Large rotorcraft are those of maximum weight of ?
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LDRH is the horizontal distance required to land ?
Maximum endurance ?
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. 
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. 
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. 
Performance class 3 helicopters are certified in The helicopter may continue its flight. Dpato defined point after take off. Question General 99 Answer 8
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 General 99 Answer 9
Performance class 3 operations to or from helidecks are A forced landing will result. Dpato defined point after take off. Question General 99 Answer 10
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 General 99 Answer 11
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 General 99 Answer 12
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 General 99 Answer 13
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 General 99 Answer 14
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 General 99 Answer 15
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 General 99 Answer 16
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 General 99 Answer 17
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 General 99 Answer 18
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 General 99 Answer 19
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 General 99 Answer 20
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 General 99 Answer 21
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 General 99 Answer 22
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 General 99 Answer 23
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 General 99 Answer 24
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 General 99 Answer 25
The density altitude Is used to determine a helicopters performance. The density altitude used to determine a helicopters performance. Question General 99 Answer 26
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 General 99 Answer 27
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 General 99 Answer 28
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 General 99 Answer 29
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 General 99 Answer 30
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 General 99 Answer 31
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 General 99 Answer 32
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 General 99 Answer 33
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 General 99 Answer 34
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. Question General 99 Answer 35
The never exceed speed vne of a helicopter as specified in flight manual May not be exceeded under any circumstances. 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 General 99 Answer 36
The part of take off path during which in a helicopter of performance class 2 an engine failure would result in a forced landing must be flown in Conditions of weather light in which a safe landing possible. 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 General 99 Answer 37
The ratio in same units and expressed as a percentage of 'change in height' divided 'horizontal distance travelle means Conditions of weather light in which a safe landing possible. The 'climb gradient' defined as ratio expressed as a percentage of change in geometric height divided the horizontal distance traveled gradient = (change in height/horizontal distance) x 100% for small angles of climb you can use rate of climb / true airspeed but this not exact definition of 'climb gradient'. Question General 99 Answer 38
The responsibility ensuring that performance claimed a helicopter can be achieved belongs to Conditions of weather light in which a safe landing possible. The 'climb gradient' defined as ratio expressed as a percentage of change in geometric height divided the horizontal distance traveled gradient = (change in height/horizontal distance) x 100% for small angles of climb you can use rate of climb / true airspeed but this not exact definition of 'climb gradient'. Question General 99 Answer 39
The speed maximum endurance Is always lower than speed maximum specific range. The 'climb gradient' defined as ratio expressed as a percentage of change in geometric height divided the horizontal distance traveled gradient = (change in height/horizontal distance) x 100% for small angles of climb you can use rate of climb / true airspeed but this not exact definition of 'climb gradient'. Question General 99 Answer 40
The speed maximum rate of climb Will be higher than speed best angle of climb. The 'climb gradient' defined as ratio expressed as a percentage of change in geometric height divided the horizontal distance traveled gradient = (change in height/horizontal distance) x 100% for small angles of climb you can use rate of climb / true airspeed but this not exact definition of 'climb gradient'.
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