# STC SA1649CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: D'Shannon Products Ltd.
- Description: Installation of either the tail safe support angles or a stub spar at the 3% chord station on the root rib of horizontal stabilizer.
- Status date: September 28, 2011
- Data sheets: 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15
- Certificate PDF: https://openairdocs.org/files/sha256/2a/f9/2af97228aba6d457ade427056ae335a8d278ab52ca45c5e35a811276de16707a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BF6BF31211BA17738625792C006F900C.0001
- Page: https://openairdocs.org/stc/SA1649CE

## ADs that name it

- [AD 94-20-04 R2](https://openairdocs.org/ad/94-20-04-R2): Empennage aft fuselage · Remove V tail and install a Beech Model F33A straight tail (D'Shannon Products STC SA2149CE). Effective Jun 27, 2003
- [AD 94-20-04 R1](https://openairdocs.org/ad/94-20-04-R1) (historical): V-tail · Remove V tail and install a Beech Model F33A straight tail (D'Shannon Products STC SA2149CE). Effective Dec 10, 2002
- [AD 94-20-04](https://openairdocs.org/ad/94-20-04) (historical): V-Tail Structure · Remove V tail and install a Beech Model F33A straight tail (D'Shannon Products STC SA2149CE). Effective Nov 28, 1994

## Approved models (10)

- Hawker Beechcraft Corporation H35 (TCDS 3A15)
- Hawker Beechcraft Corporation J35 (TCDS 3A15)
- Hawker Beechcraft Corporation K35 (TCDS 3A15)
- Hawker Beechcraft Corporation M35 (TCDS 3A15)
- Hawker Beechcraft Corporation N35 (TCDS 3A15)
- Hawker Beechcraft Corporation P35 (TCDS 3A15)
- Hawker Beechcraft Corporation S35 (TCDS 3A15)
- Hawker Beechcraft Corporation V35 (TCDS 3A15)
- Hawker Beechcraft Corporation V35A (TCDS 3A15)
- Hawker Beechcraft Corporation V35B (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.

This Certificate issued to

Part 3 of the Civil Air Regulations.

Description of Type Design Change: Installation of either the Tail Safe support angles or a Stub Spar at the 3% chord station on t he root rib of the horizontal stabilizer per Smith Speed conversions Drawing List No. 1006 with an FAA Approved date of May 8, 1981, or later.

Limitations and Conditions: This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane. Approval of this STC does not constitute authority to produce parts for sale. The installer must determine whether this design change is compatible with previously approved modifications. 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.

D’Shannon Products, Ltd.

1309 County Road 134 Buffalo, MN 134 3A15 Make : Beech Model : H35; J35; K35; M35; N35; P35; S35; V35; V35A; V35B

Date of application : April 3, 1981

Date of issuance : May 8, 1981

Date reissued : January 26, 1993; October 12, 1982;

September 28, 2011

Date amended : November 26, 1984; October 19, 1984

( Signature) S. Frances Cox Manager, Special Certification Office Southwest Region

(Title)

## Every issue (1)

- September 28, 2011: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/2a/f9/2af97228aba6d457ade427056ae335a8d278ab52ca45c5e35a811276de16707a)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.