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Q: Height of Glide slope at the middle marker is 200

Q: Radio Altimeter determines Aircraft height by the principle of Frequency Modulation

Q: A torsion stress is caused by?a) Bending

b) Twistingc) Stretching

Q: The five principal factors, which affect the magnitude of lift and drag of anairplane wing, are?a) angle of attack, gross weight, lift coefficient, shape of the airfoil and wind velocityb) Angle of attack, shape of the airfoil, wing area, airspeed, air densityc) Angle of attack, shape of the airfoil, aspect ratio, coefficient of lift, gross weight

Q: The best lift/drag ratio is achieved when?

a) Gliding for maximum range?b) Gliding for maximum endurance?c) Climbing at the best angle of climb airspeed?

Q: Missed approach in an approach using ASR, will be initiated at what place?a) DHb) MDAc) MAP

Q: A/c performance during Take off when tail wind sheer, Wind condition prolongthe Wake Terbulence on Landing Runway for the longest period of time?a) With quarterly light tailwindb) With quarterly light x-wind?

Q: At night as the sides of the hills or mountains cool, the air in contact withthem tends to become denser and blows down the slope into the valley. This windis calleda) Anabatic windb) Mountain windc) Katabatic wind

Q: During approach, Haze can give illusion of?

Q: Force that exactly opposes and balance lift in climb isa) Weight X Cos q angle of attack

Q: IN nil wind conditions, climb gradient is 3.5%, Height gained is 560, Horizontal distance covered =??

Q: Other then the pressure, what factors control the True Altitude of A/c?b) Mean Sea Level Pressurec) Mean Sea Level Temperatured) Lapse Rate

Q: Type of icing with smallest size of water dropletsa) Rime iceb) Glaze ice

Q: The Tropopause is lower:a) In summer then in winterb) Over the Equator than then over the North Pole

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c) Over the North Pole then Over the Equatord) South of the Jet Stream then North of it

Q: Density altitude will be equal to Pressure altitude when?a) Standard temperature conditions exist?b) At Sea Level

Q: Density altitude is?a) Altitude of A/c with reference to Standard datum planeb) Pressure altitude corrected for non-standard temp conditions?

Q: At FL 350, a decrease in Mach .1 results in a decrease of TAS of 49Kts. Findthe Local Speed of Sound and OAT?

Q: The efficiency with which the spring rotor will remain align with a given datum is dependent upon the rotor mass being?a) Concentrated at a great radius as possibleb) Concentrated as close to the axis of spin as possible

Q: Real Wander of gyro can be caused by?a) Asymmetric friction at the spin axisb) Earths rotation beneath the Gyroscope

Q: Center of Aerodynamics?a) Moves forward with increase in angle of attack?b) Moves backwards with increase in angle of attack?c) Remains unchanged?

Q: When you cross International Date Line from West to Easta) LMT decreases and Date Increasesb) LMT increases and Date Decreases

Q: An A/c weighs 125,000 Kg. It qualifies as?a) Heavyb) Mediumc) Lights

Q: Center of Pressure is the point where?a) All the lift is concentrated

Q: Aspect Ratio is the Ratio between the?b) Wing span and mean chord line

Q: A/c on Final approach intercept G/s 3.5% at a distance of 3 NM with a half fly up deflection (on 4 Dot indicator), Elevation of Airport is 500, find Height ofA/c?

Q: A/c Take off from Tokyo (+8:00 UTC) at 5:00 LMT for LA (-11:00 UTC) and reaches LA at LMT 10:00, find flight time and date?

Q: Scale at 60 degree N = 1:1000000, find scale at 30 degree S?

Q: Rhumb Line is?c) A curved line which cuts all the Meridians at same angle

Q: Longitudinal stability of A/c isd) Defines the Pitch movement

e) Is along the lateral axis if A/cf) All of the above

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Q: Transonic speed isa) Below 1 Machb) Between .75 Mach to 1.2 Machc) 1.2 Mach to 5 Machd) 5 Mach or above

Q: Radio Altimeter works on

a) SHFb) UHFc) VHF

Q: GPS consist of constellations ofa) 24 Satellitesb) 21 Satellitesc) 6 Satellites

Q: Flashing white lights to an A/c on Taxiway meansa) Come back to the point of Start

Q: Sigmets are valid for a period ofb) 2 hoursc) 4 hoursd) 6 hours

Q: A/c TAS = 200, Headwind =50 Kts, distance=400NM, Time to C.P.?

Q: Skin drag increases witha) Increase in airspeedb) Decrease in airspeedc) Not related to airspeed

Q: The fuel is drawn from the carburetor float chamber into the engine by meansofa) A fuel pumpb) An acceleration pumpc) A venturi effectd) A turbocharger

Q: Type of Leading Edge Flapsa) Slatsb) Kreuger Flapsc) Both a and b

Q: You are taking off on Runway 05, winds are from 290 at 20 Kts, you are experiencinga) 10 Kts of Tailwindb) 10 Kts of Headwindc) 17 Kts of X-windd) None of the above

Q: In METAR, Visibility above 6 SM and No clouds below 5000, is termed asa) CAVOK

Q: Coarse pitch; in reference to a propellerb) Is used to take off

c) Also is known as Increase RPMd) Is used for Cruisee) Should be selected for landing

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Q: TAF is applicable toa) Area of 50 NM from Airportb) Area of 10 NM from Airportc) Area of 5 NM from Airportd) None of the above

Q: The volume of the cylinder at the bottom of the compression stroke compared to the volume at the top of the stroke is called?a) The mean effective pressureb) The Volumetric efficiencyc) The Piston displacementd) The compression ratio

Q: Pressure Altitude =200, OAT =20 degree, Density Altitude=??

Q: V1 Speed is?

Q: One disadvantage of Swept wings is that?

a) Its wingtips stall ahead of roots

Q: In a steady flight, when speed decreases, we increase pitch tob) Compensate for loss of Liftc) To Provide more lift then drag

Q: The angle of Attack is the angle between Chord Line anda) The relative windb) Longitudinal Axis

Q: At the 0 degree angle of Attack the pressure over the upper wing will bea) Lower then atmospheric pressureb) Grater then atmospheric pressure

c) Equal to the atmospheric pressure

Q: Which one is not a Great Circle?a) All Meridiansb) Equatorc) 38 degree North Latitude

Q: How does rainwater affect aerodynamics of A/c?

Q: Agonic are lines ofa) Equal Variationb) Zero Variationc) Zero Deviation

Q: How many lines can be drawn between 2 Points on Earth, which are not diametrically opposite?a) 1b) Infinite

Q: DME is a?a) Primary Radarb) Secondary Radar

Q: What is Dutch Roll?

Q: What is Optimum Altitude?

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Q: What is Flat Rate Engine?

Q: Wet Start is a state of Engine, when an Engine?

Q: The Primary Emergency for which DCP is computed isa) Engine Failureb) Unavailability of Destination Airport

c) Fuel Shortaged) Emergency on Board

Q: The maximum deflection in RVSM allowed isa) 60b) 100c) 200d) 20

Q: The Secretary to Minister of Civil Aviation in India is?

Q: The new Monogram of Air India is?

Q: After the merger of Air India and Indian Airlines, the new name given to thecombined company is?

Q: The relative wind has an effect on thea) Angle of incidenceb) Angle of Attackc) Coefficient of Dragd) Asymmetric Thrust

Q: When the angle of attack of the wing is increased to the point where the wingstalls, the center of pressure willa) Move rearward and then forward

b) Move forwardc) Move forward and then rearwardd) Remain Stationary

Q:

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