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Design

A clean-sheet design for private pilots

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.