# STC SR02728NY - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Dart Aerospace Limited, Canada - Description: Installation of Quick Release Mounting Provisions on the right or left side - Applied: April 1, 2009 - Status date: October 18, 2019 - Product: Aircraft, Rotorcraft - Certification basis: Part 21 - Data sheets: [TCDS H3WE](https://openairdocs.org/tcds/H3WE) - Certificate PDF: https://openairdocs.org/files/sha256/a3/28/a3282d1e08834662ac6577ab3d5bcbe7938c8e94f38f837f27091e13ee7d1c07 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8B8AB1A41727752A862585BC00561AFA.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR02728NY ## ADs that name it (0) None. ## Approved models (1) - MD Helicopter Inc. 600N ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) ## 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 Part of the Signature Title SR02728NY Dart Aerospace Ltd. 1270 Aberdeen Street Hawkesbury, Ontario Canada K6A 1K7 Federal Aviation Regulations. 27 Configuration A – Quick Release Mounting Provisions: Installation of Quick Release Mounting Provisions on the right or left side in accordance with AERO Design Ltd. Installation Document 82802, Revision 0, as listed in Document Control List DCL828-1, Revision 0, dated December 3, 2008, Transport Canada (TCCA) approved January 27, 2009, or later TCCA approved revisions. (See Description of Type Design Change continued on Page 3 of 3) 1. Installation of Configuration A is a prerequisite for the installation of Configuration B. 2. Installation of Configuration A is a prerequisite for the installation of Configuration C. 3. Configuration A may remain installed on aircraft when Configuration B or C is removed. 4. Eligibility limitations of cargo basket modifications are noted on the drawings listed in AERO Design Ltd. Document Control List DCL704, Revision 4, dated December 22, 2008. (See Limitations and Conditions continued on Page 3 of 3) Anthony E. Gallo Acting Manager New York ACO Branch MDHI 600N October 18, 2019 April 1, 2009 August 26, 2009 IMPORT H3WE 3 FAA Form 8110-2 (5/14) Page 2 of To (Name and address of transferee) From (Name and address of grantor) 3 SR02728NY FAA Form 8110-2 (5/14) Page 3 of 3 Reissue Date: October 18, 2019 Description of Type Design Change (continued): Configuration B – Quick Release Cargo Basket Installation: Installation of Quick Release Cargo Basket on the right or left side in accordance with AERO Design Ltd. Installation Document 82801, Revision 0, as listed in Document Control List DCL828-1, Revision 0, dated December 3, 2008, TCCA approved January 27, 2009, or later TCCA approved revisions. Configuration C – Quick Release Step Installation: Installation of Quick Release Step on the right or left side in accordance with AERO Design Ltd. Installation Document 82901, Revision 0, as listed in Document Control List DCL829-1, Revision 0, dated December 3, 2008, TCCA approved January 27, 2009, or later TCCA approved revisions. Cargo Basket Modifications: Modifications to the cargo basket configuration are eligible in accordance with AERO Design Ltd. Document Control List DCL704, Revision 4, dated December 22, 2008, TCCA approved January 27, 2009, or later TCCA approved revisions. 5. AERO Design Ltd. Rotorcraft Flight Manual Supplement FMS828.91, Revision 0, dated November 27, 2008, TCCA approved January 27, 2009, or later TCCA approved revisions is required to all installation configurations. 6. AERO Design Ltd. Instructions for Continued Airworthiness ICA 828.90, Revision 0, dated November 27, 2008, TCCA accepted January 27, 2009, or later TCCA accepted revisions is required with the installation of the quick release cargo basket. 7. AERO Design Ltd. Instructions for Continued Airworthiness ICA 829.90, Revision 0, dated November 27, 2008, TCCA accepted January 27, 2009, or later TCCA accepted revisions is required with the installation of the quick release step. 8. The installer must determine whether this design change is compatible with previously approved modifications. 9. 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---------- SR02728NY ## Every issue (2) - October 18, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a3/28/a3282d1e08834662ac6577ab3d5bcbe7938c8e94f38f837f27091e13ee7d1c07) - August 26, 2009: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/aa/ef/aaef2ca86815e277113093f50b4a5c0772c8f88d90fc277222b98192b2b62dc3) --- 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.