What it approves
Installation of engine mount heat shield modification in accordance with Oregon Aircraft Design Drawing List DLPA30, dated September 24, 1999, (PA-30, PA-39) or DLPA30T, dated August 28, 1999 (Turbocharged PA-30, PA-39) or later FAA approved revisions to either document.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
Number SA01252SE
This certificate, issued to Fessler Aviation, Inc.
13342 80th Terrace Live Oak, FL 32060
Part 3 of the Civil Air Regulations.
Original ProductType Certificate Number: A1EA Make: New Piper (Piper) Model: PA-30, PA-39, Turbo PA-30, PA-39
Description of the Type Design Change: Installation of engine mount heat shield modification in accordance with Oregon Aircraft Design Drawing List DLPA30, dated September 24, 1999, (PA-30, PA-
39) or DLPA30T, dated August 28, 1999 (Turbocharged PA-30, PA-39) or later FAA approved revisions to either document.
Limitations and Conditions: Approval of this change in type design applies to the aircraft models listed above only. This approval should not be extended to other aircraft on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.
If the holder agrees to permit another person to use this Certificate to alter the product, the holder shall give the other person written evidence of that permission.
Date of application: July 29, 2003 Date reissued: January 20, 2004 Date of issuance: August 13, 2003 Date amended:
(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.