# STC SA5151NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Raisbeck Engineering Inc., United States
- Description: Installation of dual aft body strakes.
- Applied: March 20, 1991
- Status date: September 1, 2023
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/58/db/58dbba3caff7509c6b6c22d42588a732cb79e26b4760aa1a13be0d85ef919a6d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111719611820231005155325.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA5151NM

## ADs that name it (0)

None.

## Approved models (2)

- Raytheon Aircraft Company B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B300C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))

## 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 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Page 1 of 2 SA5151NM Raisbeck Engineering Inc.

2811 South 102nd Street, Suite 100 Tukwila, WA 98168 Part 23 the Federal Aviation Regulations A24CE Raytheon (Beech) B300 and B300C Installation of dual aft body strakes in accordance with Raisbeck Engineering Drawing List Number 91-1004, Rev. L, dated May 8, 2009, or later FAA-approved revisions to this document.

March 20, 1991 September 1, 2023 April 29, 1991 December 23, 1992, June 15, 2009 for Manager, West Certification Branch Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft on which other previously-approved modifications are incorporated unless it is determined that the relationship between this change and any other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft.

A copy of this certificate, Raisbeck Engineering Drawing Number 91-1004, and Airplane Flight Manual Supplement 91-111, Revision D, dated June 15, 2009, or later FAA-approved revisions to any of these documents must be maintained as part of the permanent records of the modified 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.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Page 2 of 2 SA5151NM

## Every issue (2)

- September 1, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/58/db/58dbba3caff7509c6b6c22d42588a732cb79e26b4760aa1a13be0d85ef919a6d)
- June 15, 2009: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/56/de/56de8947f3d385a73bf5d368c70e560c2f150abc30793746703c5008bcc4bb95)

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