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Question 92-1 : Which of the following statements is correct ? [ Diploma registration ]

A stopway is an area beyond the end of tora able to support the aeroplane mass during an abandoned take off

Admin .official easa definition.stopway means an area beyond the take off runway no less wide than the runway and centred upon the extended centreline of the runway able to support the aeroplane during an abortive take off without causing structural damage to the aeroplane and designated by the airport authorities for use in decelerating the aeroplane during an abortive take off .tora take off run available exemple 192 A stopway is an area beyond the end of tora able to support the aeroplane mass during an abandoned take-off.

Question 92-2 : Besides lift the forces that determine the gradient of climb of an aeroplane are ?

Weight drag and thrust

exemple 196 Weight, drag and thrust.

Question 92-3 : What happens when flying at the 'backside of the power curve' ?

The speed is unstable

Admin .vdo919 exemple 200 The speed is unstable.

Question 92-4 : The effect that an increased outside air temperature has on the climb performance of an aeroplane is that it ?

Reduces both the climb gradient and the rate of climb

exemple 204 Reduces both the climb gradient and the rate of climb.

Question 92-5 : A headwind component increasing with altitude as compared to zero wind condition assuming ias is constant ?

Has no effect on rate of climb

Admin .wind has no effect on rate of climb or rate of descent but a head wind will decrease the distance covered over the ground to climb a given distance the slope increases exemple 208 Has no effect on rate of climb.

Question 92-6 : During a descent a headwind will ?

Increases the angle of the descent flight path

Admin .during a descent a headwind will increases the angle of the descent flight path . 2518.the descent distance over ground is decreased the rate of descent and the angle of descent remain unchanged exemple 212 Increases the angle of the descent flight path.

Question 92-7 : With an true airspeed of 194 kt and a vertical speed of 1000 ft/min the climb angle is about ?

3°

Admin .climb angle ° = gradient % x tas kt .1000 = gradient x 194.gradient = 1000 / 194 = 5%.climb angle ° = climb angle % x 0 6.thus climb angle ° = 5 x 0 6 = 3° exemple 216 3°.

Question 92-8 : With regard to a jet aeroplane specific range is the ?

Tas divided by fuel flow

Ecqb03 july 2016 exemple 220 Tas divided by fuel flow.

Question 92-9 : Which of the following statements concerning tires is the major consideration when establishing the tyre speed limit ?

Rotation rate of the tyre and temperature

Ecqb04 october 2017..vmax tyre the maximum ground speed of the tyres .the highest speed that the tires can handle without becoming damaged it is possible to drive so fast that the tread actually flies of the tires if you drive fast enough the centrifugal forces become so great that the tire falls apart that must be avoided and therefore there is a maximum rolling speed for a tyre that speed is printed on the side of the tyre near the size usually a number in miles per hour .vmbe maximum brake energy speed is the speed from which the aeroplane may be brought to a stop without exceeding the maximum energy absorption capability of the brakes exemple 224 Rotation rate of the tyre and temperature.

Question 92-10 : What will increase the 'landing field length limited landing mass' when operating with the anti skid inoperative ?

A headwind

Ecqb04 october 2017..if you have a weight limitation at landing due to the length of the runway a headwind will help you to have a reduced approach and landing speed therefore you may land at a higher mass .other statements will are wrong since theay lead to an increase in the required landing distance and therefore a decrease in the 'landing field length limited landing mass' exemple 228 A headwind.

Question 92-11 : When calculating approach speeds the minimum approach speed in the initial approach phase is usually ?

1 4 to 1 5 times vs1

exemple 232 1.4 to 1.5 times vs1.

Question 92-12 : You are approaching a wet runway in gusty conditions you should ?

Increase approach speed

Ecqb04 october 2017..you should in order to avoid windshear increase slightly your approach speed but you must land at your calculated landing speed not less not more exemple 236 Increase approach speed.

Question 92-13 : Compared with a level runway the use of a runway with a 2% downslope will ?

Reduce vmbe

Ecqb04 october 2017..vmbe maximum brake energy speed is the speed from which the aeroplane may be brought to a stop without exceeding the maximum energy absorption capability of the brakes for a downhill slope you will reach vmbe at a lower speed compared to a level runway more kinetic energy needs to be absorb due to the down hill component of the runway .also a downhill slope means that you need a longer distance to stop in case of failure before v1 and you will reach v1 at an earlier point in the take off run than on a 'flat' runway v1 has to be reduced .vmbe and v1 will be reduced exemple 240 Reduce vmbe.

Question 92-14 : If the anti skid system is inoperative may auto brake system can be used ?

No never

Admin .anti skid system protection is provided during auto brake operation therefore if anti skid is inoperative you can not use the auto brake system exemple 244 No, never.

Question 92-15 : You climb with a climb speed schedule 300/ 78 what do you expect in the crossover altitude 29200 ft oat = isa ?

The rate of climb increases since the constant ias climb is replaced by the constant mach climb

exemple 248 The rate of climb increases since the constant ias-climb is replaced by the constant mach-climb.

Question 92-16 : The effect of an aft cg on take off performance are ?

Take off distance decreases climb gradient increases

Ecqb04 october 2017 exemple 252 Take-off distance decreases, climb gradient increases.

Question 92-17 : At maximum landing mass the structure of the aircraft is designed for a rate of descent of ?

600 ft/min

exemple 256 600 ft/min.

Question 92-18 : The approach climb requirement is normally met by ?

Reducing flap setting for approach with one engine inoperative

exemple 260 Reducing flap setting for approach with one engine inoperative.

Question 92-19 : A change of runway in use from a runway slope of 1% downhill to a runway slope of 1% uphill will ?

Increase take off run increase take off distance

exemple 264 Increase take-off run, increase take-off distance.

Question 92-20 : An uphill slope runway will ?

Increase asdr

Ecqb04 october 2017..a uphill slope increases the accelerate stop distance required asdr taking off on a uphill slope does decrease the braking distance in the case of a rejected take off but it increases the distance taken to accelerate to v1 due to the addition of the uphill component of the weight of the aircraft decreasing the rate of acceleration exemple 268 Increase asdr.

Question 92-21 : Runway 30 is in use and the threshold elevation is 2139 feet threshold elevation of runway 12 is 2289 feet .take off run available is 1720 metres and clearway is 280 metres .what is the slope of the runway in use ?

2 65% uphill

Admin .2289 ft 2139 ft = 150 ft .150 ft x 0 3048 = 45 72m .runway lenght is 1720m slope in % is . 45 72m /1720m x 100 = 2 65% exemple 272 2.65% uphill.

Question 92-22 : In the event of an engine failure during cruise it is necessary to reduce speed and descend to lower altitude at speed ?

For maximum lift/drag ratio and if necessary start fuel jettisoning

Ecqb04 october 2017 exemple 276 For maximum lift/drag ratio and, if necessary, start fuel jettisoning.

Question 92-23 : On a long distance flight the optimum cruise altitude is continuously increased during the flight ?

As a consequence of the fuel consumption

Ecqb04 october 2017 exemple 280 As a consequence of the fuel consumption.

Question 92-24 : The take off and landing distances on a grass runway are in relation to that for a paved runway ?

Take off distance and landing distance increase

Ecqb04 october 2017..take off distance on a dry short grass runway compared to a paved dry runway distance increases by 20% .landing distance on a dry short grass runway compared to a paved dry runway distance increases by 15% exemple 284 Take-off distance and landing distance increase.

Question 92-25 : Which take off condition is most likely resulting in the poorest climb performance ?

5000 ft field elevation isa +20° take off flaps 30°

exemple 288 5000 ft field elevation, isa +20°, take-off flaps 30°.

Question 92-26 : During take off the time between critical engine failure and v1 recognition time is assumed to be approximately ?

2 seconds

Admin .following an engine failure at v1 and allowing for a reaction time of 2 seconds a correctly loaded aircraft must be capable of decelerating to a halt within the accelerate stop distance available exemple 292 2 seconds.

Question 92-27 : The lift off speed vlof and take off safety speed v2 when flap position is changed from 10° to 5° will ?

Increase / increase

exemple 296 Increase / increase.

Question 92-28 : An aircraft has this following flap position up 5° 10° 20° if the flap setting is 'up' instead of 10° it will ?

Increase take off distance

Ecqb04 october 2017 exemple 300 Increase take-off distance.

Question 92-29 : Changing flaps selection from 10° to flaps 0° while establish in climb after take off will have the following effects ?

Climb gradient and vy increase

Ecqb04 october 2017..vy is the indicated airspeed for best rate of climb climbing at vy allows pilots to maximize the altitude gain per unit time .climb gradient is defined as the ratio of the increase of altitude to horizontal air distance expressed as a percentage .you will generate less drag with a less flaps selection the gap between the thrust available and thrust required increases exemple 304 Climb gradient and vy increase.

Question 92-30 : During a descent a headwind will have the following effects ?

