What it approves
Installation of engine cowl and full length gear doors and relocation of engine oil cooler and replacement exhaust system. For PA-24-250, S/N 24-103 and up; for PA-24-260, S/N 24-3642, 24-4000 to 24-4782 and 24-4784 to 24-4803.
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.
FAA Form 8110-2 (03/21) Page 1 of ___ SA00343AT Aire Comanche Performance 10215 Shoshone Ave Northridge, CA 91325 Civil Air Regulations 3 Piper See Page 3 1A15 Installation of engine cowl and full length gear doors and relocation of engine oil cooler and replacement exhaust system in accordance with Aviation Performance Products, Inc. Master Drawing List No. MDL9201, Revision B, dated April 1, 1993 or later FAA approved revision.
See Page 3 3/29/92 5/2/01, 4/9/24 9/21/93 (for) Christina M. Underwood 3 (for) Christina M. Underwood Manager, East Certification Branch Compliance and Airworthiness Division Aircraft Certification Service
FAA Form 8110-2 (03/21) Page ___ of ___ SA00343AT Model: PA24250, S/N 24103 and up; PA24260, S/N 243642, 244000 to 244782 and 244784 to 244803
Limitations and Conditions: This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. 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.
NOTE: This STC was originally, erroneously assigned the number ST00343AT. Installations completed under this number are still valid.
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.