# STC SA00370SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: BLR Aerospace LLC., United States
- Description: Installation of dual aft body strakes
- Applied: May 31, 1996
- Status date: August 23, 2018
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A12CE](https://openairdocs.org/tcds/A12CE)
- Certificate PDF: https://openairdocs.org/files/sha256/78/ab/78ab5fc7d250f5da9ec127c0b8cc40aa386a83e2b91e27ef41a59cba2191aa6c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C35ACB48B9AC5FCB862582F7005E3A1B.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00370SE

## ADs that name it (0)

None.

## Approved models (3)

- Hawker Beechcraft Corporation 60 ([TCDS A12CE](https://openairdocs.org/tcds/A12CE))
- Hawker Beechcraft Corporation A60 ([TCDS A12CE](https://openairdocs.org/tcds/A12CE))
- Hawker Beechcraft Corporation B60 ([TCDS A12CE](https://openairdocs.org/tcds/A12CE))

## 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.

Un ited S tates of Am erica Department of Transportation - Federal Aviation Administration Supplemental Type Certificate

Number SA00370SE

This certificate, issued to BLR Aerospace, LLC 11002 29th Ave. West Everett, WA 98204

Part 23 of the Federal Aviation Regulations.

Original ProductType Certificate Number: A12CE Make: Beech Model: 60, A60, B60

Description of the Type Design Change: Installation of dual aft body strakes in accordance with Master Drawing List Document BL-2004, and Installation Manual Document BL-2007, both dated August 20, 1996, or later FAA-approved revisions.

This modification requires the installation of BLR Aerospace vortex generators per STC SA5761NM or winglets per STC SA00112SE.

Replace any missing or damaged aft body strakes prior to further flight.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only.

This approval should not be extended to other aircraft of these models 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 to the airworthiness of the aircraft. A copy of this Certificate and FAA-Approved Aircraft Flight Manual Supplement, Document Number AFMS-B60-8, dated August 28, 1996, or later FAA-approved revisions must be maintained as part of the permanent records for the modified aircraft.

Date of application: May 31, 1996 Date reissued: November 23, 2009; August 23, 2018 Date of issuance: August 28, 1996 Date amended:

FAA FORM 8110-2 (5/14) PAGE 1 OF 2 PAGES By direction of the Administrator

(Signature)

Manager, Seattle ACO Branch (Title)

## Every issue (2)

- August 23, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/78/ab/78ab5fc7d250f5da9ec127c0b8cc40aa386a83e2b91e27ef41a59cba2191aa6c)
- November 23, 2009: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/f0/97/f097e2a0c3f3f76941b37c9549b9b58613e3624cfa73680a197209f98d930779)

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