# STC SA4733NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Raisbeck Engineering Inc., United States
- Description: Installation of lower aft fuselage strakes.
- Applied: March 31, 1989
- 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/sha256/90/6f/906f3b8bc1b9548fd66255483ffaa8e64ca7eb0d26b3b221e0012350f887bd6e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179294092320231004143021.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA4733NM

## ADs that name it (0)

None.

## Approved models (2)

- Hawker Beechcraft Corporation 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 300LW ([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 SA4733NM Raisbeck Engineering Inc.

2811 South 102nd Street, Suite 100 Tukwila, WA 98168 Part 23 the Federal Aviation Regulations A24CE Beech 300/300LW Installation of lower aft fuselage strakes in accordance with FAA Approved Raisbeck Engineering Drawing List 89-1004, initial release or later FAA Approved revisions.

March 31, 1989 September 1, 2023 May 18, 1989 for Manager, West Certification Branch The approval of this change in type design applies basically to the above model aircraft only. This approval should not be extended to other aircraft of this model on which previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate shall be maintained as part of the permanent records for 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 SA4733NM

## Every issue (2)

- September 1, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/90/6f/906f3b8bc1b9548fd66255483ffaa8e64ca7eb0d26b3b221e0012350f887bd6e)
- May 18, 1989: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/e7/ae/e7ae35bcf1d117d94fe1b01aa5b3760470842990f5c97f322449ffd3845fa6d0)

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