Design A clean-sheet design for private pilots Design Details Computational fluid dynamics including longitudinal stability using USM3D Navier-Stokes. Finite element analysis completed. CFR-title 14, subpart 23 using AGATE design allowables. Preliminary and critical design reviews completed including dynamic stability. Safety and Performance Predictable flight characteristics with excellent spin resistance and recovery. Highest IO-360 speed possible while having a 50mph stall with standard flaps. Specifications Design V-speeds VS0 Stall-w/Flaps @1400 lbs 50 mph TAS @2000 ft VS1 Stall–clean @1400 lbs 55 mph TAS @2000 ft VH Max Level Flight 230 mph TAS @10,000 ft (Stock IO-360) VH Max Level Flight 250 mph TAS @10,000 ft (Ly-con modified IO-360 with Hartzell 76CS03-2X2 blades and 3C1-R430A1X hub used for test bed) Design Loading and Flight Envelope Limit Load @ Gross Weight +6/-3 Gs (1.5 safety factor) VFE Max Full Flaps 100 KEAS VNE Not to Exceed Speed 225 KEAS TAS: 315 mph @10,000 ft VD Dive Speed 250 KEAS TAS: 350 mph @10,000 ft Weights and Dimensions Empty Weight 1095 lbs Gross Weight 1800 lbs Wing Span 28.42 ft Wing Area 113.5 sq ft Wing Loading @ Gross Weight 15.86 lbs per sq ft Wing Aspect Ratio 6.9 Washout .8053 deg @ airfoil station 20 (.820” from outboard tip) Aircraft Length 21.46 ft Height 8.15 ft Max Cabin Width 46″ Floor Board to Canopy 41“ Production Precise cradles and jigs for a fast, accurate build. Tooling and part manufacturing phase started. Certified material construction.