# STC SR02402NY - Type: Supplemental type certificate - Status: Current, Amended - Holder: Sikorsky Aircraft Corporation, United States - Description: Installation of Alternate Utility Interior - Applied: June 30, 2006 - Status date: August 2, 2016 - Product: Aircraft, Rotorcraft - Certification basis: Part 29 - Data sheets: [TCDS R00024BO](https://openairdocs.org/tcds/R00024BO) - Certificate PDF: https://openairdocs.org/files/sha256/11/08/11085f6435dc82a4a3953d9b83be343efe0af7432ef5f294fecce2f6ac182378 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183082815520230331201127.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR02402NY ## ADs that name it (0) None. ## Approved models (1) - Sikorsky Aircraft Corporation S-92A ([TCDS R00024BO](https://openairdocs.org/tcds/R00024BO)) ## What the certificate says Some pages are OCR from the scanned FAA certificate. OCR can misread letters and numbers. AVIATIO United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR02402NY This certificate issued to: 6900 Main Street Sikorsky Aircraft Corporation Stratford, CT 06615 Part _29 of the Federal Aviation Regulations. Original Product - Type Certificate Number: Make: Sikorsky R00024BO Model: S-92A Description of Type Design Change: 1. Installation of Alternate Utitity Interior in accordance with Top Kit Drawing 33792-51228 Revision CA or later FAA approved revision. 2. Sikorsky Instructions for Continued Airworthiness, Alternate Utility Interior Installation in Sikorsky Model S-92A Aircraft. Report No. ICO1228 Rev. N dated 03/01/2016 or later FAA accepted res ision is required for this modification Description of Type Design Change: continued on Page 3 of 3) Limitations and Conditions: 1. Compliance with the following regulations has not been demonstrated - 14 CER $29. 1411(0] Amdt. 29-0| and 29, 1415(b) [Amdt. 29-33: Life Vests Only]. 2. Equivalent Level of Safety Finding has been made for the following regulation: 14 CER $29.807(d)(2) at amendnem 29-30 documented in ELOS Memo # N02096-C-L. ELOS Memo # N02096-C-1 is notapplicable when 1C Top Kit 92276-20049-011 (Lef Side Hatch - Al Sliding) is installed Limitations and Conditions: continued on Page 3 of 3) Date of Application: June 30, 2006 Date Reissued: October 1. 2011: December 17.2014: June 19.2015 Date of Issuance: March 28. 2007 Date Amended: Oct. 1. 2007: Apr. 30. 2008: Nov. 23. 2009: Dee. 17. 2010: Jun. 13.2011: Dee. 14.2011: Jan. 17.2013: Dec. 23. 2013: Sept. 2. 2011: Oct. 12. 2015: Aug. 2. 2016 By Direction of the Administrator Signaure I Daniel J. Shapiro ODA Administrator ODA-800001-NE This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21 47. or propeller must provide that person with written permission acceptable to the FAA. (Ref. 14 CFR 21.120) FAA Form 8110-2 (5/14) Page 1 of 3 FAA Form 8110-2 (5/14) Page 2 of Transfer Endorsement Transfer the ownership of Supplemental Type Certificat e Number: To ( Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement): 3 SR02402NY FAA Form 8110-2 (5/14) Page 3 of 3 Date August 02, 2016 Description of Type Design Change: (continued): 3. FAA Approved Rotorcraft Flight Manual Supplement, Supplement No. FM01228 Rev. 10 dated 12/23/2013 or later FAA approved revision is required for this modification. 4. FAA Approved Rotorcraft Flight Manual Supplement, Supplement No. FM01299 Rev. 1 dated 03/29/2008 (or later FAA approved revision) or Sikorsky Supplement No. 15 Rev – dated 6/03/2011 (or later FAA approved revision) is required when the Master Switch Panel (drawing 06092A40B002) is installed. Limitations and Conditions: (continued): 3. Equivalent Level of Safety Finding for 14 CFR §29.807(d)(2) at amendment 29-30 documented in ELOS Memo # N02096-C-1 requires Sikorsky Type Design approved or FAA approved life rafts stored external to the rotorcraft when over-water operation is conducted . 4. Equivalent Level of Safety Finding for 14 CFR §29.807(d)(2) at amendment 29-30 documented in ELOS Memo # N02096-C-1 is not required when drawing 10092B10V001 Rev A, dated 12/10/2010 (or later FAA approved revision) has been installed. 5. Equivalent Level of Safety Finding has been made for the following regulation: 14 CFR §29.803(a)(e) and 29.809(a) at amendment 29-30 and §29.813(c)(2) at amendment 29-12 documented in ELOS Memo # N02326-C1 for installation of Side Facing Utility Seats in front of emergency exits. 6. Previous issuances of this STC approved IDL01228. Top Kit Drawing 33792-51228 replaced IDL01228. 7. The installer must determine whether this design change is compatible with previously approved modifications. 8. 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---------- SR02402NY ## Every issue (4) - August 2, 2016: Amended, Current. [certificate](https://openairdocs.org/files/sha256/11/08/11085f6435dc82a4a3953d9b83be343efe0af7432ef5f294fecce2f6ac182378) - October 12, 2015: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/8c/95/8c9517a8f738f4be7ac415092ac9d1f58fbfb70b8e0df8c168456d03be2efbca) - June 19, 2015: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/38/2b/382be5eed185617efe24e77f81e5992322e573e44517eaa85ae86d50623e5252) - December 23, 2013: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/92/c1/92c1ce1150b119c8908024be320942bf2926aaccc3bc6cb3fab32b2f9ec9be1b) --- 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.