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Robinson R22 Beta II

Technical Specs:

Brake Horsepower: 180
5 Min. Takeoff Horsepower: 131
Maximum Continuous Horsepower: 124
Maximum Gross Weight: 1370lbs
Empty Weight: 855lbs
Maximum Weight per seat: 240lbs
Minimum pilot weight: 130lbs
Rotor blade Diameter: 25feet 2inches
Rotor blade Chord: 7.2inches
Tail Rotor Diameter: 42inches
Tail Rotor Chord: 4inches
Engine: Lycoming 0-360-J2A (4 cylinders)
Vne Speed: 102 knots
Maximum Density Altitude: 14,000feet MSL
Maximum Fuel Capacity Main Tank: 19.8gallons
Maximum Fuel Capacity Aux. Tank: 10.9 gallons
Maximum Rate of Descent: 1500fpm
Maximum Rate of Climb: 1000+ fpm
Rotor System: Semi-Rigid

Robinson R44 Clipper II

Technical Specs:

Not Available at this time.

Robinson R44 Raven I

Technical Specs:

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

Robinson R44 Raven II

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

Robinson R44 Clipper

Technical Specs:

Brake Horsepower: 260
5 Min. Takeoff Horsepower: 225
Maximum Continuous Horsepower: 205
Maximum Gross Weight: 2400lbs
Empty Weight: 1466lbs
Maximum Weight per seat: 300lbs
Minimum pilot weight: 150lbs
Rotor blade Diameter: 33feet
Rotor blade Chord: 10inches
Tail Rotor Diameter: 58inches
Tail Rotor Chord: 5.1inches
Engine: Lycoming 0-540-F1B5 (6 cylinders)
Vne Speed: 130 knots
Maximum Density Altitude: 14,000 MSL
Maximum Fuel Capacity Main Tank: 31.6gallons
Maximum Fuel Capacity Aux. Tank: 18.5gallons
Maximum Rate of Descent: 1300fpm
Maximum Rate of Climb: 1000+ fpm
Rotor System: Semi-Rigid

Enstrom 280c

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

Schweizer 300C

Technical Specs:

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

Schweizer 300CBi

Technical Specs:

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.

Schweizer 333

Technical Specs:

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