# STC SR02258SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Dart Aerospace USA Inc., United States - Description: Installation of a tail rotor pedal lockout kit - Applied: August 30, 2012 - Status date: October 17, 2018 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 27 - Data sheets: [TCDS H7EU](https://openairdocs.org/tcds/H7EU), [TCDS H2SW](https://openairdocs.org/tcds/H2SW) - Certificate PDF: https://openairdocs.org/files/sha256/de/93/de933222863e553835c0d6bc8aa7df018940d28b2f5ef7cb6de92803355c634e - Approved model list and other attachments: [SR02258SE_AML.pdf](https://openairdocs.org/files/sha256/d9/96/d996db1894eef3bde74981c6ee216ef61f093a8d16bf78669dd85a14eb816f7d) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1FC7B52F902090C58625832E004F784B.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SR02258SE ## ADs that name it (0) None. ## Approved models (20) - Agusta S.p.A. A109 ([TCDS H7EU](https://openairdocs.org/tcds/H7EU)) - Agusta S.p.A. A109A ([TCDS H7EU](https://openairdocs.org/tcds/H7EU)) - Agusta S.p.A. A109A II ([TCDS H7EU](https://openairdocs.org/tcds/H7EU)) - Agusta S.p.A. A109C ([TCDS H7EU](https://openairdocs.org/tcds/H7EU)) - Agusta S.p.A. A109E ([TCDS H7EU](https://openairdocs.org/tcds/H7EU)) - Agusta S.p.A. A109K2 ([TCDS H7EU](https://openairdocs.org/tcds/H7EU)) - Agusta S.p.A. A109S ([TCDS H7EU](https://openairdocs.org/tcds/H7EU)) - Agusta S.p.A. A119 ([TCDS H7EU](https://openairdocs.org/tcds/H7EU)) - Agusta S.p.A. AW109SP ([TCDS H7EU](https://openairdocs.org/tcds/H7EU)) - Agusta S.p.A. AW119 MKII ([TCDS H7EU](https://openairdocs.org/tcds/H7EU)) - Bell Helicopter Textron Canada Limited 206 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206A ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206A-1 (OH-58A) ([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 206B-1 ([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. Un ited S tates of Am erica Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number SR02258SE This certificate, issued to Dart Aerospace USA, Inc. 3845 NE 30th Avenue Hillsboro, OR 97124 Part * of the * Regulations. Original ProductType Certificate Number: * See attached Federal Aviation Administration (FAA) Make: Approved Model List (AML) SR02258SE for approved Model: rotorcraft models and applicable airworthiness regulations Description of the Type Design Change: Installation of a tail rotor pedal lockout kit in accordance with the applicable master document list and installation instructions as listed on AML SR02258SE. Limitations and Conditions: Approval of this change in type design applies to the models listed on AML SR02258SE only. This approval should not be extended to other rotorcraft of this model series unless the installer determines that the relationship between this change and any other previously incorporated approved modifications will introduce no adverse effect upon the airworthiness of that rotorcraft. A copy of this certificate and the applicable instructions for continued airworthiness documents as listed on AML SR02258SE, must be maintained as part of the permanent records for the modified rotorcraft. NOTE: The D119-827-011 Pedal Lock Installation consist of a co-pilot pedal lock assembly that is designed to disconnect the co-pilot’s tail rotor pedals from the flight control system when the co-pilot dual control sticks are removed, thus preventing passenger interference with flight controls. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. Date of application: August 30, 2012 Date reissued: October 28, 2015; October 17, 2018 Date of issuance: December 21, 2012 Date amended: March 17, 2014; June 29, 2017 (Signature) Manager, Seattle Aircraft Certification Office (Title) ### SR02258SE_AML.pdf **FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SR02258SE FOR** INSTALLATION OF A TAIL ROTOR PEDAL LOCKOUT KIT ISSUE DATE: March 17, 2014 Page 1 of 1 **ITEM ROTORCRAFT MAKE** **ROTORCRAFT MODEL** **ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **FAA APPROVED** **INSTRUCTIONS FOR** **CONTINUED** **AIRWORTHINESS** **FAA APPROVED** **INSTALLATION** **INSTRUCTIONS** **FAA APPROVED MASTER** DOCUMENT LIST AML REV DATE Number Revision* Number Revision Drawing Revision* 1. Augusta S.p.A. A109, A109A, A109A II, A109C, A109K2, A119, A109E, A109S, AW119 MKII, AW109SP H7EU FAR Part 27 ICA-D119-827 Revision 3, dated 2/6/2017 IIN-D119-827 Revision E, dated 2/3/2017 MDL-D119-827 Revision G, dated 3/31/2017 6/29/2017 2. Bell Helicopter Textron Canada Limited 206, 206A, 206A-1, 206B, 206B-1, 206L, 206L-1, 206L-3, 206L-4, 407 H2SW FAR Part 27 ICA-D407-827 Revision 3, dated 2/6/2017 IIN-D119-827 Revision E, dated 2/3/2017 MDL-D119-827 Revision G, dated 3/31/2017 6/29/2017 * Or later FAA Approved Revision FAA Approved: Manager, Seattle Aircraft Certification Office AMENDED: June 29, 2017 REISSUED: ## Every issue (5) - October 17, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/de/93/de933222863e553835c0d6bc8aa7df018940d28b2f5ef7cb6de92803355c634e), [SR02258SE_AML.pdf](https://openairdocs.org/files/sha256/d9/96/d996db1894eef3bde74981c6ee216ef61f093a8d16bf78669dd85a14eb816f7d) - June 29, 2017: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/c6/db/c6dbad2bdbb12b7beb69125af1c4c2f0fda942d1de277df4cff52a6eb6ac3134), [SR02258SE_AML.pdf](https://openairdocs.org/files/sha256/d9/96/d996db1894eef3bde74981c6ee216ef61f093a8d16bf78669dd85a14eb816f7d) - October 28, 2015: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/a3/4d/a34d9646b5f370913aa2f92d6d0626b91bd2dc8097becb4594b5247b99973785), [AML_SR02258SE.pdf](https://openairdocs.org/files/sha256/21/e5/21e51d29916bc1dc8c17e702c5e9bd4354b076023b4ad333c24b6a8af7106aaf) - March 17, 2014: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/d1/4e/d14e46f4afd4689f3c096ef9372bd6bd4402d31ad5146803e7b566aaf0250845), [AML_SR02258SE.pdf](https://openairdocs.org/files/sha256/21/e5/21e51d29916bc1dc8c17e702c5e9bd4354b076023b4ad333c24b6a8af7106aaf) - December 21, 2012: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/f7/b7/f7b7c7ae4cc1f1fbc3b1289d4dcb176c69930d964bcf5a7f8c9be1dade4fe521) --- 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.