Landing distance correction factor for (i) forecast headwind component (ii) forecast tailwind component.

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 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

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

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

The transition phase of RTO demonstrated in flight test is artificially expanded in the accelerate-stop distance required calculation, this expansion is to:

Which on of the following is correct in relation to takeoff flight path?

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

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.”

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

In the Vmcg calculation, the path from the point at which the critical engine is inoperative to the point at which recovery to a direction parallel to the centreline is completed may not deviate by:

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

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

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

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

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

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

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.

The definition of takeoff distance available is:

Assuming takeoff weight, Vr (rotation speed) and aerodrome ambient conditions remain constant. A decrease in takeoff flap setting will cause:

Vmcg is dependent on:

What thrust setting should be used for operating engines in the third segment of the flight path?

Ambient conditions at an airport are considered in the determination of RTOW, these include: 1. humidity 2. visibility 3. wind 4. pressure

Minimum control speed (Vmcg) on the ground:

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

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

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

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 is true about TODA:

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

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

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

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

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

Which is true of Vmcg on the ground?

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

The definition of accelerate-stop distance available is:

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

In the case of engine failure, the aeroplane must be capable of clearing all objects on either side of the intended track within: 1. 10nm 2. 5nm providing the operator takes into account navigational aide en route 3. 20nm in mountainous areas

Which of the following can be used to recover control of the aeroplane when the critical engine is suddenly made inoperative in the minimum control speed on the ground (Vmcg) definition? 1. with the use of primary aerodynamic controls alone to enable the takeoff to safely continue 2. with the use of nose gear steering 3. with the use of asymmetrical setting on engine 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

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

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

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

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

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 _____”

For a given declared temperature at which the aircraft performance is being assessed, if it is within a certain termperature of the maxinum aircraft operating temperature, the use of declared temperature is not permitted.

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

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

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:

RTOWs are computed taking into considerations runway wind components. They are predicted on: 1. 50% of headwind component 2. 150% of headwind component 3. 50% of tailwind component 4. 150% of tailwind component

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

In addition to runway slope and wind component, which one of the following sets of factors affects the brake energy (Vmbe)?

The relationship of the takeoff speeds is: 1. V1 must not exceed Vmbe 2. V1 must not exceed Vr 3. V1 must not be less than Vmcg

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

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?

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

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:

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.

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

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

When the airplane takeoff weight is not field length limited, the advantage of selecting a high V1 are: 1. required less takeoff distance for a continued takeoff 2. better vertical clearance above an obstacle 3. more stopping margin for the RTO 4. more margin for climb limit

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

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

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

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

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

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

On a dry runway, the landing distance required is:

The technique of improved climb can be used to: 1. enhance the field length limit weight 2. enhance the obstacle limited weight when limited by distant obstacles 3. enhance the Vmcg limited weight due to the increase in V1 4. enhance the climb limited weight

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.

You have an engine failure between V1 and Vr: what speed do you accelerate to and to what height do you climb to?

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

Pertaining to Vmcg, what is true?

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

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

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

If the RTOW is climb limited, which of the following actions are correct to increase RTOW:

Which statement concerning improved climb technique are correct: 1. an increase in V2 does not result in the increase in the assoiciated V1 and Vr 2. an increase in the takeoff speed V1, Vr and V2 results in an increase in the field length required 3. for a fixed runway length, the field length limit weight increase with an increase in V2 4. the tire speed limits and brake energy limits may become limiting at the higher takeoff speeds

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

JAA regulations define threshold crossing speed at:

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

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

The definition of climb gradient is:

A larger flap setting will result in: 1. better field length limit weight for a given runway 2. a smaller climb limited weight 3. a lower V1 speed for a given weight 4. a lower Vmbe

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

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

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

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: