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Question 113-1 : In performance class 2 when there is a head wind component an operator when calculating take off performance may take into account ? [ Training professional ]

More than 50% of the headwind component if a precise wind measuring equipment enables accurate measurement

Cat pol h 105 general . .c when showing compliance with the requirements of this section account shall be taken of the following parameters .1 mass of the helicopter .2 the helicopter configuration .3 the environmental conditions in particular .i pressure altitude and temperature .ii wind . a except as provided in c for take off take off flight path and landing requirements accountability for wind shall be no more than 50% of any reported steady headwind component of 5 kt or more . b where take off and landing with a tailwind component is permitted in the afm and in all cases for the take off flight path not less than 150% of any reported tailwind component shall be taken into account and . c where precise wind measuring equipment enables accurate measurement of wind velocity over the point of take off and landing wind components in excess of 50% may be established by the operator provided that the operator demonstrates to the competent authority that the proximity to the fato and accuracy enhancements of the wind measuring equipment provide an equivalent level of safety .4 the operating techniques and.5 the operation of any systems that have an adverse effect on performance exemple 213 More than 50% of the headwind component if a precise wind measuring equipment enables accurate measurement.

Question 113-2 : In performance class 1 when the wind measuring equipment has not received official approval and there is a headwind component to determine landing performance an operator may take account of at ?

Most 50% of the reported headwind component

Cat pol h 105 general . .c when showing compliance with the requirements of this section account shall be taken of the following parameters .1 mass of the helicopter .2 the helicopter configuration .3 the environmental conditions in particular .i pressure altitude and temperature .ii wind . a except as provided in c for take off take off flight path and landing requirements accountability for wind shall be no more than 50% of any reported steady headwind component of 5 kt or more . b where take off and landing with a tailwind component is permitted in the afm and in all cases for the take off flight path not less than 150% of any reported tailwind component shall be taken into account and . c where precise wind measuring equipment enables accurate measurement of wind velocity over the point of take off and landing wind components in excess of 50% may be established by the operator provided that the operator demonstrates to the competent authority that the proximity to the fato and accuracy enhancements of the wind measuring equipment provide an equivalent level of safety .4 the operating techniques and.5 the operation of any systems that have an adverse effect on performance exemple 217 Most, 50% of the reported headwind component.

Question 113-3 : In performance class 2 when the wind measuring equipment has not received official approval and there is a headwind component to determine landing performance an operator may take account of at ?

Most 50% of the reported headwind component

Cat pol h 105 general . .c when showing compliance with the requirements of this section account shall be taken of the following parameters .1 mass of the helicopter .2 the helicopter configuration .3 the environmental conditions in particular .i pressure altitude and temperature .ii wind . a except as provided in c for take off take off flight path and landing requirements accountability for wind shall be no more than 50% of any reported steady headwind component of 5 kt or more . b where take off and landing with a tailwind component is permitted in the afm and in all cases for the take off flight path not less than 150% of any reported tailwind component shall be taken into account and . c where precise wind measuring equipment enables accurate measurement of wind velocity over the point of take off and landing wind components in excess of 50% may be established by the operator provided that the operator demonstrates to the competent authority that the proximity to the fato and accuracy enhancements of the wind measuring equipment provide an equivalent level of safety .4 the operating techniques and.5 the operation of any systems that have an adverse effect on performance exemple 221 Most, 50% of the reported headwind component.

Question 113-4 : In straight and level flight at constant indicated airspeed a reduction in pressure altitude ?

Reduces the power required

exemple 225 Reduces the power required.

Question 113-5 : In the context of performance planning dr means ?

The horizontal distance travelled from the end of the take off distance available

Distance dr dr is the horizontal distance that the helicopter has travelled from the end of the take off distance available . 698 exemple 229 The horizontal distance travelled from the end of the take-off distance available.

Question 113-6 : In the cruise a helicopter with performance class 3 must be able to fly at ?

The minimum flight altitude

exemple 233 The minimum flight altitude.

Question 113-7 : In which document is an official 'power required chart' to be found ?

In the 'helicopter flight manual'

exemple 237 In the 'helicopter flight manual'.

Question 113-8 : Landing distance required means ?

The distance from a specified point on the approach until the helicopter comes to rest


Question 113-9 : Large rotorcraft are those of maximum weight of ?

9072 kg 20000 lbs or more

Large rotorcraft are classified in .accordance of cs 29 exemple 245 9072 kg (20000 lbs or more).

Question 113-10 : Ldrh is the horizontal distance required to land ?

And stop completely from a point 50 ft above the landing surface

Annex 6 operation of aircraft helicopter part 3 .landing distance required ldrh the horizontal distance required to land and come to a full stop from a point 15 m 50 ft above the landing surface

Question 113-11 : Maximum endurance ?

Will be achieved by flying with minimum fuel flow kg/h

exemple 253 Will be achieved by flying with minimum fuel flow (kg/h).

Question 113-12 : Maximum range for a helicopter ?

Will be obtained at the optimum altitude

exemple 257 Will be obtained at the optimum altitude.

Question 113-13 : Minimum weather limits are applied to helicopter class 3 operations these are ?

