McMullan Aircraft Design

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Construction Materials

‚ Steel tube fuselage with fiberglass shell gives excellent aerodynamics, light weight and safety

‚ Full composite wing

‚ Spring aluminum main gear

‚ The Vortex Magnum can be built as a taildragger or with tricycle gear

Click Here Click Here to see drawing of the fuselage structure

Wingspan 33 ft Fuselage Length 25 ft
Wing Area 164 ft2 Fuselage Height 7.5 ft
Aspect Ratio 6.73 Fuselage Width 53 in
Wing Loading 19.2 lbs/ft2 Empty Weight 1500 lbs
Fuel Capacity 80 Gallons US Gross Weight 3000 lbs


Calculated Performance Specifications

Calculations are based on the 350 hp Chevy 350 cubic inch engine with prop speed reduction unit. Calculations are computer based and may vary with each individual aircraft.

Max Speed @ 5500 ft msl 242 mph Cruise Speed @ 5500 ft msl 225 mph
Stall w/Flaps 61 mph Rate of Climb Sea Level 1,156 fpm

Plans

The Vortex Magnum is designed to be a plans only aircraft at this time. The plans for the horizontal stabilizer and elevator are completed. By downloading Autodesk's Whip Viewer, you can take a look at them.

Click Here Download the Autodesk Whip Viewer
Click Here Take a look at the Horizontal Tail Plan Sheet 1
Click Here Take a look at the Horizontal Tail Plan Sheet 2
To the left is a drawing of a typical horizontal tail rib. Each one is cut from 1/8" birch plywood.
To the right is a drawing of the horizontal tail in construction, with some of the fiberglass spar caps in place, before sheeting.
To the left is a closeup showing the aluminum spars and elevator hinge.

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by Jay S. McMullan. DO NOT copy in any form without the written, expressed
permission of Jay S. McMullan and/or his designees. All information contained
on this website or in any publication written by Jay S. McMullan is strictly
for entertainment purposes only! Use at your own risks!