Welcome to my Online Cootery

The Online Construction Record of Russ Milham's Taylor Coot-A Amphibian

WoW Check: 313 lbs

Home

Galleries

    New Shop!

    Acquisitions

Links

    Scrounging

    Cooting

Musings

    Comparisons

    Compromises

    My first look

Reference

     About this builder

    Contact
 

How does it stack up?

  Aviat Husky A1B (amphib) 8GCBC Scout (amphib) Coot-A
Engine Lycoming 0-360-A1P, 180hp Lycoming O-360-C1G, 180hp Various 150 - 220 hp
Propeller Constant Speed Constant Speed Constant Speed (typ)
Airfoil Modified Clark Y/USA 35B NACA 4412 NACA 4415
Wing Span 35ft 6in 36ft 2in 36ft
Length 22ft 7in 23ft 22ft
Wing Area sq ft. 183 180 180*
Gross Weight 2200 lbs 2150 1900* - 2170
Empty Weight 1368 lbs 1315 1450 - 1650 (typ)*
Useful Load (lb) 832 835 250 - 720 (550 practical)
Seats 2, tandem 2, tandem 2, abreast
Fuel Capacity (std) 52 US gal (50 usable) 35 US gal 30 (typ)
Stall (kts, ldg config) 45 50 43 (typ)
Rate of climb (fpm) 1500 1080 600 - 800 (typ)*
Price example ($US) $189,000 $169.500 Varies (but let's guess $30K)
Cost variance $159,000 $139,500 N/A
Useful load variance (lb) 282 285 N/A
Cost per additional lb $564 /lb $489 /lb N/A

* Steeves, R.  (1997).  The Coot Story.  Richard A Steeves.  Madison.

 
   

This page last updated on 05/18/2008