STC SA02631AT

FAA FORM 8110-2(10-68) PAGE 1 of 1 PAGES United States of America Department of Transportation -- Federal Aviation Administration Supplemental Type Certificate Number SA02631AT This certificate issued to

Part 3 of the Civil Air Regulations.

Description of Type Design Change: Replace Lord Isolating Mounting Assemblies, P/N J-10520-1 with Lord Assembly P/N J- 23135-1.

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 determine by the installer that the interrelationship between this change and any 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." Installation eligibility is limited to aircraft certified in the utility category. Acrobatic category aircraft a re specifically excluded. Mount isolation system to be installed and maintained in accordance with Aviation Technical Consultants Instructions for Continued Airworthiness, document ATC 200903 Revision A dated 1/19/03, or later FAA Approved Revision.

James R. Moseley and/or Rita K. Moseley 61471 Palestine Road California, MO 65018 3A15 Make : Beech Model : 35-C33A; 36; A36; A36TC; B36TC; E33A; E33C; F33A;

F33C; G33; S35; V35; V35A; V35B Date of application : November 11, 2000

Date of issuance : February 13, 2003

Date reissued : March 12, 2007

( Signature) Melvin D. Taylor Manager Atlanta Aircraft Certification Office

( Title)