PERF A ReStudy

Regarding improved V2 climb, which statements are correct? 1. Increasing V2 requires an increase in V1 and Vr 2. Increase in takeoff speeds (V1/Vr/V2) increases TODR 3. Takeoff climb limit weight is reduced 4. With an increase in takeoff speed, tyre speed limit and Vmbe may become limiting. 1 and 3. 1, 2, and 3. 1,2, and 4. All of the above.

The following airplane related factors have been considered in the RTOW. 1. one engine inoperative accountability 2. two engine inoperative accountability 3. tyre speed rating 4. brake energy limitation. 1 only. 2, 3, and 4. 1, 2 and 3. 1, 3, and 4.

At a given takeoff weight, aerodrome ambient conditions and characteristics, an increase in takeoff flap setting will (i) the second segment climb gradient and (ii) the takeoff distance required. (i) decrease (ii) decrease. (i) increase (ii)increase. (i) decrease (ii) increase. (i) increase (ii) decrease.

The relationship of the takeoff speeds are: 1. The lower limit for V1 is Vmcg 2. The lower limit for V1 is 1.05 Vmca 3. The upper limit for V1 is either Vmbe or VR. 2 & 3. 1 & 3. 1 & 2. None of the above.

Using a higher V2 (i) TODR and (ii) distance to an obstacle, resulting in a (iii) climb gradient required. (i) increases (ii) decreases (iii) increased. (i) decreases (ii) increases (iii) decreased. (i) increases (ii) increases (iii) increased. (i) decreases (ii) decreases (iii) decreased.

Decrease flap from 10° to 5° will result in: 1. Increase in field length limit for a given runway 2. Increase climb limit weight 3. Increase V1 speed for a given weight. 1 only. 1 & 2. 2 & 3. All of the above.

Which of the following statements are true concerning operation on a contaminated runway?. Takeoff from a runway contaminated by up to 20mm of standing water may be made, providing the max speed for abandoning takeoff (Vstop) on such a runway is used as the V1 wet for takeoff. The use of increased V2 procedure in the interest of improved climb performance is recommended. Takeoff may be made with reported tailwind up to 5kts. Any significant loss of runway distance available due to line up for takeoff should be taken into account for and takeoff performance recalculated.

The relationship of the takeoff speeds are: 1. V1 must not be equal to VR 2. V1 must not be less than Vmcg 3. VR must not be less than 1.05 times Vmca 4. V2 must not be less than 1.13 times Vs1g. 2 & 3. 2 & 4. 1 & 2 & 3. 2 & 3 & 4.

Published takeoff performance data for aircraft in Performance Group A makes allowance for use of a runway line up distance of: 100. 200. 4 x longitudinal distance from nose wheel axle to rear main gear axle. Not applicable.

Which is true of the declared distance for a given runway? *. LDA is always greater than TORA. LDA is always greater than TODA. LDA takes into account the stopway. Stopway is required to have an equal strength as the runway.

Which is true of the declared distance for a given runway?. LDA and TODA are equal. Stopway cannot be longer than clearway. The maximum slope for a clearway plane is 1.25%. ASDA comprises the useable runway length plus clearway.

Which is true of the declared distance for a given runway?. LDA is always greater than ASDA. The maximum slope for the clearway is 1.25°. ASDA comprises the useable runway length plus stopway. Whenever TORA and ASDA are equal a balanced field is said to exist.

When an aeroplane takeoff weight is not field length limited, the benefits of selecting a lower V1 are: 1. Improved obstacle clearance 2. Reduced aircraft noise 3. Greater stop margin for a RTO 4. Decrease chance of exceeding Vmbe. 2 & 3. 3 & 4. 2, 3 & 4. All of the above.

The Regulated Takeoff Weight (RTOW) takes into consideration the following airport factors: 1. Runway lengths 2. Runway slopes 3. Obstacles within 25nm of the airport 4. Obstacles within a specificed area along takeoff flight path. 1 & 3 only. 1 & 4 only. 1 & 2 & 3. 1 & 2 & 4.