Un compte Premium offert sur le site FCL.055 ! Rendez-vous sur www.fcl055-exam.fr puis créez un compte avec le même email que celui...   [Lire la suite]


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 ?

Attainment > AIM

exemple reponse 208
Most 5 % of reported headwind component. cat pol h 105 general c) when showing compliance with requirements of this section account shall be taken of following parameters 1) mass of helicopter 2) helicopter configuration 3) environmental conditions in particular i) pressure altitude temperature ii) wind a) except as provided in (c) take off take off flight path landing requirements accountability wind shall be no more than 50% of any reported steady headwind component of 5 kt or more b) where take off landing with a tailwind component permitted in afm in all cases 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 point of take off landing wind components in excess of 50% may be established the operator provided that operator demonstrates to competent authority that proximity to fato accuracy enhancements of wind measuring equipment provide an equivalent level of safety 4) operating techniques and 5) operation of any systems that have an adverse effect on performance.



In straight and level flight at constant indicated airspeed a reduction in pressure altitude ?

exemple reponse 209
In straight and level flight at constant indicated airspeed a reduction in pressure altitude Reduces power required. cat pol h 105 general c) when showing compliance with requirements of this section account shall be taken of following parameters 1) mass of helicopter 2) helicopter configuration 3) environmental conditions in particular i) pressure altitude temperature ii) wind a) except as provided in (c) take off take off flight path landing requirements accountability wind shall be no more than 50% of any reported steady headwind component of 5 kt or more b) where take off landing with a tailwind component permitted in afm in all cases 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 point of take off landing wind components in excess of 50% may be established the operator provided that operator demonstrates to competent authority that proximity to fato accuracy enhancements of wind measuring equipment provide an equivalent level of safety 4) operating techniques and 5) operation of any systems that have an adverse effect on performance.

In the context of performance planning DR means ?

exemple reponse 210
In context of performance planning dr means The horizontal distance travelled from end of take off distance available. Distance dr dr the horizontal distance that helicopter has travelled from end of take off distance available .

  • exemple reponse 211
    In cruise a helicopter with performance class 3 must be able to fly at The minimum flight altitude. Distance dr dr the horizontal distance that helicopter has travelled from end of take off distance available .

  • exemple reponse 212
    In which document an official 'power required chart' to be found In 'helicopter flight manua. Distance dr dr the horizontal distance that helicopter has travelled from end of take off distance available .

  • exemple reponse 213
    Landing distance required means The distance from a specified point on approach until helicopter comes to rest. Distance dr dr the horizontal distance that helicopter has travelled from end of take off distance available .

  • exemple reponse 214
    Large rotorcraft are those of maximum weight of 9 72 kg (2 lbs or more). Large rotorcraft are classified in accordance of cs 29.

  • Question 97-8

    Ldrh the horizontal distance required to land And stop completely from a point 5 ft above landing surface. Annex 6 operation of aircraft helicopter (part 3) landing distance required (ldrh) the horizontal distance required to land come to a full stop from a point 15 m (50 ft) above landing surface.

  • Question 97-9

    Maximum endurance Will be achieved flying with minimum fuel flow (kg/h). Annex 6 operation of aircraft helicopter (part 3) landing distance required (ldrh) the horizontal distance required to land come to a full stop from a point 15 m (50 ft) above landing surface.

  • Question 97-10

    Maximum range a helicopter Will be obtained at optimum altitude. Annex 6 operation of aircraft helicopter (part 3) landing distance required (ldrh) the horizontal distance required to land come to a full stop from a point 15 m (50 ft) above landing surface.

  • Question 97-11

    Minimum weather limits are applied to helicopter class 3 operations these are Cloud ceiling less than 6 ft above local surface. Cat pol h 400 general d) operations shall not be conducted 1) out of sight of surface 2) at night 3) when ceiling less than 600 ft or 4) when visibility less than 800 m.

  • Question 97-12

    On take off of a performance class 2 helicopter from an elevated heliport 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.

  • Question 97-13

    Performance class 3 helicopters are certified in The helicopter may continue its flight. Dpato defined point after take off.

  • Question 97-14

    Performance class 3 may be defined a single engined helicopter such that if an engine becomes inoperative A forced landing will result. Dpato defined point after take off.

  • Question 97-15

    Performance class 3 operations to or from helidecks are A forced landing will result. Dpato defined point after take off.

  • Question 97-16

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

  • Question 97-17

    Performance such that in event of failure of a critical power unit enables a helicopter to land within rejected take off distance available The space required a manoeuvre less than space available. Performance planning refers to weight calculation in order to safely manoeuvring helicopter if space required a manoeuvre (the clearance path take off or landing) equal or greater than space available you will not be able to perform manoeuvre.

  • Question 97-18

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

  • Question 97-19

    Small rotorcraft are those of maximum weight of 3 75 kg (or 7 lbs). Performance planning refers to weight calculation in order to safely manoeuvring helicopter if space required a manoeuvre (the clearance path take off or landing) equal or greater than space available you will not be able to perform manoeuvre.

