# STC SH2941SO-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Bell Helicopter Textron Inc., United States
- Description: Low skid landing gear.
- Applied: June 25, 1990
- Status date: August 2, 2013
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/b7/fe/b7fefe06a349af414c081bcbcd0344d237dda6ed6d8bcff8e2cc55ec0f1a78f5
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D5E2FEEB4823931D86257C7E0054FC93.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SH2941SO-D

## ADs that name it (0)

None.

## Approved models (4)

- Bell Helicopter Textron (Canada) 206L ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L-3 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L-4 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))

## 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.

Number SH2941SO-D

This certificate issued to: Bell Helicopter Textron, Inc.

441 Industrial Park Road Piney Flats, TN 37686

Part 6of the Civil Air Regulations.

Original Product – Type Certificate Number: H2SW

Make: Bell Helicopter Textron Canada Limited Model: 206L, L-1, L-3, L-4 Description of Type Design Change:

Low Skid Landing Gear in accordance with Aeronautical Accessories, Inc. Drawing List Report AA-90039, Revision A, dated February 18, 1991, and installation per Report AA-90038, No Revision, dated August 27, 1990, or later FAA /DAS approved revisions.

Instructions for Continued Airworthiness, Aeronautical Accessories, Inc. Report AA-01145, Revision A, dated March 27, 2003, and AA-01149, No Revision, dated September 7, 2001, or later AEG accepted revisions are required. The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

Date of application: June 25, 1990 Date reissued: August 2, 2013 Date of issuance: April 15, 1991 Date amended: 11/15/93; 3/11/98; 6/6/03

Signature Scott A. Horn

Title Acting Manager, Rotorcraft Certification Office, Southwest Region

FAA Form 8110-2 (8/13) Page 1

**SUPPLEMENTAL TYPE CERTIFICATE, FAA FORM 8110-2 (CONTINUED)**

To (Name of transferee)

(Address of transferee)

(Number and street)

(City, State, and ZIP Code)

From (Name of grantor)

(Address of grantor)

(Number and street)

(City, State, and ZIP Code)

FAA Form 8110-2 (8/13) Page 2

## Every issue (1)

- August 2, 2013: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/b7/fe/b7fefe06a349af414c081bcbcd0344d237dda6ed6d8bcff8e2cc55ec0f1a78f5)

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