By changing the bending of attack of a wing, the airplane pilot can control the aeroplane's: a. Lift and airspeed, but not drag b. Elevator, gross weight and drag c. Elevator, airspeed and drag d. Lift and drag, but non airspeed
Last Answer : c. Lift, airspeed and elevate
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To maintain altitude, what must be done as Indicated Airspeeed (IAS) is reduced? a. Decrease bending of attack to reduce the elevate b. Increment angle of attack to maintain the right lift force c. Deploy the speed brakes to increase drag d. Reduce thrust
Terminal Reply : b. Increase angle of set on to maintain the correct elevator strength
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If the angle of attack is increased beyond the disquisitional bending of set on, the wing volition no longer produce sufficient lift to back up the weight of the shipping: a. Unless the airspeed is greater ... beneath the natural horizon d. In which case, the control cavalcade should be pulled-back immediately
Terminal Answer : b. Regardless of airspeed or pitch attitude
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What flight status should be expected when an aircraft leaves ground effect? a. A decrease in parasite elevate permitting a lower angle of attack b. An increment induced drag and a requirement ... increase in dynamic stability d. A subtract in induced elevate requiring a smaller angle of attack
Terminal Answer : b. An increase induced drag and a requirement for a higher angle of attack
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At a constant mass and altitude, a lower airspeed requires: a. More thrust and a lower coefficient of lift b. Less thrust and a lower coefficient of lift c. More thrust and a lower coefficient of elevate d. A higher coefficient of elevator
Last Reply : d. A higher coefficient of elevator
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What phenomenon causes induced elevate? a. Wing tip vortices b. Wing tanks c. The increased pressure level at the leading edge
Last Answer : a. Wing tip vortices
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Which statement is true regarding the opposing forces interim on an aeroplane in steady-state level flight? a. Thrust is greater than drag and weight and lift are equal b. These forces are equal ... greater than weight d. Thrust is slightly greater than lift, but the drag and weight are equal
Last Answer : b. These forces are equal
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What true airspeed and angle of attack should be used to generate the same corporeality of lift as distance is increased? a. A college truthful airspeed for whatsoever given angle of attack b. The aforementioned truthful ... c. A lower true airspeed and higher angle of attack d. A constant bending of set on and true airspeed
Last Respond : a. A higher true airspeed for any given angle of attack
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Which statement best describes the operating principle of a constant-speed propeller? a. As throttle setting is changed past the pilot, the prop governor causes pitch bending of the propeller blades to ... the pilot, the RPM of the engines remains constant every bit the pitch bending of the propeller changes
Last Reply : b. The propeller command regulates the engine RPM and in turn the propeller RPM
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What effect does attribute ratio have on induced drag? a. Increased aspect ratio increases induced elevate b. Increased aspect ratio reduces induced drag c. Changing attribute ratio has no upshot on induced drag d. Induced drag volition equal one:three ten aspect ratio/chord ratio
Last Respond : b. Increased attribute ratio reduces induced drag
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If flaps are lowered during the take-off run: a. The lift would not change until the aircraft is airborne b. The lift would increase when the flaps are lowered c. The lift would decrease d. The acceleration would increase
Last Reply : b. The lift would increase when the flaps are lowered
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To recover from a spin, the elevators should exist: a. Moved up to increase the angle of attack b. Moved down to reduce the bending of attack c. Set to neutral d. Allowed to float
Last Respond : b. Moved downward to reduce the angle of set on
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When would the negative differential limits be reached/exceeded? a. Rapid descent when AC descends below cabin altitude b. During ground pressure testing c. Rapid ascent when aircraft climbs d. When changing to manual operation
Last Answer : a. Rapid descent when AC descends beneath cabin altitude
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If airbrakes are extended during a glide, and speed maintained, the rate of descent will: a. Increment and glide angle will be steeper b. Increase only glide angle volition remain the same c. Subtract d. Remain the aforementioned
Last Answer : a. Increment and glide bending will exist steeper
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You are flying at a abiding FL 290 and a constant mach number. The full temperature increases by 5°. The CAS will: a. Remain approximately constant b. Increase past 10 kts c. Subtract by 10 kts d. Will increase or decrease depending on whether you lot are to a higher place or beneath ISA
Final Respond : a. Remain approximately constant
