# STC SH2804SO-D - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Bell Helicopter Textron Inc., United States - Description: High Skid Landing Gear. - Applied: March 2, 1990 - Status date: August 2, 2013 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 27 - Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) - Certificate PDF: https://openairdocs.org/files/sha256/23/45/2345b00c3a0c689210281087244304c998070b0e54dcdbc2af76e713ebe846ac - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/62C8831A75C9816286257C7E004F597D.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SH2804SO-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 SH2804SO-D This certificate issued to: Bell Helicopter Textron, Inc. 441 Industrial Park Road Piney Flats, TN 37686 Part 6of the Civil Air and Part 27 & 21.29 of the Federal Aviation 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: High Skid Landing Gear in accordance with Aeronautical Accessories, Inc. Drawing List Report AA-90009, Revision P, dated June 22, 2006, and installation per Report AA-90055, Revision H, dated July 28, 2004, or Report AA-93083, Revision S, dated December 8, 2003 or later DAS approved revisions. Date of application: March 2, 1990 Date reissued: August 2, 2013 Date of issuance: August 1, 1990 Date amended: 3/11/98; 12/30/99; 6/6/03; 8/1/06 Signature Scott A. Horn Title Acting Manager, Rotorcraft Certification Office, Southwest Region FAA Form 8110-2 (8/13) Page 1 Number: SH2804SO-D Date of Issuance: August 1, 1990 Date Amended: August 1, 2006 Reissuance Date: August 2, 2013 STC SR01535LA is required in conjunction with the installation of 206-324-357/-358/-359/-360 Skid Tube Assemblies. The Rotorcraft Flight Manual Supplement, Report No. AA-90010, Revision B, dated April 23, 1998, or AA-90011, Revision B, dated April 23, 1998, or AA-90012, Revision B, dated April 23, 1998 or later DAS approved revisions and the Instructions for Continued Airworthiness, Aeronautical Accessories, Inc. Report AA-01145, Revision B, dated May 25, 2006, and AA-01149, Revision A, dated May 12, 2004, or later 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. -END- FAA Form 8110-2 (8/13) Page 3 **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/sha256/23/45/2345b00c3a0c689210281087244304c998070b0e54dcdbc2af76e713ebe846ac) --- 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.