STC SA02205AK

This Certificate issued to

Part 3 of the Civil Air Regulations.

Description of Type Design Change: Removal of Piper PA-31 series main landing gear inboard doors, in accordance with American Aircraft Engineering drawing “Piper PA-31 MLG I/B Door Removal Procedure”, Document Number ST580-1, Revision None, dated December 12, 2002, or later FAA approved revision.

1. Compatibility of the design change with previously approved modifications must be determined by the installer.

2. Accomplishment of the actions in this STC, permanent removal of inboard main gear doors and hinge assemblies, removes the requirement for compliance with AD 2000-25-01.

3. 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.

Arthur King 3408 Spring Bluff Place Lauderhill, FL 33319

* See attached No. SA02205AK, FAA Approved Model List (AML), dated May 14, 2003, or later approved revision, for a list of approved airplane models and applicable airworthiness regulations.

Make: * Model: * Date of application: November 09, 2002

Date of issuance: May 14, 2003

Date reissued: February 19, 2013

( Signature) August A. Asay Manager, Anchorage Aircraft Certification Office

( Title)

FAA APPROVED MODEL LIST (AML) FOR Supplemental Type Certificate No. SA02205AK

Issue Date: May 14, 2003

AIRPLANE MAKE

AIRPLANE MODEL TYPE

CERTIFICATE NUMBER

CERTIFICATION

BASIS FOR

ALTERATION Piper PA-31, PA-31-300 PA-31-325, PA-31-350

A20SO CAR 3 Piper PA-31P, PA-31T, PA-31T1, PA-31T2, PA-31T3, PA-31P-350

A8EA CAR 3