You are correct, technically, but the FAA has a list of specific aircraft that 
are are approved as LSA and it only includes the 415C and 415CD.

Bill 


To: [email protected]
CC: [email protected]; [email protected]
From: [email protected]
Date: Wed, 22 Jul 2009 14:02:22 -0500
Subject: Re: [ercoupe-tech] FW: is it a C or a D

  




You can make every change required to make a C a D but if the gross weight was 
never increased it is still a LSA. Remember, the only thing making a D a 
non-LSA is the gross weight. 

Larry Snyder
Washington, Missouri

On Jul 22, 2009, at 1:29 PM, Roy Stubbs <[email protected]> wrote:




  




Interesting wording – “if these modifications allowed it be become a CD or D 
model.”
 
What is important is if the model was legally changed, not what modifications 
allow it to be changed.
 
JMHO,
 
Roy
 




From: [email protected] [mailto:[email protected]] On 
Behalf Of Bill BIGGS
Sent: Wednesday, July 22, 2009 2:25 PM
To: ercoupe tech
Subject: [ercoupe-tech] FW: is it a C or a D
Importance: Low
 
  




 
> Subject: Ercoupe 415-C
> To: [email protected]
> From: [email protected]
> Date: Mon, 6 Aug 2007 14:26:43 -0500
> 
> 
> 
> 
> 
> Mr. Biggs
> 
> This in response to you email sent to the FAA with respect to your aircraft
> model type.
> 
> I have researched our records which indicate it came down the production
> line as a C model with the C-75-12 Continental engine.
> 
> The aircraft could however had some of the modifications of a D model done
> in its past. Univair Corporation is now the Type Certificate holder and may
> have any evidence if these modifications allowed it to become a CD or D
> model.
> 
> 
> FAA defines LSA as being: 
> · Simple, low-performance, low-energy aircraft including airplanes, 
> gliders, gyroplanes, balloons, airships, weight-shift control (trikes), 
> and powered parachutes. 
> · With a maximum weight of 1,320 pounds (1,430 pounds seaplanes). 
> · Single reciprocating engines (which includes diesel and rotary engines, 
> but does not allow jet engines). 
> · Maximum stall speed of 45 knots (52 mph with no lift-enhancing devices). 
> · Maximum top speed of 120 knots (138 mph). 
> · Fixed landing gear (except if equipped with amphibious floats, which can 
> be repositionable once in flight). 
> · Fixed-pitch propeller (unless equipment is ground-only repositionable). 
> 
> 
> 
> 
> 
> 
> Hope this information helps.
> 
> 
> Paul Vercellino
> Aviation Safety Inspector
> FAA AFW-FSDO




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