# STC SH2889SW - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Bell Helicopter Textron Inc. - Description: Fuel filler neck. - Status date: August 2, 2013 - Data sheets: H2SW, H2SW - Certificate PDF: https://openairdocs.org/files/sha256/d2/c9/d2c9fc57c1c04ddd81fa82c131da048efa23048f3db5683b04409bbb088ad46b - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/74FFDBCB921E4CD886257C7E00546F44.0001 - Page: https://openairdocs.org/stc/SH2889SW ## ADs that name it None. ## Approved models (2) - Bell Helicopter Textron (Canada) 206A (TCDS H2SW) - Bell Helicopter Textron (Canada) 206B (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 SH2889SW This certificate issued to: Bell Helicopter Textron, Inc. 441 Industrial Park Road Piney Flats, TN 37686 Part 21.29of the Federal Aviation Regulations. Original Product – Type Certificate Number: H2SW Make: Bell Helicopter Textron Canada Limited Model: 206A, 206B Description of Type Design Change: (A) Installation fuel filler neck according to Fuel Extender Installation Instructions dated October 9, 1978. (B) Manufacture of Range Extender or Range Extender-Quick Disconnect in accordance with Aeronautical Accessories, Inc. Drawing List Report No. AA-89006 (was Report KR-285), Revision A, dated June 22, 1989, and installed in accordance with Installation Instructions Report No. AA-88063, Revision A, dated August 25, 1988, or later FAA approved revisions. FAA Approved Rotorcraft Flight Manual Supplement (Report No. AA-88021), dated August 1, 1979, or later FAA approved revision, is a required part of this STC. 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. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage. Date of application: October 9, 1978 Date reissued: 6/15/79; 8/16/79; 8/17/81; 8/31/82; 8/2/13 Date of issuance: December 20, 1978 Date amended: 12/2/83; 7/5/96 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/d2/c9/d2c9fc57c1c04ddd81fa82c131da048efa23048f3db5683b04409bbb088ad46b) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.