PER atpl

Which of the following statements is correct?. If any clearway is present it must be reduced to no greater distance than the stopway. The TODA is always longer than the TORA. The TORA is 50% of the TODA as a declared distance making the TORA 1.5 times the TODA. The maximun clearway that can be used is limited to 50% of the TORA making the TODA 150% of the TORA.

What effect has a downhill slope on the Take-Off speeds? The slope: Decreases the TAS for take-off. Has no effect on the take-off speed V1. Increases the IAS for take-off. Decreases the take-Off speed V1.

The drift down procedure specifies requirements concerning the: Obstacle clearance after engine failure. Climb gradient during the descent to the net level-off altitude. Weight during landing at the alternate. Engine power at the altitude at wich engine failure occurs.

During a descent at constant Mach Number, the margin to low speed buffet will. Increase, because the lift coefficient decreases. Decreases, because the lift coefficient decreases. Remain constant, because the Mach number remains constant. Increase, because the lift coefficient increases.

The angle of attack required to attain the maximum still-air range for a turbo-jet airplane is: Less than that for the maximum lift to drag ratio. The same as that giving zero induced drag. Greater than that for the maximun lift to drag ratio. The same as for that for the maximun endurance.

The pilot decides to increase v2. Does this have any effect on the 35ft screen height?. The 35ft screen height is located further down along the runway. The distance from the beginning of the take-off roll to the location of the screen height will be shorter. The screen height an the location of the screen height along the runway will no change. The screen height will be increased to 50 ft.

Reduced take-off thrust. Has the benefit of improving engine life. Is not recommended at very low temperature (OAT). Can be used if the actual take-of Mass is higher than the performance limited Take-off Mass. Can be used if the headwind component during take-off is at least 10 kt.

Assume a take-off with a class A airplane on a wet runway. Which of the following values shows the corresponding screen height of the take-off distance?. 15ft. 35ft. 0ft. 50ft.

Which statement regarding the relationship between traffic load and range is correct?. The traffic load can be limited by the desire range. The maximun Zero Fuel Mass limits the maximun quantity of fuel. The maximun Landing Mass is basically equal to the maximun Zero Fuel Mass. The maximun traffic load is not limited by the reserve fuel quantity.

Which of the following will increase if you increase V1 but VR remains unchanged?. Accelerate Stop Distance. All engine Take-off Distance. Take-Off Run. Take-Off Distance.

Aircraft mass is reduced at 5% on level flight. Assuming the specific fuel consumption is unchanged, the fuel flow over a one-hour period will be reduced by?. 5%. 10%. 15%. Nothing.

During certification flight testing of a transport jet aeroplane, the distances measured from brake release to 35 ft point are equal to: 1.779 m. 1.720m. 1.978m. 1.547m.

How is wind considered in the Take-Off performance data of the airplane Operations Manual?. Not more than 50% of ah headwind and not less than 150% of a tailwind. Unfactored headwind and tailwind components are used. Since Take-offs with tailwind are not permitted, only headwinds are considered. Not more than 80% headwind and not less than 125% tailwind.

The speed VR: Is the speed at which rotation to the lift-off angle of attack is initiated. Must be equal to or lower than V1. Must be higher than V2. Must be higher than VLOF.

What effect has a downhill slope on the take-off speeds? The slope. Decreases the take-off speed V1. Decreases the TAS for take-off. Has no effect on the take.off speed V1. Increases the IAS for take-off.

At which MINIMUM height will the second climb segment end?. 400 ft above field elevation. 35 ft. above ground. 1500 ft. above field elevation. When gear retraction is completed.

If the thrust available exceeds the thrust required for level flight. The aeroplane accelerates if the altitude is maintained. The aeroplane decelerates if the altitude is mantained. The aeroplane descents if the airspeed is mantained. The aeroplane decelerates if it is in the region of reversed command.

For a jet airplane, the speed for maximum range is: That corresponding to the point of contact of the tangent from the origin to the Drag versus TAS curve. That corresponding to the point of the minimun drag at the Drag versus TAS curve. That corresponding to the point of contact of the tangent from the origin to the Power required versus TAS curve. That corresponding to the point of the minimum power required the Drag versus TAS curve.

What is a balance field length?. The one engine inoperative take-off distance and the rejected take-off distance to full stop are equal. The one engine inoperative acceleration distance to V1 and the rejected take-off distance to full stop are equal. The one engine inoperative take-off distance and the rejected take-off distance to full stop are equal. The all engine take-off distance and the rejected take-off distance to full stop are equal.

What happens when flying at the backside of the power curve?. The speed is unstable. The aeroplane will not stall. The altitude cannot be maintained. The elevator must be pulled to lower the nose.

The vertical Interval by which a Class A aeroplane must avoid all obstacles in the drift down path, during the drift down following an engine failure is: 2.000 ft. 35 ft. 1.000 ft. 1.500 ft.

Provided all other parameters stay constant, which of the following alternatives will decrease the take-off ground run?. Decreased Take-Off Mass, increased density, increased flap setting. Decreased Take-Off Mass, increased Pressure Altitude, increased temperature. Increased pressure altitude, increased outside air temperature, increases Take-Off Mass. Increase outside air temperature, decreased pressure altitude, decreased flap setting.

For class A aircraft, the net take-off flight path is subdivided into various segments. Which of the following statements is correct?. The final segment starts at the end of segment 3 with the aircraft in clean configuration, at the final segment climb speed with maximum continuous power set, ending at 1,500 ft or higher if there are distant obstacles to clear. The 3rd segment is completed at the normal flap retraction height and is flown at max continuous thrust. The second segment is flown at V3 up to a height of 400 ft. ( flap retraction height). The first segment starts at the end of TODA where the aircraft should be at 50ft. and V2. This segment is flown at V2 whilst the landing gear is retracted.

Which speed provides maximum obstacle clearance during climb?. The speed at which the excess of power available over thrust required is the greatest. V2. V2 + 10kts. The speed for maximum rate of climb.

For a jet transport aeroplane, which of the following is the reason for the use of ¨maximum range speed¨?. Minimum specific fuel consumption. Minimun Drag. Minimum specific fuel consuption. Minimum fuel flow.

A headwind component increasing with altitude, as compared to zero wind condition (assuming IAS constant). Has no effect on ROC. Decrease angle and ROC. Improves angle and ROC. Does not have any effect on the angle of flight path during climb.

In case of an engine failure recognized below V1: The take-off must be rejected. The take-off should only be rejected if a stopway is available. The take-off is to be continued unless V1 is less than balanced V1. The take-off may be continued is a clearway is available.

Which of the following statements about the optimum flight level is true?. ATC never allows you to fly at it continuously. You should always fly about it. You should always fly at this level because it is the most economically viable. You should always fly above it.

VR cannot be lower than. V1 and 105% of VMCA. 105% of V1 and VMCA. 1.12 VS for turbo-prop with three or more engines. 1.2 VS for twin and three engine jet aeroplanes.

Which statement in relation to the climb limited Take-Off Mass of a jet aeroplane is correct?. The climb limited Take-Off Mass decreases with increasing OAT. The climb limited Take-Off Mass is determined at the speed for best rate of climb. Oh high elevation airports equipped with long runways the aeroplane will always be climb limited. 50% of a headwind is taken into account when determining the climb limited take-Off Mass.

Which of the following distances will increase if you increase V1 but VR remains unchanged. Accelerate Stop Distance. All engine Take-Off distance. Take-off Run. Take-off Distance.