Higher V2 uses (i) takeoff distance, a (ii) in the distance to an obstacle resulting in a (iii) climb gradient required

Which is true of the declared distance for a given runway?

Operations involving the use of variable takeoff thrust may be conducted:

Which of the following statements are correct concerning reduced thrust takeoff using assumed temperature method: 1. reduced thrust takeoff using assumed temperature method gives an aircraft performance equal to perform at the assumed temperature 2. if the assumed temperature is lower than flat rated temperature, this can achieve thrust reduction 3. reduced thrust my not be used on wet runway

Which is true of the declared distance for a given runway?

On wet or contaminated runway, the accelerate-stop distance calculated is based on: 1. performance credit for reverse thrust 2. no reverse thrust credit 3. manual braking/full spoilers 4. auto braking

Takeoff WAT curve for an aircraft in performance group A assumes:

The definition of accelerate-stop distance available is:

Decrease flap from 10 degrees to 5 degrees 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

Which is a recommended procedure when operating from a contaminated runway?

What factors other than slope and wind affect Vmbe?

With one engine inoperative, obstacle clearance, when overhead an aerodrome, should be maintained above:

The demonstrated landing distance under the JAA rules is predicted on the use of: 1. maximum manual wheel braking 2. full auto speed brakes 3. reverse thrust 4. wet runway

Which is true of the declared distance for a given runway?

In the calculation of accelerate-stop distance required, the transition distance calculation allow time for pilot reaction time for: 1. applying maximum braking 2. retarding the throttles 3. configuring the airplane to stopping mode for an average pilot 4. raising the speed brakes

What thrust settings should be used for operating engines in the fourth or final segment of the flight path?

All other factors remaining constant, a decrease in aerodrome pressure altitude will _____ the takeoff distance required and ______ the second segment net gradient of climb.

When the airplane takeoff weight is not field length limited, the advantages of selecting a lower V1 are: 1. increased safety margin for obstacle clearance 2. increased safety margin for tyre speed limit 3. increased safety margin for brake energy limit 4. increased stopping margin for an RTO

Which of the following is true for V speeds relationships are correct? 1. Vr higher limit = V2 2. Vr lower limit = Vmca x 1.05/1.1 3. Vr lower limit = Vmu x 1.05

Which of the following statement is correct concerning reduced thrust takeoff using assumed temperature method:

Takeoff decision speed (V1) is the speed: 1. from which a decision to continue the takeoff is made, which results in a takeoff distance to a height of 35ft on a dry runway at a speed of V2, that will not exceed the useable takeoff distance 2. at which the engine failure is recognized 3. at which the first action is taken to bring the aeroplane to a full stop and will not exceed the ASDA

Regulation requires that after one engine failure, the airplane can continue the flight to an aerodrome where a safe landing may be made by using:

When calculating RTOW, what runway slope is taken into account?

Takeoff flight path is divided into segments according to the: 1. thrust 2. configuration of the aeroplane, eg flaps 3. speed 4. time required

An engine failure is recognized at V1:

For which airplane in performance group A is this statement true? “If an alternate airport is designated in the flight plan, the landing distiance required may be that appropriate to an alternate aérodrome when assessing the ability of the airplane to satisfy the requirement of the destination aérodrome.”

Which statement is correct? The relationship of the takeoff speeds is:

Select the answer which you consider will correctly complete the following statement. “The net takeoff flight path extends from _____ to 1500’ above aerodrome level, and should clear any obstacle in its path by a vertical interval of _____”

Given the following data, which is the overal gradient on runway 07? elevation at start of runway 07 is 305ft elevation at start of runway 25 is 283ft length 2745m

JAA regulations define threshold crossing speed at:

Minimum climb gradient for each segment in the takeoff is:

The landing WAT curve or graph ensures that at a given weight, the aircraft will have an acceptable minimum climb capability with:

Published takeoff performance data for aircraft in performance group A makes allowances for use of a runway line up distance of:

If the RTOW is climb limited, which of the following actions are correct to increase RTOW: 1. use a smaller flap setting 2. use improved climb technique 3. use air-conditioning packs off takeoff

Which of the following statements is correct?

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

Which of the following is true regarding use of reduced thrust takeoff? 1. if the assumed temperature is lower than flat rated temperature, then there will be no reduction in thrust 2. can be used if OAT is less than the assumed temperature 3. reduced thrust may not be used on wet runway takeoff 4. reduced thrust takeoff using assumed temperature method gives an aircraft performance lower to performance at the assumed temperature

When an engine inoperative, regulation requirement is to have a vertical clearance of (i) en route and (ii) above aerodrome.

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 specified area along takeoff flight path

Which of the following is true?

The minimum level off pressure altitude, as applied to the clearance of distant obtacles when using the extended second segment climb procedure, may be defined as:

Obstacle height is generally referenced to the elevation at the end of the TODA. Assuming the climb gradient is constant, the flight path of an uphill slope runway will begin at a relatively ______ elevation relative to a downhill slope.

Which of the following statements is true concerning operations involving the use of variable takeoff thrust?

