# STC SA01151AT

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: FFC Manufacturing, United States
- Description: Installation of left hand side and right hand side leading edge inboard fuel cell assemblies.
- Applied: May 17, 1996
- Status date: May 1, 2009
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A16](https://openairdocs.org/tcds/3A16), [TCDS A23CE](https://openairdocs.org/tcds/A23CE)
- Certificate PDF: https://openairdocs.org/files/sha256/af/58/af589a341ad01eded15820b5869b94602dfd7caebdc05e61882219d63be1261a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/03F7D0083150BF07862575BA00550C66.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01151AT

## ADs that name it (0)

None.

## Approved models (3)

- Hawker Beechcraft Corporation 58 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation 58P ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Hawker Beechcraft Corporation 58TC ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))

## 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.

This certificate issued to

Part * of the Regulations.

Installation of left and right side leading edge inboard fuel cell assemblies in accordance with A/C Fuel Cells Worldwide, Inc.,” Installation Instructions,” dated August 30, 1994; and A/C Fuel Cells Worldwide, Inc., Drawing B0301, Revision D, dated July 2, 1996, for the left hand side fuel cell; and Drawing B0302, Revision D, dated July 2, 1996, for the right hand side fuel cell; or later FAA approved revision.

(See continuation 3 of 3)

Limitations and Conditions: 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 interrelationship between this change and any of those other previously approved modifications will introduce no adverse effects upon the airworthiness of the 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.

FFC Manufacturing 4010 Pilot Dr., Suite 103 Memphis, TN 38118 3A16 Make: Beech Craft Model: BE-58, -58P, -58TC (See continuation 3 of 3)

Date reissued: July 31, 2002, May 01, 2009

Date amended: April 08, 1999

( Signature) Melvin D. Taylor Manager Atlanta Aircraft Certification Office

( Title)

Date of application: May 17, 1996

Date of issuance: September 06, 1996

FAA FORM 8110-2-1(10-69) PAGE 2 of 3 PAGES

Number SA01151AT

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

Number SA01151AT

Aircraft Model Eligibility:

Beech BE-58; S/N TH669 and up Beech BE-58P; S/N TJ91 and up Beech BE –58TC; S/N TK24 and up

Continuation Description of Type Design Change:

Left Hand Side Leading Edge Inboard Fuel Cell -P/N B0301-2

Right Hand Side Leading Edge Inboard Fuel Cell – P/N B0302-2

## Every issue (1)

- May 1, 2009: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/af/58/af589a341ad01eded15820b5869b94602dfd7caebdc05e61882219d63be1261a)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.