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Question		Answer
Maximum Continuous Cruise RPM start learning		7500 RPM
Maximum Continuous Climb RPM start learning		7800 RPM
Max Operational RPM start learning		8000 RPM for 2 minutes
Minimum In-Flight RPM start learning		3800 RPM
Maximum Static Full Throttle RPM start learning		7200 RPM
Minimum Static Full Throttle RPM start learning		6300 RPM
Minimum Cylinder Head Temperature start learning		80 deg C
Rotor Temperature Operating Range start learning		64-175 deg C
Max Transient Cylinder Head Temperature start learning		>259 deg C during a climb to 1000' AGL
Max Continuous Cylinder Head Temperature start learning		<249°C
Static Idle RPM (Payload & IFF start learning		3720+- 120 RPM
Battery Fail start learning		<19 VDC
Bus Voltage (w/ engine running) start learning		28 +- 2 VDC
Commanded Roll Tolerance start learning		+- 6 deg AOB
Roll: Knobs start learning		+-20 deg AOB
Pitch start learning		+20 -15 deg AOB
Roll: TALS start learning		+-25 deg AOB
Turbulence (Rough Air) start learning		70 KIAS
Maximum Airspeed Limits start learning		IAW Maximum Commanded Airspeed Chart
Low Airspeed Alert start learning		55 KIAS
Maximum Reported Airspeed (Descent) start learning		90 KIAS
TALS Automatic Abort (High) start learning		> 78 KIAS for 2 seconds
TALS Automatic Abort (Low) start learning		<52 KIAS for 2 seconds
Descent Law start learning		70-90 KIAS
Climb Law (Legacy/IE) start learning		65 KIAS / 62 KIAS
Fuel on Ground Limit w/ electric fuel pump start learning		10L
Capacity (Legacy/IE) start learning		44L / 58L
Minimum Altitude start learning		ELOS
Service Ceiling start learning		15000' MSL
Maximum Launch Altitude start learning		10,500' DA
Minimum Safe FTS Deploy start learning		500' AGL
Maximum Tailwind for Launch start learning		Refer to LAU Nitrogen Pre-Charge Pressure Charts
Maximum Headwind/Crosswind start learning		20 KTS / 25 KTS
Approach Tailwind (at Land AV) start learning		0 KTS
Landing Tailwind Component (Maximum) start learning		5 KTS

System Limitations

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