# STC SR00218IB

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Croman Corporation, United States
- Description: Installation of the Cockpit Door
- Applied: April 19, 2024
- Status date: October 7, 2024
- Product: Aircraft, Rotorcraft
- Certification basis: Part 29
- Foreign approvals: TCCA SH97-51 @ Issue 4
- Data sheets: [TCDS 1H15](https://openairdocs.org/tcds/1H15)
- Certificate PDF: https://openairdocs.org/files/sha256/d6/ee/d6eeee35f3b3ff87909220a41830ebe8977aa9b02d47d7aaa586c1f68cb0f915
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106486465720241101151136.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00218IB

## ADs that name it (0)

None.

## Approved models (2)

- Sikorsky Aircraft Corporation S-61L ([TCDS 1H15](https://openairdocs.org/tcds/1H15))
- Sikorsky Aircraft Corporation S-61N ([TCDS 1H15](https://openairdocs.org/tcds/1H15))

## 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 8110-2 (10/24) Page 1 of ___ SR00218IB Croman Corporation 801 Ave C White City, OR 97503 Part 29 Title 14, Code of Federal Regulations

1. 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.

2. The installer must determine whether this design change is compatible with previously approved modifications.

(See continuation sheet 3) 4/19/24 10/7/24 9/10/24 Gregory S. DiLibero Manager, West Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3

1. Installation of the Cockpit Door must be in accordance with S & H Helipro drawing number SHS61-52-001, Revision NC, dated July 24, 1997, or later FAA approved revision.

Sikorsky Aircraft S-61L, S-61N 1H15

SR00218IB 10/07/24 SR00218IB 3

SR00218IB 10/07/24 Limitations and Conditions (continued):

3. This STC is applicable to all serial numbers for these Make-Models.

4. Placards: Emergency door release instructions are to be placarded on both sides of the cockpit door per drawing SHS61-52-001, Revision NC, dated July 24, 1997.

----------END----------

## Every issue (2)

- October 7, 2024: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d6/ee/d6eeee35f3b3ff87909220a41830ebe8977aa9b02d47d7aaa586c1f68cb0f915)
- September 10, 2024: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/7c/9e/7c9ef242aa2ce7467854433df0035a483555f2caca1234169600c66a65d3e02c)

---
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.