# STC SA2287NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc, United States
- Description: Installation of tail stabilizer support.
- Status date: December 13, 2016
- 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/de/ae/deae1739b2ca37c79f8c797c8cdfcd0cb0c8950a9f7ad6af781fd06ff81d0989
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/966D0DBD219A05C88625814D0044A33D.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2287NM

## ADs that name it (3)

- [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. Cited in the text
- [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. Cited in the text
- [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. Cited in the text

## Approved models (8)

- Hawker Beechcraft Corporation H35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation J35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation K35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation M35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation N35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation P35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation S35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation V35 ([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 (5/14) Page 1 of

Part of the

Signature

Title Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 2 SA2287NM Civil Air Regulations * 3 3A15 H35, J35, K35, M35, N35, P35, S35, V35 Installation of tail stabilizer support in accordance with B&N Industries Report No. 1 dated April 28, 1984. Parts manufactured in accordance with FAA sealed B&N Industries Drawings 1000 "NC" dated March 28, 1984 and 1001 "NC" dated January 25, 1984, or later FAA approved revisions.

Beech *as amended to May 15, 1956 including Amendment 3-8.

The approval of this change in type design applies to the basic aircraft of the specified models that are otherwise unmodified. This approval should not be extended to other specific aircraft of these models 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 introduce no adverse effect upon the airworthiness of the aircraft. 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.

May 15, 1987; April 15, 1996; March 26, 2007;

December 13, 2016 January 12, 1984 June 5, 1984 Mark Fuller STC ODA administrator ODA-100129-CE

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

## Every issue (2)

- December 13, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/de/ae/deae1739b2ca37c79f8c797c8cdfcd0cb0c8950a9f7ad6af781fd06ff81d0989)
- March 26, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/42/94/4294717c7b79a953f38f4d61a8d0a84aede4bbe187299ed7a8b876039bc4731e)

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