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61 Cards in this Set
- Front
- Back
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Basic Vne under 3000lbs gross weight |
130 kias, Vne decreases by 3.5 kias per 1000ft above 3000ft DA |
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Basic Vne over 3000lbs gross weight |
122 kias, Vne decreases by 7 kias per 1000ft about 3000ft DA |
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Vne with fwd doors off (training, no pax) |
110 kias |
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Vne with fwd doors off (pax) |
69 kias |
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Vne with rear doors off |
87 kias |
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Vne when above 85% Q |
80 kias |
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Max airspeed permitted for sideward or rearward flight |
30 kias |
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Max sidewards/rearwards airspeed above 3000lbs or above 3000ft DA |
17 kias |
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Max run-on landing with skis installed |
10 kts |
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Max airspeed in autorotation |
100 kias |
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Airspeed for max range at 90% Nr in autorotation |
69 kias |
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Airspeed for min descent rate at 90% Nr in autorotation |
52 kias |
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Max windspeed for start up or shutdown |
45 kts |
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Max gust spread for start up or shutdown |
15 kts |
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With less than 15 gals of fuel, what is your maximum angle of bank/pitch? |
10 degrees to prevent air ingestion into the fuel lines |
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Max operating altitude at or below 3000 lbs gross weight |
20 000 ft PA |
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Max operating altitude above 3000lbs |
13 500 ft DA |
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Starter duty cycle (Battery) |
40 sec on 1 min off 40 sec on 1 min off 40 sec on 30 min off |
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Starter duty cycle (GPU) |
25 sec on 30 sec off 25 sec on 30 sec off 25 sec on 30 min off |
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Max loadmeter at or below 8000 ft PA |
100% |
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Max loadmeter above 8000 ft PA |
70% |
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Recommended amps for external 28 VDC GPU |
350 to 450A |
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Allowed amperage for external 28 VDC GPU for engine start |
300 to 750 A |
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N1 Gas producer turbine rpm: idle range |
60-64% |
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N1 Gas producer turbine rpm: continuous range |
60 - 105% |
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N1 Gas producer turbine rpm: maximum transient |
106% for 15 seconds. Intentional use prohibited |
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N2 power turbine rpm: Continuous range |
97-100% |
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N2 power turbine rpm: Maximum above 30% Q |
100% |
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N2 power turbine rpm: max transient |
105% for 15 seconds |
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What range of N2 should steady state operations be avoided? |
71 - 88%, dwell time of no more than 1 second at any N2 speed in this range |
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Engine torque: Continuous range |
0 - 85% |
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Engine Torque: maximum at takeoff |
100%, do not exceed 5 minutes |
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Engine Torque: maximum transient |
110%, intentional use prohibited, do not exceed 5 seconds |
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TOT: Continuous range |
100 - 738 degrees |
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TOT: range at maximum takeoff power |
738 - 810, do not exceed 5 minutes |
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TOT: maximum transient range |
810 - 843 degrees, intentional use prohibited, do not exceed 6 seconds |
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TOT: maximum for starting and shutdown |
810 - 927 degrees, do not exceed 10 seconds |
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Eng oil px below 78.5% N1 range |
50 to 130 psi |
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Eng oil px between 78.5 - 94.2% N1 range |
90 - 130 psi |
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Eng oil px above 94.2% N1 range |
115 - 130 psi |
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Eng oil temp: normal range |
0 - 107 degrees |
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Fuel pressure range |
4 - 30 psi |
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Minimum fuel pressure when OAT < -18 °C, using JET-A, JET-A1, JP-5 |
8 psi |
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Transmission oil pressure: continuous range |
30 to 50 psi |
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Transmission oil px range: Maximum |
70 psi |
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Transmission oil temp range: Continuous |
15 - 110 degrees |
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Nr range for Power Off (autorotation) |
90 - 107% |
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Nr range for Power On |
97-100% |
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NR avoidance range during acceleration |
50 to 60% |
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Rotor Brake engagement range |
30 to 38% |
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Max external gross weight |
3350 lbs |
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Max internal gross weight |
3200 lbs |
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Min gross weight for flight |
2000 lbs |
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Min combined front seat weight for flight using range extender fuel capacity |
200 lbs |
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Min combined front seat crew weight |
170 lbs |
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Maximum weight in baggage compartment |
250 lbs |
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Maximum cargo loading limit (lbs/ft^2) |
86 lbs/ft^2 |
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Maximum baggage weight when using range extender fuel capacity and 3 pax in back |
110 lbs |
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Longitudinal CG range (all doors on, or aft cabin doors off) |
106.0 to 114.2 |
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Longitudinal CG with one or both fwd doors off, or fwd and aft doors off) |
106.0 to 110.0 |
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Lateral CG limits |
3 inches left, 4 inches right |