Cloud ceiling is less than 600 ft above local surface

Cat pol h 400 general. .d operations shall not be conducted .1 out of sight of the surface .2 at night .3 when the ceiling is less than 600 ft or.4 when the visibility is less than 800 m exemple 261 Cloud ceiling is less than 600 ft above local surface.

Question 113-14 : On the take off of a performance class 2 helicopter from an elevated heliport the take off weight must be such that if one engine becomes inoperative at or after dpato ?

The helicopter may continue its flight

Dpato defined point after take off exemple 265 The helicopter may continue its flight.

Question 113-15 : Performance class 3 helicopters are certified in ?

Category a or b

exemple 269 Category a or b.

Question 113-16 : Performance class 3 may be defined for a single engined helicopter such that if an engine becomes inoperative ?

A forced landing will result

exemple 273 A forced landing will result.

Question 113-17 : Performance class 3 operations to or from helidecks are ?

Never made

exemple 277 Never made.

Question 113-18 : Performance planning is required to ensure that ?

The space required for a manoeuvre is less than the space available

Performance planning refers to weight calculation in order to safely manoeuvring the helicopter if the space required for a manoeuvre the clearance path for take off or landing is equal or greater than the space available you will not be able to perform the manoeuvre exemple 281 The space required for a manoeuvre is less than the space available.

Question 113-19 : Performance such that in the event of failure of a critical power unit enables a helicopter to land within the rejected take off distance available is ?

Performance class 1

exemple 285 Performance class 1.

Question 113-20 : R means ?

Rotor radius

Cat pol h 110 exemple 289 Rotor radius.

Question 113-21 : Small rotorcraft are those of maximum weight of ?

3175 kg or 7000 lbs

exemple 293 3175 kg (or 7000 lbs).

Question 113-22 : The rate of climb will be negative affected by ?

High temperature high pressure altitude contaminated rotor blades

exemple 297 High temperature, high pressure altitude, contaminated rotor blades.

Question 113-23 : A helicopter with performance class 3 shall be able to maintain the minimum altitude that allows it to fly ?

Above the minimum prescribed altitude at maximum continuous power

Cat pol h 410 en route.a the helicopter shall be able with all engines operating within the maximum continuous power conditions to continue along its intended route or to a planned diversion without flying at any point below the appropriate minimum flight altitude .b except as provided in cat pol h 420 in the event of an engine failure the helicopter shall be able to perform a safe forced landing exemple 301 Above the minimum prescribed altitude at maximum continuous power.

Question 113-24 : The 'density altitude' is ?

The altitude in the standard atmosphere at which the prevailing density occurs

exemple 305 The altitude in the standard atmosphere at which the prevailing density occurs.

Question 113-25 : The 'maximum operating altitudes' of a certain helicopter are laid down in ?

The helicopter flight manual

exemple 309 The helicopter flight manual.

Question 113-26 : The abbreviation vle means ?

Maximum landing gear extended speed

exemple 313 Maximum landing gear extended speed.

Question 113-27 : The abbreviation vlo means ?

Maximum landing gear operating speed

exemple 317 Maximum landing gear operating speed.

Question 113-28 : The abbreviation vne means ?

Never exceed speed

exemple 321 Never exceed speed.

Question 113-29 : The abbreviation vtoss means ?

Take off safety speed for a category a rotorcraft

exemple 325 Take-off safety speed for a category a rotorcraft.

Question 113-30 : The abbreviation vy means ?

Speed for best rate of climb

exemple 329 Speed for best rate of climb.

Question 113-31 : The absolute ceiling of a helicopter as specified in its performance data is the altitude at which the helicopter is ?

No longer able to climb at all

exemple 333 No longer able to climb at all.

Question 113-32 : The altitude calculated by 'pressure altitude +/ 118 8 x temperature deviation from isa' is ?

Density altitude

The density altitude is used to determine a helicopters performance exemple 337 Density altitude.

Question 113-33 : The density altitude ?

Is used to determine a helicopters performance

exemple 341 Is used to determine a helicopters performance.

Question 113-34 : The distance necessary for a landing is the horizontal distance required to land ?

And come to a full stop from a point 50 ft above the landing surface

Annex 6 operation of aircraft helicopter part 3 .landing distance required ldrh the horizontal distance required to land and come to a full stop from a point 15 m 50 ft above the landing surface exemple 345 And come to a full stop from a point 50 ft above the landing surface.

Question 113-35 : The distance required for an aborted take off is the horizontal distance required between the start of the take off and the point where the helicopter stops following the failure of ?

The critical engine and the interruption of the take off at the take off decision point

exemple 349 The critical engine and the interruption of the take off at the take off decision point.

Question 113-36 : The effect of wind on angle of climb path will be ?

Headwind will increase the angle of climb path

exemple 353 Headwind will increase the angle of climb path.

Question 113-37 : The effect of wind on rate of climb roc will be ?

Nil

exemple 357 Nil

Question 113-38 : The main end product of performance planning is ?

The maximum mass of the aircraft at different phases of flight

exemple 361 The maximum mass of the aircraft at different phases of flight.

Question 113-39 : The maritime zone located north of latitude 50 n is considered hostile ?

Even if a safe emergency landing can be carried out

exemple 365 Even if a safe emergency landing can be carried out.

Question 113-40 : The mass of a helicopter with performance class 3 must be such that the following is always possible ?

A hover ige

exemple 369 A hover ige.


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