Descent angle remains constant flight path angle increases

Ecqb04 october 2017..during a descent a headwind will increases the flight path angle . /com en/com080 642 jpg.the descent distance over ground is decreased the rate of descent and the angle of descent remain unchanged .angle of descent descent angle is the angle you maintain on your attitude indicator artificial horizon / pfd .note for theoretical knowledge examination purposes 'flight path angle' is assumed to be ground related .the flight path angle is the actual vector flown in relation to the ground it will increase during descent with a headwind exemple 308 Descent angle remains constant, flight path angle increases.

Question 92-31 : During a descent a tailwind will have the following effects ?

Descent angle remains constant flight path angle decreases

Ecqb04 october 2017..during a descent a tailwind will decreases the flight path angle . /com en/com032 351 jpg.the descent distance over ground is increased the rate of descent and the angle of descent remain unchanged .angle of descent descent angle is the angle you maintain on your attitude indicator artificial horizon / pfd .note for theoretical knowledge examination purposes 'flight path angle' is assumed to be ground related .the flight path angle is the actual vector flown in relation to the ground it will decrease during descent with a tailwind exemple 312 Descent angle remains constant, flight path angle decreases.

Question 92-32 : The 'flight path angle' is the angle ?

Between the horizontal plane and the flight path

Ecqb04 october 2017.. 682.note for theoretical knowledge examination purposes 'flight path angle' is assumed to be ground related .the flight path angle is the actual vector flown in relation to the ground it will decrease during descent with a tailwind .angle of descent descent angle is the angle you maintain on your attitude indicator artificial horizon / pfd exemple 316 Between the horizontal plane and the flight path.

Question 92-33 : The vertical 'flight path angle' is assumed to be ?

Ground related

Ecqb04 october 2017.. 682.note for theoretical knowledge examination purposes 'flight path angle' is assumed to be ground related .the flight path angle is the actual vector flown in relation to the ground it will decrease during descent with a tailwind and will increase with a headwind .angle of descent descent angle is the angle you maintain on your attitude indicator artificial horizon / pfd exemple 320 Ground related.

Question 92-34 : Specific fuel consumption sfc is ?

Mass of fuel required to produce unit power for unit time

Ecqb04 october 2017..specific fuel consumption is the amount of fuel burnt per unit of thrust for jets it reduces with altitude up to the tropopause exemple 324 Mass of fuel required to produce unit power for unit time.

Question 92-35 : The specific range sr is ?

The air distance that the aircraft would fly per kilogram of fuel

Admin .specific range sr is the enroute tas divided by the current fuel flow .sr = true airspeed/total fuel flow .the units of sr are nautical miles per gallon or nautical miles per pound of fuel exemple 328 The air distance that the aircraft would fly per kilogram of fuel.

Question 92-36 : How does the asdr accelerate stop distance required will be affected by the addition of a stopway into the runway strip length the asdr ?

Remains the same

Ecqb04 november 2017..a stopway is a defined rectangular area on the ground at the end of the take off run available prepared as a suitable area in which an aircraft can be stopped in the case of an abandoned take off .asdr accelerate stop distance required is calculated with the actual values of the flight mass wind up or down slope oat pressure altitude etc it's a fixed value for the projected take off .the declared distances 'asda' acceleration stop distance available is the length of the take off run available plus the length of stopway with a stopway provided the 'runway strip' is increase exemple 332 Remains the same.

Question 92-37 : What is the effect of using engine bleed air on the take off distance ?

Reduces available thrust and increases the take off distance

exemple 336 Reduces available thrust and increases the take-off distance.

Question 92-38 : Which of the following will decrease landing distance ?

The spoilers

Ecqb04 november 2017 exemple 340 The spoilers.

Question 92-39 : If cabin altitude cannot be controlled eg rapid decompression while in cruise at fl370 a rapid descent is needed if structural integrity is not in doubt you should adopt at first the following speed and configuration ?

Target speed mmo speedbrake deployed no flaps

Ecqb04 november 2017 exemple 344 Target speed mmo, speedbrake deployed, no flaps.

Question 92-40 : The climb gradient is ?

Always larger than the angle of climb

Ecqb04 november 2017 ..the 'climb gradient' is defined as the ratio expressed as a percentage of the change in geometric height divided by the horizontal distance travelled .climb gradient = change in height / distance travelled.the value of the climb gradient is given as percent the value of the angle of climb is given in degree .for example 5% = 3° .we can say that the climb gradient is always larger than the angle of climb exemple 348 Always larger than the angle of climb.


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