Mailing List lml@lancaironline.net Message #32999
From: Marvin Kaye <marv@lancaironline.net>
Subject: Re: Experimental Safety and Insurability
Date: Thu, 24 Nov 2005 23:26:59 -0500
To: <lml>
Posted for Sky2high@aol.com:

 Maybe this can help Lancairians understand some high insurance  premiums.  I
 noticed a Kitplane's article "The Safe Homebuilt",  available on their
 website.  You may find that it  makes interesting reading.
 
 http://www.kitplanes.com/magazine/pdfs/1004-3335.pdf
 
 I have extracted the following text from the article:
 
 ……….
 As the vice president in charge  of homebuilt insurance at Avemco, Jim
 Lauerman cites two primary gauges for  homebuilt safety.  The first is wing
 loading. Wing loading is calculated by taking the maximum gross weight of the
 
 airplane and dividing that number by the number of square feet of wing area.
For
 homebuilt airplanes, wing loadings can vary from 10 pounds per square foot
for a
 Kitfox, to 15 pounds per square foot for an RV-7, to 33 pounds per square
 foot  for a Lancair IV-P. Wing loading is often used in preliminary design
 calculations to predict landing speeds. In Lauerman’s experience, wing
 loading is
 directly proportional to severity of loss.
 The second criterion Lauerman  uses is how well tested a design is. For
 example, the Van’s Aircraft RV-6 is a  well known and well tested design. If
a new
 design comes from a manufacturer  with a good track record, such as Van’s new
 RV-10, that manufacturer’s track  record counts, too.
 Beyond those two primary  criteria, there are issues of low-speed handling
 qualities and longitudinal  stability. It also helps if the plane was
designed
 by real engineers.  Lauerman says that you can look at the distance from the
 c.g. to the tail and  the size of the tail, and just from that you’ll be able
to
 tell something about  the aircraft’s handling. Also important as a predictor
 of safety is how well the  plane conforms to the manufacturer’s original
 design, especially for critical  items like the fuel system.
 Drifting more into insurability  than safety, Lauerman considers a three
 legged stool of aircraft, pilot and  operating environment, which includes
runway
 length and the availability of  crosswind runways. If one is marginal, the
 other two had better be solid.  Avemco provides discounts to customers  who
have
 taken the King Schools video on risk management, but Lauerman observes  that
 external pressures are seldom a factor in homebuilt accidents. Of more
 significance is whether, when selecting the aircraft, the pilot understands
what
 they have gotten themselves into.
 ……..
 Added Notes:
 (1) Lancair 320/360 at 1800  pounds is about 26 lbs per sq ft (70 sq ft wing
 area). The Quad City's  Challenger II that I built was 5.4#/sq-ft.  The
 Skymaster that I once  owned was 22#/sq-ft.
 (2) Underlining was added for  emphasis.
 
 Scott Krueger  AKA Grayhawk
 Lancair N92EX IO320 SB 89/96
 Aurora, IL  (KARR)
 
 
 
 
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