Using a wet V1 on a wet runway, compared to a dry V1 on a dry runway, in the event of an engine failure the safety margin with a continued takeoff will:

Increase flap from 5 deg to 10 deg will result in: 1. decrease in field length limit for a given runway 2. decrease climb limit weight 3. decrease V1 speed for a given weight

For a given weight and takeoff weight is not field length limit, with a low V1 gives: 1. long ASD required 2. short TOD required 3. short ASD required 4. long TOD required

Which of the following is correct concerning weight and performance provisions/regulations during the en route phase of flight involving an engine failure?

When a runway is defined as a contaminated runway: 1. any part of the runway surface is covered by water greater than 3mm deep 2. it has an accumulation of compacted snow or wet ice 3. more than 25 percent of the runway surface area is covered by slush or dry snow equivalent to greater than 3mm of water 4. 10% of the runway covered by water with a depth less than 3mm

For twin engines airplanes without ETOPS approval, the airplane cannot operate beyond what time limit flying time at the normal one engine inoperative cuise speed from the nearest aerodrome:

On a wet runway, the landing distance required is:

An obstacle is identified as being 5920m from the end of the takeoff distance available, and 830m from the intended line of flight. Given the wingspan of the aircraft is 48m, the semi width of the funnel at a given point is?

Pertaining to Vmcg, what is true?

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 x Vmca 4. V2 must not be less than 1.13 x Vs1g

On a dry runway, the landing distance required is:

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.

A range of V1/Vr values become available for takeoff when:

Which is true of Vmcg on the ground?

The gross climb gradients of the takeoff flight path for a given weight is a function of: 1. airport pressure altitude 2. airport temperature 3. runway slope 4. runway length

The definition of takeoff distance available is:

Which is the correct procedure in relation to the moment at which an engine failure is recognized?

Which of the following statements are true concerning operation on a contaminated runway?

The aircraft is not field length limited, multiple V1 is available. Some operators may prefer to use a lower V1, State the benefits of using a high V1. 1. requires less takeoff distance for a confirmed takeoff 2. better vertical clearance above an obstacle 3. greater stop margin in abandoned takeoff

Reduced thrust takeoff will: 1. lower the turbine operating temperature 2. not change the RPM of rotating components 3. reduce maintenance cost 4. increase engine reliability

For airplanes with 3 or more engines, the 2 engines inoperative terrain clearance need not be considered

What action should you take when an engine failure happens between V1 and V2?

Which one of the following statements is true concerning the calculation of the maximum speed for abandoning takeoff Vstop on a contaminated runway?

When an obstacle is to be cleared, on the basis of an extended second segment climb:

The takeoff distance available (TODA) is:

Under the following conditions, what happens to the Vr and V2 speed?

If you have a range of V1’s available, and an engine failure is recognized at V1:

A clearway: 1. can always be used as stopway 2. is an obstacle-free area beyond the runway 3. under the control of the airport authorities 4. can be used as part of the takeoff distance available

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

When an obstacle is to be cleared, on the basis of an extended second segment climb:

Which statements are correct concern thrust derate: 1. use of derates is permitted on contaminated runway, anti-skid inoperative, landing gear extended. 2. it is necessary to publish specific performance data tailored to that derate to flight crew. 3. one of the advantages of using derate thrust is when maximum takeoff weight is Vmcg limited at full takeoff thrust rating. 4. the Vmcg speed is independent of the levels of takeoff thrust derate.

The definition of climb gradient is:

Obstacle height is generally referenced to the elevation at the end of takeoff distance (i). Assuming the climb gradient is constant, the flight path of a (ii) slope runway will begin at a relatively (iii) elevation.

Which of the following is true for V speeds relationships are correct? 1. V2 lower limit = Vr and V1 2. V2 lower limit = Vs x 1.2 and Vmca x 1.1 3. V2 higher limit = Vmbe or Vr

With one engine inoperative, the airplane must be capable of clearing all obstacles en route using net performance:

Which of the following values may be used in the assessment of takeoff performance? 1. actual 2. forecast 3. reported 4. expected

If an engine failure is recognised above V2, which of the following is correct?

Which is true of the declared distance for a given runway?

Which of the following statements is correct concerning assumed temperature method?

In a recent CIVIL AVIATION INFORMATION CIRCULAR the recommended procedure for operating on a contaminated runway is to:

For which of the following flights may forecast temperature (as opposed to actual or reported) be used in assessing performance? 1. takeoff 2. en route 3. landing

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

The improved climb procedure during takeoff is a technique:

The auto brake system is normally used during landing, which of the following is true?

Which is true of runway slope in relation to performance calculations for aircraft in performance group A?

The landing weight of the airplane must satisfy:

On dry runway the accelerate-stop distance is established based on: 1. Manual braking/full spoilers 2. Auto brakes 3. Reverse thrust 4. No reverse thrust

The screen height requirement for a continued takeoff with a failed engine is: 1. 15ft on a wet runway 2. 15ft on a contaminated runway 3. 35ft on a dry runway 4. 35ft on a contaminated runway