Technical Specs:

Not Available at this time.

 Weights
 Gross Weight: 2,400 lb
 Empty Weight Equipped (incl oil & avionics): 1,442 lb
 Standard Fuel (30.6 gal): 184 lb
 Auxiliary Fuel (18.3 gal): 110 lb
 Passengers and Baggage w/standard fuel: 774 lb

 Performance
 Cruise Speed: up to 130 mph (113 kts)
 Maximum Range (no reserve): approx 400 miles
 Hover Ceiling IGE @ 2400 lb: 6,400 feet
 Hover Ceiling OGE @ 2200 lb: 5,100 feet
 Rate-of-Climb: over 1,000 fpm
 Maximum Operating Altitude: 14,000 feet

 Technical Specs:

 Weights
 Gross Weight: 2,500 lb
 Empty Weight Equipped (incl oil & avionics): 1,506 lb
 Standard Fuel (30.6 gal): 184 lb
 Auxiliary Fuel (18.3 gal): 110 lb
 Passengers and Baggage w/standard fuel: 810 lb
 Passengers and Baggage w/ auxiliary fuel: 700 lb

 Performances
 Cruise Speed: up to 135 mph (117 kts)
 Maximum Range (no reserve): approx 400 miles (348   nm)
 Hover Ceiling IGE @ 2500 lb: 8,950 feet
 Hover Ceiling OGE @ 2300 lb: 7,500 feet
 Hover Ceiling OGE @ 2500 lb: 4,500 feet
 Rate-of-Climb @ 2500 lb & 6000 feet: over 1,000 fpm
 Maximum Operating Altitude: 14,000 feet

 Technical Specs:

 Brake Horsepower: 205 Hp Turbocharged
 5 Min. Takeoff Horsepower: No Limit up to 12,000 ft
 Maximum Continuous Horsepower: 205 Hp Turbocharged
 Maximum Gross Weight: 2350 lbs
 Empty Weight: 1659 lbs
 Maximum Weight per seat: No CG Limits
 Minimum pilot weight: No CG Limits
 Rotor blade Diameter: 32 feet
 Rotor blade Chord: 9.5 inches
 Tail Rotor Diameter: 4.67 feet
 Tail Rotor Chord: 4.4 inches
 Engine: Lycoming HIO-360-E1AE (4 cylinders)
 Vne Speed: 117 knots
 Maximum Density Altitude: 16,000 MSL
 Maximum Fuel Capacity Main Tank: 40.0 gallons

 Fuel Burn: 8 to 13.5 GPH
 Hover Ceiling – IGE 8800 feet
 Maximum Rate of Descent: 1500fpm
 Maximum Rate of Climb: 1125+ fpm
 Rotor System: Fully-Articulated 3 Blade

 Seats: 3

 IFR Equipped: Yes – Garmin 430

 Performance
 VNE(Kias) SeaLevel 95 knots 176 km/hr
 Cruise Speed 86 knots 159 km/hr
 Maximum Endurance 3.8 hrs 3.8 hrs
 Hover Ceiling IGE 10800 ft 3292 m
 Hover Ceiling OGE 8600 ft 2621 m

 Dimensions
 Height (overall) 8.72 ft 2.65 m
 Length (overall) 30.83 ft 9.40 m
 Fuselage length 22.19 ft 6.76 m
 Landing gear tread width 6.54 ft 1.99 m

 Weight
 Empty weight 1100 lbs 499 kg
 Gross weight 2050 lbs 930 kg
 Useful load 950 lbs 431 kg

 Power Plant
 Textron Lycoming H10-360 D1A
 Maximum Take Off 190 shp 141 kw
 Maximum Continuous 190 shp 141 kw

 Rotor System
 Main rotor diameter 26.83 ft 8.18 m
 Main rotor disk area 565 sq ft 52.49 sq m
 Main rotor RPM 471
 Tail rotor diameter 4.25 ft 1.30 m

 Fuel
 Standard capacity 32 gal 192 lbs 87 kg
 Auxiliary capacity 32 gal 192 lbs 87 kg

 Seating Capacity
 Training 2
 Utility 3

 Performance
 VNE(Kias) SeaLevel 94 knots 174 km/hr
 Cruise Speed 80 knots 148 km/hr
 Max Endurance (32 gal) 3.0 hrs 3.0 hrs
 Max Endurance (64 gal) 6.1 hrs 6.1 hrs
 Max Range (32 gal) 220 mi 353 km
 Max Range (64 gal) 430 mi 691 km
 Hover Ceiling IGE 7000ft 2133 m
 Hover Ceiling OGE 4800ft 1463 m
 (Hover Ceiling displayed at 1600ibs)

 Dimensions
 Height (overall) 8.72 ft 2.65 m
 length [overall) 30.83 ft 9.40 m
 Fuselage length 22.19 ft 6.76 m
 Landing gear tread width 6.54 ft 1.99 m

 Weight
 Empty weight 1088 lbs 493.5 kg
 Gross weight 1750 lbs 793.8 kg
 Useful load 662 lbs 300.0 kg

 Powerplant
 Textron Lycoming HIO-360-G1A Engine
 Maximum Take Off 180 shp 134 kw
 Maximum Continuous 180 shp 134 kw

 Rotor System
 Main rotor diameter 26.83 ft 8.18 m
 Main rotor disk areas 565 sq ft 52.49 sq m
 Main rotor RPM 471
 Tail rotor diameter 4.25 ft 1.30 m

 Fuel
 Standard capacity 32 gal 192 lbs 87 kg
 Auxiliary Fuel 32 gal 192lbs 87 kg

 Seating Capacity
 2
 Optional L/H P.I.C.

 Performance
 VNE(Kias) SeaLevel 120knots 222km/hr
 Cruise Speed 105 knots 192 km/hr
 Maximum Endurance 4.1 hrs
 Maximum Range 310nm 574km

 Weight
 Empty weight 1250 lbs 567 kg
 Gross weight 2550 lbs 1157 kg
 Useful load 1300 lbs 590 kg

 Rotor System
 Main rotor diameter 27.51 ft 8.39 m
 Main rotor disk area 594 sq/ft 55.18 sq/m
 Main rotor RPM 466 - 471 466 - 471
 Tail rotor diameter 4.25 ft 1.30 m

 Powerplant
 Rolls-Royce 250-C20W Gas Turbine Engine
 Maximum takeoff (Derated) 250 shp 186 kw
 Maximum continuous (Derated) 230 shp 171 kw

 Fuel (Turbine Fuel)
 Usable capacity (73 gal) 493 lbs 224 kg

 Weight
 Empty weight 1250 lbs 567 kg
 Gross weight 2550 lbs 1157 kg
 Useful load 1340 lbs 590 kg