# STC SR03283NY - Type: Supplemental type certificate - Status: Current, Amended - Holder: Dart Aerospace Limited, Canada - Description: Installation of Cyclic Stick Control Friction as a direct replacement for Bell Cyclic Knob and Shaft Assembly - Applied: December 12, 2012 - Status date: August 24, 2020 - Product: Aircraft, Rotorcraft - Certification basis: Part 21 - Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) - Certificate PDF: https://openairdocs.org/files/sha256/a4/3d/a43d73170b0d84b87f43900bb3aec926389d6739d3f74d85f717b29cd92b2a71 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/31CEEA72FBEA3589862585F900469B84.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR03283NY ## ADs that name it (0) None. ## Approved models (7) - 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)) - Bell Helicopter Textron Canada Limited 206L ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206L-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206L-3 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206L-4 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 407 ([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. FAA Form 8110-2 (5/14) Page 1 of This certificate issued to: Part of the Original Product – Type Certificate Number: Make: By Direction of the Administrator Signature Title Timothy J. Hadsall Acting Manager New York ACO Branch IMPORT SR03283NY Dart Aerospace Ltd. 1270 Aberdeen Street Hawkesbury, Ontario Canada K6A 1K7 6/27 Civil Air and Federal Aviation Regulations. H2SW 206A, 206B, 206L, 206L-1, 206L-3, 206L-4, 407 Configuration 1: 1. Installation of Cyclic Stick Control Friction as a direct replacement for Bell Cyclic Knob and Shaft Assembly must be in accordance with Installation Data listed in AERO Design Ltd. Document Control List DCL 952-1, Revision 1, dated August 7, 2014, Transport Canada Civil Aviation (TCCA) approved February 15, 2015, or later TCCA approved revision. 2. Aero Design Ltd. Rotorcraft Flight Manual Supplement FMS 952.91, Revision 1, dated August 6, 2014, TCCA approved February 15, 2015, or later TCCA approved revision, is required with this installation. (See Description of Type Design Change Continued on Page 3 of 3) 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. 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. April 13, 2015, October 18, 2019 Bell December 12, 2012 June 5, 2013 September 15, 2015, August 24, 2020 3 FAA Form 8110-2 (5/14) Page 2 of To (Name and address of transferee) From (Name and address of grantor) 3 SR03283NY FAA Form 8110-2 (5/14) Page 3 of Amended Date : August 24, 2020 Description of Type Design Change (continued): 3. Aero Design Ltd. Instructions for Continued Airworthiness ICA 952.90, Revision 1, dated January 9, 2015, Transport Canada accepted February 13, 2015, or later Transport Canada accepted revision, is required with this installation. Configuration 2: 1. Installation of the Cyclic Stick Control Friction must be in accordance with Transport Canada Civil Aviation (TCCA) approved Dart Aerospace Ltd., Installation Instructions IIN-D407-1086, Revision A, dated March 31, 2020, or later TCCA approved revision. 2. Operation of the Cyclic Stick Control Friction must be in accordance with TCCA approved Dart Aerospace Ltd., Flight Manual Supplement FMS-D407-1086, Revision A, dated April 03, 2020, or later TCCA approved revision. 3. Maintenance of the Cyclic Stick Control Friction must be in accordance with TCCA accepted Dart Aerospace Ltd., Instructions for Continued Airworthiness ICA-D407-1086, Revision 0, dated March 31,2020, or later TCCA accepted revision. 4. Definition of the Type Design Change for Configuration 2 is in TCCA approved Dart Aerospace Ltd., Master Document List MDL-D407-1086, Revision A, dated May 17, 2020, or later TCCA approved revision. ----------END---------- 3 SR03283NY ## Every issue (4) - August 24, 2020: Amended, Current. [certificate](https://openairdocs.org/files/sha256/a4/3d/a43d73170b0d84b87f43900bb3aec926389d6739d3f74d85f717b29cd92b2a71) - October 18, 2019: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/c3/4b/c34b2419f9867cd2613cfed8ad906bb7e9c06bc3f90900acfa70b132184a74b8) - September 15, 2015: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/cd/77/cd77ed877843572f209617dc7dcd60606438bb124e953c90bc2f0152565c1073) - June 5, 2013: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/a4/61/a461bd45c97ca9e394fbf228c846368d179b54a5b285c5dcdca6be5c5e6edb27) --- 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.