Statistical Data

 Wing Span

 28.5 ft.

 Fuselage Length

 25.7 ft.

 Maximum Height

 9.4 ft.

 Cockpit Width

 29.5 in. (front) 28 in. (rear)

 Wing Area

 101 sq. ft.

 Aspect Ratio

 8.0

 Wing Loading

 24 lbs./sq. ft. (solo), 32.6 lbs./sq. ft. (gross)

 G-Limits (at 2700 lbs.)

 +6, -4 (limit) +9, -6 (ultimate)

 Gross Weight

 3300 lbs.

 Empty Weight

 2050 lbs.

 Baggage Capacity

 120 lbs. or 10.1 cu. ft.

 Fuel Capacity

 100 gals. std.

 Engine

 Walter M601 series Turbine

 AVIA 3-Blade Propeller

 V508E/84" dia. constant speed, reversing

Performance Data

 Vso, Stall Speed

 66 mph. (57 kts.) solo

 Vso, Landing Configuration

 76 mph. (66 kts.) gross

 Maneuvering Speed

 300 mph. (261 kts.)

 Vne, Never Exceed Speed (design)

 400 mph. (348 kts.)

 Max Speed @ sea level

 315 mph. (274 kts.) 100% torque

 Roll Rate

 190 degrees/second

 Best Rate of Climb Speed

 150 mph. (130 kts.)

 Best Angle of Climb

 120 mph. (104 kts.)

 Climb Rate @ sea level

 6500 FPM (solo) 5500 FPM (gross)

Cruise Performance

Torque

Speed

Range

 Typical @ 17,500

66%

 338 mph. (294 kts.)

 718 SM

(625 NM)

 Economy @ 17,500

42%

 282 mph. (245 kts.)

 856 SM

(745 NM)

 Typical @ 25,000

49%

 333 mph. (290 kts.)

 943 SM

(821 NM)

 Economy @ 25,000

31%

 282 mph (245 kts.)

 1141 SM

(993 NM)