System Limitations

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Question English
Answer English

Maximum Continuous Cruise RPM
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7500 RPM

Maximum Continuous Climb RPM
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7800 RPM

Max Operational RPM
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8000 RPM for 2 minutes

Minimum In-Flight RPM
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3800 RPM

Maximum Static Full Throttle RPM
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7200 RPM

Minimum Static Full Throttle RPM
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6300 RPM

Minimum Cylinder Head Temperature
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80 deg C

Rotor Temperature Operating Range
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64-175 deg C

Max Transient Cylinder Head Temperature
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>259 deg C during a climb to 1000' AGL

Max Continuous Cylinder Head Temperature
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<249°C

Static Idle RPM (Payload & IFF
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3720+- 120 RPM

Battery Fail
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<19 VDC

Bus Voltage (w/ engine running)
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28 +- 2 VDC

Commanded Roll Tolerance
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+- 6 deg AOB

Roll: Knobs
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+-20 deg AOB

+20 -15 deg AOB

Roll: TALS
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+-25 deg AOB

Turbulence (Rough Air)
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70 KIAS

Maximum Airspeed Limits
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IAW Maximum Commanded Airspeed Chart

Low Airspeed Alert
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55 KIAS

Maximum Reported Airspeed (Descent)
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90 KIAS

TALS Automatic Abort (High)
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> 78 KIAS for 2 seconds

TALS Automatic Abort (Low)
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<52 KIAS for 2 seconds

Descent Law
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70-90 KIAS

Climb Law (Legacy/IE)
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65 KIAS / 62 KIAS

Fuel on Ground Limit w/ electric fuel pump
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10L

Capacity (Legacy/IE)
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44L / 58L

Minimum Altitude
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ELOS

Service Ceiling
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15000' MSL

Maximum Launch Altitude
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10,500' DA

Minimum Safe FTS Deploy
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500' AGL

Maximum Tailwind for Launch
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Refer to LAU Nitrogen Pre-Charge Pressure Charts

Maximum Headwind/Crosswind
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20 KTS / 25 KTS

Approach Tailwind (at Land AV)
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0 KTS

Landing Tailwind Component (Maximum)
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5 KTS


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