# STC SR01934NY

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Eagle Copters Ltd, Canada
- Description: Reclassification to Category B, Utility Operations, reduction of passenger seating configuration.
- Applied: March 5, 2004
- Status date: April 8, 2008
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H1SW](https://openairdocs.org/tcds/H1SW)
- Certificate PDF: https://openairdocs.org/files/sha256/f6/cf/f6cf6b9612b50782f3705e84033c49162c62683ff1298fb6970596979e4ef69d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4CDDCAA0C8FCE2B18625743B007DE771.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR01934NY

## ADs that name it (0)

None.

## Approved models (1)

- Bell Helicopter Textron 205A-1 ([TCDS H1SW](https://openairdocs.org/tcds/H1SW))

## 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.

823, McTavish Road, NE Calgary, Alberta T2E 7G9 Canada

Part 7 of the Civil Air Regulations.

Original Product -- Type Certificate Number: H1SW Make: Bell

Model: 205A-1 Description of Type Design Change:

Reclassification to Category B, reduction of passenger seating configuration (9 passengers) to be completed in accordance with Eagle Copters Ltd, Installation Instructions IIN-D205-754, Revision A, dated October 18, 2007, Transport Canada approved October 18, 2007, or later Transport Canada approved revision.

1. Eagle Copters Ltd. Flight Manual Supplement FMS-D205-754-1, Revision A, dated October 9, 2007, Transport Canada approved October 9, 2007, or later Transport Canada approved revision, is required when the helicopter is modified by both the installation of Honeywell T5317A, T5317B, or T5317BCV Engine and the installation of Bell 212 Main Rotor Blades in accordance with approved Supplemental Type Certificates.

2. Installation of the Honeywell T5317A, T5317B, or T5317BCV in accordance with FAA STC SR01496NY is required for this STC.

3. Installation of Bell 212 main rotor in accordance with FAA STC SH5132NM is required for this STC.

4. 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.

5. The Installer must determine whether this design change is compatible with previously approved modifications.

Date of Application: March 5, 2004Date of issuance: July 27, 2004 Date reissued:

Date amended: April 28, 2005, April 08, 2008

( Signature) Anthony Socias Acting Manager New York Aircraft Certification Office

( Title)

## Every issue (2)

- April 8, 2008: Amended, Current. [certificate](https://openairdocs.org/files/sha256/f6/cf/f6cf6b9612b50782f3705e84033c49162c62683ff1298fb6970596979e4ef69d)
- April 28, 2005: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/24/6f/246f5356a979f81d046a11940c07f51cd7ed279f4d9129bf0e33e41d78332f22)

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