# STC SH1392SO - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Bell Helicopter Textron Inc., United States - Description: High Skid Landing Gear - Applied: April 20, 1982 - Status date: May 29, 2013 - Product: Aircraft, Rotorcraft - Certification basis: Part 21 - Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) - Certificate PDF: https://openairdocs.org/files/sha256/c8/e7/c8e786b6a8acfd19944efbddaf9e446a7d0b548540b60f1d249c117f018c8021 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C4533D93792A6AE686257C13005E4583.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SH1392SO ## ADs that name it (1) - [AD 2005-16-04](https://openairdocs.org/ad/2005-16-04): High forward crosstube · Bell Helicopter Textron Canada 206A and 206B with STC SH1392SO. Effective Sep 12, 2005. Named in the applicability ## Approved models (2) - Bell Helicopter Textron Canada Limited 206A ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206B ([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. N umber SH1392SO This certificate issued to Part 6 of the Civil Air and Part 21.29 of the Federal Aviation R egulations . Original Product -- Type Certificate N umber : High Skid Landing Gear in accordance with Aeronautical Accessories, Inc. Drawing List Report KR-177, No Revision, dated May 19, 1982, and installation per Report AA-90054, Revision E, dated March 24, 2003, Report AA-91051, Revision E, dated August 20, 2002, Report AA-94063, No Revision, dated September 7, 1994, Report AA-94091, No Revision dated December 23, 1994, Report AA-95002, Revision D, dated March 24, 2003, or Report AA-03024, No Revision, dated March 19, 2003 or later FAA/DAS approved revisions. Bell Helicopter Textron, Inc. 441 Industrial Park Road Piney Flats, TN 37686 H2SW M ake : Bell Helicopter Textron Canada Limited M odel : 206A, B Date of application : April 20, 1982 Date of issuance : December 13, 1982 Date reissued : May 29, 2013 Date amended : 4/8/85; 7/23/85; 10/20/87; 3/11/98; 6/6/03 B y di rection of the A dministrator (Signature) Scott A. Horn, Acting Manager, Rotorcraft Certification Office, Southwest Region (Title) FAA Form 8110-2-1(10-69) Page 2 of 3 FAA Form 8110-2-1(10-69) Page 3 of 3 Number SH1392SO Date of Issuance: December 13, 1982 Date of Reissuance: May 29, 2013 The Rotorcraft Flight Manual Supplement, Report No. AA-85011, dated April 8, 1985, Report No. AA-85012, dated April 8, 1985, or Report NO. AA-85025, dated October 20, 1987 or later FAA/DAS approved revisions and the Instructions for Continued Airworthiness, Aeronautical Accessories, Inc. Report AA-01143, Revision A, dated March 25, 2003, and AA-01147, Revision B, dated September 17, 2002, or later AEG accepted revisions are required. Model 206A, S/N’s 3 through 153, must comply with Service Instructions 206-36. 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- ## Every issue (1) - May 29, 2013: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/c8/e7/c8e786b6a8acfd19944efbddaf9e446a7d0b548540b60f1d249c117f018c8021) --- 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.