# STC SR00242SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Turbolyft USA Corporation, United States
- Description: Fabrication and Installation of a new instrument panel and pedestal
- Applied: September 7, 1995
- Status date: May 11, 2026
- Product: Aircraft, Rotorcraft
- Certification basis: Part 27
- Data sheets: [TCDS H11EU](https://openairdocs.org/tcds/H11EU), [TCDS H9EU](https://openairdocs.org/tcds/H9EU)
- Certificate PDF: https://openairdocs.org/files/sha256/09/05/0905b8d3ac908ec1b79ff29c21b2a344c09e9339a6d02bdc5e09673c5a3d2c59
- Approved model list and other attachments: [SR00242SE_AML.pdf](https://openairdocs.org/files/sha256/58/be/58be0193298547ba4cecd7cab2661b95143001ebeba16be1dad4034eecd438fe)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174510542820260715160251.0001
- DRS record last changed: July 15, 2026
- Page: https://openairdocs.org/stc/SR00242SE

## ADs that name it (0)

None.

## Approved models (10)

- Airbus Helicopters AS350B ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Airbus Helicopters AS350B1 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Airbus Helicopters AS350B2 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Airbus Helicopters AS350B3 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Airbus Helicopters AS350BA ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Airbus Helicopters AS350C ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Airbus Helicopters AS350D ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Airbus Helicopters AS350D1 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Airbus Helicopters AS355F1 ([TCDS H11EU](https://openairdocs.org/tcds/H11EU))
- Airbus Helicopters AS355F2 ([TCDS H11EU](https://openairdocs.org/tcds/H11EU))

## 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.

SR00242SE Turbolyft USA Corporation 9230 Highway 279 Brownwood, TX 76801 Part * * * * *See attached Federal Aviation Administration (FAA) Approved Model List (AML) SR00242SE for approved aircraft models and applicable airworthiness regulations Approval of this change in type design to the above model aircraft only. The AS355F1 and AS355F2 model aircraft shall be modified with the Heli-Lynx FX Mod Supplemental Type Certificate (STC) SR02015NY before installation of this STC. 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 changes in type design will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate, the AML, the MDL, and the ICA must be maintained as part of the permanent records of the modified rotorcraft.

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.

09/07/1995 09/29/2014 10/28/2015 11/16/2018 10/12/1995 01/18/2000 04/10/2009 04/15/2010 ✔ for Manager, West Certification Branch 3 Fabrication and Installation of a new instrument panel and pedestal per Geneva Aviation Master Drawing List (MDL) as listed on AML SR00242SE. This modification must be inspected and maintained in accordance with the FAA approved Instructions for Continued Airworthiness (ICA), document as listed on AML SR00242SE.

SR00242SE 05/11/2026 3

SR00242SE 05/11/2026 Date Reissued: 5/20/2022; 4/17/2024; 5/11/2026

-----------------------End------------------------ 3 3 Add Page

### SR00242SE_AML.pdf

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SR00242SE FOR**

FABRICATION AND INSTALLATION OF A NEW INSTRUMENT PANEL AND PEDESTAL ISSUE DATE: September 29, 2014 Page 1 of 1

**ITEM ROTORCRAFT MAKE**

**ROTORCRAFT MODEL**

**ORIGINAL TC NUMBER**

**CERTIFICATION**

**BASIS FOR**

**ALTERATION**

**FAA APPROVED**

**INSTRUCTIONS FOR**

**CONTINUED AIRWORTHINESS**

**FAA APPROVED MASTER**

DRAWING LIST AML REV DATE Number Revision** Drawin g Revision*

1. Airbus Helicopters AS350B, BA, B1, B2, B3, C, D, and D1 H9EU Part 27 ICA 162-2 Revision N/C, dated January 6, 2009 GA162 Revision F, dated August 25, 2010

2. Airbus Helicopters AS355F1 and AS355F2 H11EU Part 27 ICA 162-3 Revision N/C, dated February 10, 2010 GA162 Revision F, dated August 25, 2010 * Or later FAA Approved Revision **Or later FAA Accepted Revision FAA Approved:

For Manager, West Certification Branch AMENDED:

REISSUED: May 20, 2022; September 13, 2022; April 17, 2024;

May 11, 2026

## Every issue (5)

- May 11, 2026: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/09/05/0905b8d3ac908ec1b79ff29c21b2a344c09e9339a6d02bdc5e09673c5a3d2c59), [SR00242SE_AML.pdf](https://openairdocs.org/files/sha256/58/be/58be0193298547ba4cecd7cab2661b95143001ebeba16be1dad4034eecd438fe)
- May 20, 2022: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/9e/6c/9e6c722c3ece8793b9451fa945d9bb1eb0184fda0954ed554e80ebf78a1d8287), [AML SR00242SE.pdf](https://openairdocs.org/files/sha256/cf/1b/cf1ba5f5cf6bab453ed9913a18d18972f7d2a5a6aea8199516ef87c3263b1e71)
- November 16, 2018: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/fe/c5/fec5af0aea9f67240741aa496f9f2245dcf1acfc2a6aaecf03048f6cc516b5ab)
- October 28, 2015: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/45/a7/45a7c71b26b41c86d8fe6e13bc6769942b3f03acddaf678ca7d22f652dc708d2)
- April 15, 2010: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/36/2f/362fb57e9bff4b569b7d0312a84411f5af29d533d4fca81a4a5fbef15d0738ac)

---
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.