# STC SA00479SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: BLR Aerospace LLC., United States
- Description: Increased capacity fuel system (wet wing tips) manufactured
- Applied: November 23, 2009
- 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/sha256/75/10/75101168bf004d5b03a33adf57090ef4dca9a735c958c3cda7a97413c121df7a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3657B24E5B1FA6F1862582F7005E3D8B.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00479SE

## 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 SA00479SE

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, and B60

Description of the Type Design Change: Increased capacity fuel system (wet wing tips) manufactured in accordance with Document BL2021, initial release, dated November 12, 1997, installed in accordance with Document BL2022, initial release, dated November 12, 1997, and maintained in accordance with Document BL2020, initial release, dated November 12, 1997, or later FAA-approved revisions.

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 by the installer 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 FAA approved Flight Manual Supplement, Document Number AFMS-B60-10, initial release, dated November 12, 1997, or later FAA-approved revision must 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.

Date of application: October 31, 1996 Date reissued: November 23, 2009; August 23, 2018 Date of issuance: November 12, 1997 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/sha256/75/10/75101168bf004d5b03a33adf57090ef4dca9a735c958c3cda7a97413c121df7a)
- November 23, 2009: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/94/4e/944e61f822db623bd8e0c1df582597b0db9defdbc7b43810346fc2ea93bae6de)

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