Which of the alternatives represents the correct relationship ? [ Diploma registration ]

Question 92-1 : Vmcg and v1 should not exceed vr vmca and v2 should not exceed v1 vmcl and v1 should not exceed vr v2 and v1 should not exceed vmcg

With all engines out a pilot wants to fly for maximum time therefore he has to ?

Question 92-2 : The minimum power required the critical mach number the minimum angle of descent the maximum lift

Considering the take off decision speed v1 which of the following is correct ?

Question 92-3 : If an engine failure is recognized before reaching v1 the take off must be aborted v1 may not be less than v2min the minimum take off safety speed if an engine failure is recognized after reaching v1 the take off must be aborted v1 is sometimes greater than the rotation speed vr

The effect of a higher take off flap setting up to the maximum certified take ?

Question 92-4 : An increase of the field length limited take off mass but a decrease of the climb limited take off mass a decrease of both the field length limited take off mass and the climb limited take off mass a decrease of the field length limited take off mass but an increase of the climb limited take off mass an increase of both the field length limited take off mass and the climb limited take off mass

Which of the following statements is correct ?

Question 92-5 : A stopway is an area beyond the end of tora able to support the aeroplane mass during an abandoned take off a declared safe area is an area beyond the runway end which can be used for an abandoned take off a clearway is an area beyond the runway end which can be used for an abandoned take off if a clearway or a stopway is used in the take off calculations the lift off point may be beyond the end of tora

Besides lift the forces that determine the gradient of climb of an aeroplane are ?

Question 92-6 : Weight drag and thrust weight and drag only thrust and drag only weight and thrust only

What happens when flying at the 'backside of the power curve' ?

Question 92-7 : The speed is unstable the aeroplane will not stall the altitude cannot be maintained the elevator must be pulled to lower the nose

The effect that an increased outside air temperature has on the climb ?

Question 92-8 : Reduces both the climb gradient and the rate of climb increases the climb gradient and decreases the rate of climb does not affect the climb performance reduces the climb gradient and increases the rate of climb

A headwind component increasing with altitude as compared to zero wind ?

Question 92-9 : Has no effect on rate of climb does not have any effect on the angle of flight path during climb improves angle and rate of climb decreases angle and rate of climb

During a descent a headwind will ?

Question 92-10 : Increases the angle of the descent flight path increases the angle of descent increases the rate of descent increases the descent distance over ground

With an true airspeed of 194 kt and a vertical speed of 1000 ft/min the climb ?

Question 92-11 : 3° 3% 5° 8%

With regard to a jet aeroplane specific range is the ?

Question 92-12 : Tas divided by fuel flow fuel flow divided by tas unit of thrust per unit of fuel fuel flow per unit of thrust

Which of the following statements concerning tires is the major consideration ?

Question 92-13 : Rotation rate of the tyre and temperature tyre pressure and brake temperature rotation rate of the tyre and vmbe tyre pressure and temperature

What will increase the 'landing field length limited landing mass' when ?

Question 92-14 : A headwind a downslope a contaminated runway an increase in pressure altitude

When calculating approach speeds the minimum approach speed in the initial ?

Question 92-15 : 1 4 to 1 5 times vs1 2 times vs1 1 15 times vs0 1 05 times vat

You are approaching a wet runway in gusty conditions you should ?

Question 92-16 : Increase approach speed adopt a steeper approach path decrease approach speed increase landing speed

Compared with a level runway the use of a runway with a 2% downslope will ?

Question 92-17 : Reduce vmbe increase vmbe and v1 not affect the value of v1 increase vmbe and decreased v1

If the anti skid system is inoperative may auto brake system can be used ?

Question 92-18 : No never without any limitation if selected to minimum only if full reverse thrust is used

You climb with a climb speed schedule 300/ 78 what do you expect in the ?

Question 92-19 : The rate of climb increases since the constant ias climb is replaced by the constant mach climb during the acceleration to the mach number 0 78 the rate of climb is approximately zero the rate of climb decreases since climb performance at a constant mach number is grossly reduced as compared to constant ias no noticeable effect since the true airspeed at 300 kts ias and 0 78 mach are the same at isa temperature tas = 460 kt

The effect of an aft cg on take off performance are ?

