# STC SR00886DE - Type: Supplemental type certificate - Status: Current, Issued - Holder: RSG Products, United States - Description: Installation of Goodrich Hoist - Applied: July 11, 2017 - Status date: June 17, 2020 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 29 - Data sheets: [TCDS H4SW](https://openairdocs.org/tcds/H4SW) - Certificate PDF: https://openairdocs.org/files/sha256/f5/5a/f55a0467c3446931abae215d0369646f95a2b09e6b640eef8a0fee2af2704cb8 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6DAC4C1896CE388E862586AB0055A98D.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR00886DE ## ADs that name it (0) None. ## Approved models (1) - Bell Textron Inc. 412EP ([TCDS H4SW](https://openairdocs.org/tcds/H4SW)) ## 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 (4/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ Part of the . SR00886DE RSG AeroDesign, LLC 3900 Falcon Way West, Hanger 16S Fort Worth, TX 76106 29 H4SW Bell 412EP Installation of Goodrich Hoist in accordance with Document No. 00BL207400001, Master Document List, Hoist Installation, Revision A dated 5/18/2020, FAA approved 6/16/2020 or later FAA approved revision. See continuation 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. 07/11/2017 06/17/2020 3 Federal Aviation Regulations Kreg R. Voorhies, ODA Lead administrator Cert Works, LLC. ODA ODA No ODA(AIR)-833887-NM FAA Form 8110-2 (4/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ SR00886DE SR00886DE 3 FAA Form 8110-2 (4/20) Page ___ of ___ SR00886DE Description of Type Design Change Continued: FAA Approved Flight Manual Supplement, Document No. 10BL207300004, Revision B dated 5/15/2020, FAA approved 6/16/2020 or later FAA approved revision, is required for this installation. Instructions for Continued Airworthiness (ICA), Document No. 10BL207200003, Revision A dated 5/21/2020, FAA accepted 6/16/2020, or later FAA accepted revision is required to be made available at installation. Certification Basis: Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Bell 412EP installation of the Hoist Installation is as follows: a. The type certification basis for Bell 412EP series rotorcraft is shown on TCDS H4SW for parts not changed or not affected by the change. b. The certification basis for parts changed or affected by the change since the reference date of application, 7/11/2017, is based upon 14 CFR Part 29, effective February 1, 1965 plus Amendments 29-1 through 29-2, and additional requirements at later amendment level per the TCDS H4SW. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be: Regulations at the latest amendment; None Regulations at an intermediate amendment; None Regulations at the amendment level in TCDS H4SW; 14 CFR Sections: 29.21 Amdt. - ; 29.29 Amdt. - ; 29.143 Amdt. - ; 29.175 Amdt. - ; 29.251 Amdt. - ; 29.301 Amdt. - ; 29.303 Amdt. - ; 29.305(a) Amdt. - ; 29.307(a) Amdt. - ; 29.337(a) Amdt. - ; 29.341 Amdt. - ; 29.351 Amdt. - ; 29.561 (a-c) Amdt. - ; 29.601(a) Amdt. - ; 29.603 Amdt. - ; 29.605 Amdt. - ; 29.607 Amdt. - ; 29.609(a) Amdt. - ; 29.610 Amdt. 29-40; 29.611 Amdt. - ; 29.613(a-d) Amdt. - ; 29.619(b)(1) Amdt. - ; 29.625(a-c) Amdt. - ; 29.771(a-c) Amdt. 29-24; 29.773(a,b) Amdt. 29-57; 29.777 Amdt. - ; 29.853(a) Amdt. - ; 29.865(a,d) Amdt. 29-43; 29.865(b)(1,2),(3)(i) Amdt. 29-43; 29.865(b)(3)(ii)(A) Amdt. 29-43; 29.865(e) Amdt. 29-43; 29.865(f) Amdt. 29-43; 29.939 Amdt. 29-2; 29.1301 (a-c) Amdt. - ; 29.1301(d) Amdt. - ; 29.1309(a,h) Amdt. 29-24; 29.1309(b-d,h) Amdt. 29-24; 29.1322 Amdt. 29-12; 29.1351(a) Amdt. 29-14; 29.1353(a) Amdt. 29-15; 29.1353(a,b) Amdt. 29-15; 29.1357(a-d) Amdt. 29-24; 29.1359(a,b) Amdt. - ; 29.1387 Amdt. 29-9; 29.1435(a)(1,2,5,6)(b,c) Amdt. - ; 29.1501 Amdt. 29-15; 29.1523(a,b) Amdt. - ; 29.1529 Amdt. 29-20; 29.1541 Amdt. - ; 29.1555(a,d) Amdt. 29-24; 29.1581(a,b,d) Amdt. 29-15; 29.1583(a,c,e) Amdt. 29-24; 29.1585(a) Amdt. 29-24 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ## Every issue (1) - June 17, 2020: Issued, Current. [certificate](https://openairdocs.org/files/sha256/f5/5a/f55a0467c3446931abae215d0369646f95a2b09e6b640eef8a0fee2af2704cb8) --- 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.