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Two aircrafts, 1 with a abrupt fly profile (Southward) and the other with a thick contour (T), are flying through the same deject with the same true airspeed. The deject consists of pocket-size ... aircrafts accumulate water ice due to the small size of droplets d. Shipping S experiences more icing than T
Last Answer : d. Shipping Southward experiences more icing than T
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What is the recommended technique to counter the loss of airspeed and resultant elevator from wind shear? a. Maintain, or increase, pitch attitude and accept the lower-than-normal airspeed ... shaker, and utilize maximum ability d. Accelerate the aircraft to prevent a stall by sacrificing altitude
Last Answer : c. Avoid overstressing aircraft, pitch to stick shaker, and apply maximum power
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Which stall has the greatest bending of set on? a. Depression speed stall b. Loftier speed stall (stupor stall) c. Deep stall d. Accelerated stall
Last Answer : c. Deep stall
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The bending of attack of a stock-still pitch propeller: a. Depends on forward speed only b. Depends on forward speed and engine rotational speed c. Depends on engine rotational speed simply d. Is constant for a fixed pitch propeller
Last Answer : b. Depends on forward speed and engine rotational speed
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What factors affect descent angle in a glide? a. Configuration and distance b. Configuration and angle of attack c. Mass and altitude d. Mass and configuration
Last Answer : b. Configuration and angle of attack
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An inversion is: a. A subtract of pressure with height b. A decrease of temperature with tiptop c. An increment of temperature with acme d. An increase of pressure level with height
Final Answer : c. An increase of temperature with height
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At a abiding mass and distance, a lower airspeed requires: a. More thrust and a lower coefficient of lift b. Less thrust and a lower coefficient of lift c. More thrust and a lower coefficient of elevate d. A higher coefficient of elevator
Final Reply : d. A higher coefficient of lift
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What is the purpose of inboard ailerons? a. To reduce wing angle at high speed b. To reduce wing twisting at low speed c. To reduce wing angle at depression speed d. To reduce fly twist at high speed
Last Answer : d. To reduce wing twist at high speed
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Whenever a plate is held immersed at some angle with the direction of catamenia of the liquid, it is subjected to some pressure. The component of this pressure, in the direction of flow of the liquid, is known every bit (A) Lift (B) Elevate (C) Stagnation pressure level (D) Bulk modulus
Concluding Answer : Reply: Pick B
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The maximum induced drag occurs at a speed of: a. VMD b. VMP c. VSO d. VATO
Last Answer : c. VSO
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The best EAS/Elevate ratio is approximately: a. 1.three VMD b. one.32 VMD c. 1.6 VMD d. 1.8 VMD
Terminal Answer : b. 1.32 VMD
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When does THRUST = Elevate? a. Climbing at a constant IAS b. Descending at a abiding IAS c. Flight level at a constant IAS d. All of the above
Last Answer : c. Flying level at a constant IAS
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CAS is IAS corrected for: a. Position and instrument mistake b. Instrument, pressure level, and density fault c. Relative density only d. Compressibility
Last Answer : a. Position and instrument error
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How tin the airplane pilot increase the rate of turn and subtract the radius at the same time? a. Shallow the banking company and increment airspeed b. Steeper bank and increase airspeed c. Steeper bank and decrease airspeed
Last Answer : c. Steeper banking company and decrease airspeed
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Shortly after take-off, the altitude of the airplane suffers an abrupt pitch-up and IAS apace decreases followed quickly by a decrease in altitude. Engine indications are normal. You should suspect what ... to gain airspeed d. Local articulate air turbulence; reduce speed to VRA and ride it out
Concluding Answer : b. Loss of head wind or an increase in tail wind; apply full power
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What is normally the most effective measure to reduce or avoid True cat effects? a. Alter of flight level b. Change of course c. Increase of speed d. Decrease of speed
Last Answer : a. Alter of flight level
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With an almost discharged bombardment at that place will be: a. A decrease of voltage with increasing load b. Increase of electric current with decrease of voltage c. Decrease of current with increasing load d. Increase of voltage with increasing load
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A pilot suffering from decompression sickness should: a. Descend to a lower level where the symptoms will disappear and continue the flying at this or a lower level b. Decrease the cabin pressure level ... the hurting in the affected site d. Country as soon as possible and seek medical aid
Last Reply : d. Country as presently as possible and seek medical assist
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Disorientation is more likely when the airplane pilot is: one. flying in VMC 2. ofttimes irresolute between within and exterior references 3. flying from IMC to VMC 4. approaching over still water at dark a. one, ii & ... ane, 2 & 4 only are correct c. one, two, 3 & 4 are right d. one only is right