Question 92-20 : Take off distance decreases climb gradient increases take off distance decreases climb gradient remains constant take off distance and climb gradient increase take off distance and climb gradient decrease

At maximum landing mass the structure of the aircraft is designed for a rate of ?

Question 92-21 : 600 ft/min 200 ft/min 250 ft/min 220 ft/min

The approach climb requirement is normally met by ?

Question 92-22 : Reducing flap setting for approach with one engine inoperative selecting a runway with no obstacles in the go around area a threshold speed of 2 times stall speed reducing final approach speed

A change of runway in use from a runway slope of 1% downhill to a runway slope ?

Question 92-23 : Increase take off run increase take off distance increase take off run decrease take off distance decrease take off run decrease take off distance decrease take off run increase take off distance

An uphill slope runway will ?

Question 92-24 : Increase asdr decrease asdr increase asdr only if the tom increases decrease asdr only if the tom decreases

Runway 30 is in use and the threshold elevation is 2139 feet threshold ?

Question 92-25 : 2 65% uphill 1 49% uphill 2 53% per minute 1 86% downhill

In the event of an engine failure during cruise it is necessary to reduce speed ?

Question 92-26 : For maximum lift/drag ratio and if necessary start fuel jettisoning close to stall speed and if necessary starting fuel jettisoning for best rate of climb with full flaps for minimum drag speed vmd with full flaps

On a long distance flight the optimum cruise altitude is continuously increased ?

Question 92-27 : As a consequence of the fuel consumption to take in account the passenger movements all along the flight due do the decreasing outside air temperature because of the movements of the centre of gravity

The take off and landing distances on a grass runway are in relation to that ?

Question 92-28 : Take off distance and landing distance increase take off distance and landing distance decrease take off distance decreases and landing distance increases take off distance increases and landing distance decreases

Which take off condition is most likely resulting in the poorest climb ?

Question 92-29 : 5000 ft field elevation isa +20° take off flaps 30° sea level field elevation isa 20° take off flaps 10° sea level field elevation isa +5° take off flaps 10° 5000 ft field elevation isa 5° take off flaps 10°

During take off the time between critical engine failure and v1 recognition ?

Question 92-30 : 2 seconds 5 seconds 6 seconds 0 seconds

The lift off speed vlof and take off safety speed v2 when flap position is ?

Question 92-31 : Increase / increase decrease / increase increase / decrease decrease / decrease

An aircraft has this following flap position up 5° 10° 20° if the flap ?

Question 92-32 : Increase take off distance decrease landing distance decrease ground roll distance decrease take off distance

Changing flaps selection from 10° to flaps 0° while establish in climb after ?

Question 92-33 : Climb gradient and vy increase climb gradient and vy decrease climb gradient remains unchanged and vy decreases climb gradient increases and vy decreases

During a descent a headwind will have the following effects ?

Question 92-34 : Descent angle remains constant flight path angle increases descent angle decreases flight path angle increases descent angle and flight path angle increases descent angle remains constant flight path angle decreases

During a descent a tailwind will have the following effects ?

Question 92-35 : Descent angle remains constant flight path angle decreases descent angle remains constant flight path angle increases descent angle and flight path angle increases descent angle increases flight path angle decreases

The 'flight path angle' is the angle ?

Question 92-36 : Between the horizontal plane and the flight path between the relative airflow and the horizontal plane between the longitudinal axis and the horizontal plane displayed on the attitude indicator artificial horizon

The vertical 'flight path angle' is assumed to be ?

Question 92-37 : Ground related the same as pitch angle relative to the longitudinal axis the angle of attack

Specific fuel consumption sfc is ?

Question 92-38 : Mass of fuel required to produce unit power for unit time designed fuel consumption for a given rpm quantity of fuel required to run the engine for one minute at maximum operating conditions maximum fuel consumption of the aircraft

The specific range sr is ?

Question 92-39 : The air distance that the aircraft would fly per kilogram of fuel the ground distance that the aircraft would fly per kilogram of fuel the ground distance divided by air distance the air distance that the aircraft would fly per unit of thrust

How does the asdr accelerate stop distance required will be affected by the ?

Question 92-40 : Remains the same increases decreases decreases only for a downhill stopway