# STC SA02631AT

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Mosely James R. and/or Rita K., United States
- Description: Replace Lord Isolating Mounting Assemblies, P/N J-10520-I with Lord Assembly P/N J-23135-1, four each.
- Applied: November 11, 2000
- Status date: March 12, 2007
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15)
- Certificate PDF: https://openairdocs.org/files/sha256/0f/2b/0f2b66a90af970c465fe18577e0a97db61f7eafbc266e0eefb0ca866422c2de6
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D08A789FD9FBD9B3862572B3006462EF.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA02631AT

## ADs that name it (0)

None.

## Approved models (14)

- Raytheon Aircraft Company 35-C33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company 36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company A36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company A36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company B36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company E33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company E33C ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company F33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company F33C ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company G33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company S35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company V35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company V35A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company V35B ([TCDS 3A15](https://openairdocs.org/tcds/3A15))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

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)

## Every issue (1)

- March 12, 2007: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/0f/2b/0f2b66a90af970c465fe18577e0a97db61f7eafbc266e0eefb0ca866422c2de6)

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