Last Answer : b. 1, ii & 4 only are right
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The minimum content of a readback of the message from ATC "X-CD Change FREQUENCY TO STEPHENVILLE Belfry 118.7" is: a. 118.7 b. Changing FREQUENCY X-CD c. TO STEPHENVILLE Ten-CD d. 118.7 X-CD
Concluding Answer : d. 118.seven X-CD
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Which of the following statement is an interpretation of the SIGMET? LSAW SWITZERLAND 0307 SIGMET 2 VALID 030700/031100 LSSW mod to sev cat fcst north of alps btn fl 260 and fl 380 / ... towards the surface area north of the Alps. Intensity increasing. Pilots advised to cantankerous this expanse higher up FL260
Terminal Answer : c. Moderate to severe clear air turbulence to be expected north of the Alps. Intensity increasing. Danger zone between FL260 and FL380
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The VOR indications on an RMI whose deviation is not zero: a. Are magnetic b. Are compass c. Are relative d. Must have departure practical before existence used
Terminal Answer : a. Are magnetic
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How will an oncoming aircraft on a line of constant bearing announced visually? a. There will be no relative movement and it will appear to be very small until seconds before the collision ... relative movement and it will appear to be very modest until seconds before the aircraft passes well clear
Last Reply : a. There will be no relative move and it will appear to be very modest until seconds before the standoff
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Mostly, as altitude increases: a. Temperature decreases and density increases b. Temperature, pressure and density decreases c. Temperature and pressure increase and density decreases d. Temperature decreases and pressure level and density increase
Last Respond : b. Temperature, pressure and density decreases
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The furnishings of carbon monoxide: a. Increases with altitude b. Decreases with distance c. Increases with increase of density d. Decreases with pressure loss
Last Reply : a. Increases with altitude
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Selection up the correct statement from the following: (A) Coefficient of compressibility is the decrease in void ratio per unit increase of pressure (B) The percent settlement at any time is called degree of consolidation (C) Time factor is a dimensionless quantity (D) All the above
Last Answer : Reply: Option D
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If the ailerons are deflected to x°, compared to 5°, this will cause: a. An increased angle of bank b. An increased charge per unit of curlicue c. No modify to either banking company angle or roll rate d. A reduction in the adverse yawing moment
Last Answer : b. An increased rate of roll
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To give the best obstacle clearance on take-off, take-off should be made with: a. Flaps partially extended and at best rate of climb speed (Vy) b. Flaps partially extended and at best bending of climb ... at best rate of climb speed (Vy) d. Flaps retracted and at all-time angle of climb speed (Vx)
Last Reply : d. Flaps retracted and at best bending of climb speed (Vx)
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Which of the following increases the stall angle? a. Slats b. Flaps c. Spoilers d. Ailerons
Last Reply : a. Slats
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What is the effect of deploying leading edge flaps? a. Increased minimum glide angle b. Decreased minimum glide angle c. Increased glide range d. Decreased sink rate
Terminal Answer : d. Decreased sink charge per unit
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Lowering the flaps during a landing approach: a. Increases the bending of descent without increasing the airspeed b. Decreases the angle of descent without increasing power c. Eliminates floating d. Permits approaches at a higher indicated airspeed
Last Answer : a. Increases the angle of descent without increasing the airspeed
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The method of alighting the airplane on water during a ditching is to: a. Carry out a normal approach with flaps and gear selected as normal but to calculate all speeds plus 10kts b. Reduce ... d. Fly a normal approach to stalling speed and and then drop the plane vertically onto the water
Terminal Answer : c. Fly a normal approach merely go on the gear upward and land at lowest possible speed with the nose raised for the tail to strike beginning
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An aircraft is travelling at 120 kts, what angle of bank would be required for a charge per unit one(1) turn? a. thirty° b. 12° c. 18° d. 35°
Last Answer : c. eighteen°
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Y'all are cruising at FL 200, OAT is -forty°C, sea level pressure is 1033 hPa. Calculate the true distance. a. xx,660 ft b. 21,740 ft c. eighteen,260 ft d. 19, 340 ft
Last Answer : d. 19, 340 ft
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A stall warning device must be set to operate: a. At the stalling speed b. At a speed just beneath the stalling speed c. At a speed about 5% to 10% above the stalling speed d. At a speed about 20% to a higher place the stalling speed
Last Answer : c. At a speed about five% to ten% above the stalling speed
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