Airplane Kit Manufacturing

Of  The 

Phoenix II

Specifications:

Engine: Two-Stroke Rotax 582, 65 hp, water-cooled.

Rpm: 6,500 (max), 5,700 (cruise)

Propeller: 68” Warp Drive 3-blade ground adjustable

Chord: 5’0”

Span: 32’6”

Wing Area: 162.5 sq. ft. (177.5 sq. ft. with allerons)

Dihedral: 4 deg.

Wing Incidence: 1.5” degrees

Length: 18’0”

Empty Weight: 475 lbs (inc. 1 gal. Of fuel and water for the radiator)

 Gross Weight: 616 lbs (single-place, est.); 791 lbs. (2 * 175 lbs. Pilot and student, plus 60 lbs. Fuel, est. max.)

 Fuel: 10 gal.

Load Limits: +6.0 g, -2.5 g

Wing Loading: 3.97 lbs./ sq. ft., (1-place est.) 4.87 lbs/ sq. ft., 2-place, est. )

Power Loading: 8.8 lbs./hp, (1-place, est.) 11.3 lbs./hp, (2-place, est.)

Cruise Speed: 55 mph (est.) 38 mph (1-place, max. est. L/D) 46 mph (2-place, max. est. L/D)

VNE: 72 mph

Stall Speed: 29 mph (1-place), 34 mph (2-place)

Climb: 1,000 fpm (1-place, est.), 575 fpm (2-place, est.)

Sink rate: 475 fpm (1-place, est.), 575 fpm (2-place, est.)

Take-off Distance: 100-150’ (1-place), 500’ (2-place, est.)

Landing Distance: 100-150’ (1-place), 500’ (2-place, no brake used, est.)