  • Question 97-20

    The rate of climb will be negative affected High temperature high pressure altitude contaminated rotor blades. Performance planning refers to weight calculation in order to safely manoeuvring helicopter if space required a manoeuvre (the clearance path take off or landing) equal or greater than space available you will not be able to perform manoeuvre.

  • Question 97-21

    A helicopter with performance class 3 shall be able to maintain minimum altitude that allows it to fly Above minimum prescribed altitude at maximum continuous power. Cat pol h 410 en route a) the helicopter shall be able with all engines operating within maximum continuous power conditions to continue along its intended route or to a planned diversion without flying at any point below appropriate minimum flight altitude b) except as provided in cat pol h 420 in event of an engine failure helicopter shall be able to perform a safe forced landing.

  • Question 97-22

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

  • Question 97-23

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

  • Question 97-24

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

  • Question 97-25

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

  • Question 97-26

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

  • Question 97-27

    The abbreviation vtoss means Take off safety speed a category a rotorcraft. Cat pol h 410 en route a) the helicopter shall be able with all engines operating within maximum continuous power conditions to continue along its intended route or to a planned diversion without flying at any point below appropriate minimum flight altitude b) except as provided in cat pol h 420 in event of an engine failure helicopter shall be able to perform a safe forced landing.

  • Question 97-28

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

  • Question 97-29

    The absolute ceiling of a helicopter as specified in its performance data the altitude at which helicopter No longer able to climb at all. Cat pol h 410 en route a) the helicopter shall be able with all engines operating within maximum continuous power conditions to continue along its intended route or to a planned diversion without flying at any point below appropriate minimum flight altitude b) except as provided in cat pol h 420 in event of an engine failure helicopter shall be able to perform a safe forced landing.

  • Question 97-30

    The altitude calculated 'pressure altitude +/ 118 8 x temperature deviation from isa' No longer able to climb at all. The density altitude used to determine a helicopters performance.

  • Question 97-31

    The density altitude Is used to determine a helicopters performance. The density altitude used to determine a helicopters performance.

  • Question 97-32

    The distance necessary a landing the horizontal distance required to land And come to a full stop from a point 5 ft above landing surface. Annex 6 operation of aircraft helicopter (part 3) landing distance required (ldrh) the horizontal distance required to land come to a full stop from a point 15 m (50 ft) above landing surface.

  • Question 97-33

    The distance required an aborted take off the horizontal distance required between start of take off and point where helicopter stops following failure of The critical engine the interruption of take off at take off decision point. Annex 6 operation of aircraft helicopter (part 3) landing distance required (ldrh) the horizontal distance required to land come to a full stop from a point 15 m (50 ft) above landing surface.

  • Question 97-34

    The effect of wind on angle of climb path will be Headwind will increase angle of climb path. Annex 6 operation of aircraft helicopter (part 3) landing distance required (ldrh) the horizontal distance required to land come to a full stop from a point 15 m (50 ft) above landing surface.

  • Question 97-35

    The effect of wind on rate of climb roc will be Headwind will increase angle of climb path. Annex 6 operation of aircraft helicopter (part 3) landing distance required (ldrh) the horizontal distance required to land come to a full stop from a point 15 m (50 ft) above landing surface.

  • Question 97-36

    The main end product of performance planning The maximum mass of aircraft at different phases of flight. Annex 6 operation of aircraft helicopter (part 3) landing distance required (ldrh) the horizontal distance required to land come to a full stop from a point 15 m (50 ft) above landing surface.

  • Question 97-37

    The maritime zone located north of latitude 50 n considered hostile Even if a safe emergency landing can be carried out. Annex 6 operation of aircraft helicopter (part 3) landing distance required (ldrh) the horizontal distance required to land come to a full stop from a point 15 m (50 ft) above landing surface.

  • Question 97-38

    The mass of a helicopter with performance class 3 must be such that following always possible Even if a safe emergency landing can be carried out. Annex 6 operation of aircraft helicopter (part 3) landing distance required (ldrh) the horizontal distance required to land come to a full stop from a point 15 m (50 ft) above landing surface.

  • Question 97-39

    The maximum indicated air speed of a helicopter in level flight reached At lowest possible altitude. Annex 6 operation of aircraft helicopter (part 3) landing distance required (ldrh) the horizontal distance required to land come to a full stop from a point 15 m (50 ft) above landing surface.

  • Question 97-40

    The minimum rate of descent in autoration will occur At vy rotor speed within limits. Annex 6 operation of aircraft helicopter (part 3) landing distance required (ldrh) the horizontal distance required to land come to a full stop from a point 15 m (50 ft) above landing surface.


Exclusive rights reserved. Reproduction prohibited under penalty of prosecution.

3839 Free Training Exam