missiles.(a) False(b) TrueI got this question by my college professor while I was bunking the class.My enquiry is from Fundamentals in division Aircraft Fundamentals of Aircraft Maintenance

Answer»

The correct answer is (a) False

To EXPLAIN I would SAY: Sonobuoys are used to determine the location of enemy submarines. They are relatively small buoys, which are dropped from aircrafts deployed on underwater research and WARFARE.

48.

Ground-proximity warning systems use ___________ altimeters.(a) Radio(b) Sound(c) Radar(d) PressureThis question was posed to me in a national level competition.Origin of the question is Fundamentals in division Aircraft Fundamentals of Aircraft Maintenance

Answer»

Right choice is (c) Radar

Best explanation: The GROUND-proximity warning systems USE radar altimeters. The GPWS is USED to avoid the aircraft being UNINTENTIONALLY flown into the ground or an obstacle. It improves FLIGHT safety.

49.

Which was the first U.S. jet fighter with twin tails?(a) Lockheed Martin F-35 Lightning II(b) Sukhoi SU-57(c) Sukhoi SU-30(d) Grumman F-14 TomcatI have been asked this question in my homework.I would like to ask this question from Fundamentals topic in section Aircraft Fundamentals of Aircraft Maintenance

Answer»

Correct ANSWER is (d) Grumman F-14 Tomcat

To ELABORATE: The Grumman F-14 Tomcat was the first U.S. jet fighter with TWIN TAILS. It first flew on 21 December 1970 and was deployed with the U.S. NAVY in 1974. The aircraft was retired from the U.S. Navy in September 2006.

50.

What is the full form of TAWS?(a) Terrain awareness warning system(b) Traffic awareness warning system(c) Terrain awareness waking system(d) Traffic awareness waking systemThis question was addressed to me in semester exam.The above asked question is from Fundamentals in portion Aircraft Fundamentals of Aircraft Maintenance

Answer»

The correct choice is (a) Terrain awareness warning system

The explanation: TAWS refers to the Terrain awareness warning system, it may ALSO be called a controlled FLIGHT into terrain. The system is used for avoiding unintended IMPACTS with the GROUND during the FLYING phases.