# STC SA3819NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Raisbeck Engineering Inc., United States
- Description: Installation of nacelle overwing stowage lockers and lower flap fairing.
- Applied: January 6, 1987
- Status date: September 1, 2023
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A14CE](https://openairdocs.org/tcds/A14CE)
- Certificate PDF: https://openairdocs.org/files/sha256/16/2c/162cf4d3f49c81b92684483af7dd2062d8253d9530057462775a6a924180ee9c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142546577920231003174233.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA3819NM

## ADs that name it (0)

None.

## Approved models (3)

- Hawker Beechcraft Corporation 100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Hawker Beechcraft Corporation B100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Textron Aviation Inc. A100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))

## 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 SA3819NM Raisbeck Engineering Inc.

2811 South 102nd Street, Suite 100 Tukwila, WA 98168 Part 23 the Federal Aviation Regulations A14CE Beech 100, A100, and B100 Installation of nacelle overwing stowage lockers and lower flap fairing in accordance with FAA-approved Raisbeck Engineering List 86-1001, Revision IR, dated March 31, 1987, or later FAA-approved revisions.

January 8, 1987 September 1, 2023 April 1, 1987 May 30, 1990, July 20, 1990 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 of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those 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 and Raisbeck Engineering Drawing List 86-1001 shall 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 SA3819NM

## Every issue (2)

- September 1, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/16/2c/162cf4d3f49c81b92684483af7dd2062d8253d9530057462775a6a924180ee9c)
- July 20, 1990: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/8c/7c/8c7cef990678ae86a9b5976fa34faa846c365a026b0feeba6d75ea219326c908)

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