# STC SR03038NY

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: M.R. Airframe Ltd, Canada
- Description: Installation of Vertical Fin Composite Leading and Trailing Edge Caps,
- Applied: July 15, 2011
- Status date: December 21, 2011
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/30/f4/30f4fa7e69842edcfa0c65e3b564f2cc027266685ac3175e8bf488738074ed7e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/960DAFA56978D4FA86257A4D005D5530.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR03038NY

## ADs that name it (0)

None.

## Approved models (10)

- Bell Helicopter Textron Canada Limited 206 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206A ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206A-1 (OH-58A) ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206B ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206B-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206L ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206L-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206L-3 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206L-4 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 407 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))

## 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.

Part 27 of the Federal Regulations.

Original Product -- Type Certificate Number: H2SW

Installation of Vertical Fin Composite Leading and Trailing Edge Caps, must be done in accordance with M.R. Airframe Installation Instructions INST10-010, Revision - dated February 18, 2011, Transport Canada approved June 30, 2011, or later Transport Canada approved revision.

1. Instructions for Continued Airworthiness contained in M.R. Airframe Instructions for Continued Airworthiness ICA10-010, Revision A, dated December 15, 2011, Transport Canada accepted December 16, 2011 or later Transport Canada accepted revision.

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

3. If the holder agrees to permit another person to use this certificate to alter a product, the holder shall give the other person written evidence of that permission.

M.R. Airframe Ltd.

5104 Hwy 17 Arnprior, Ontario K7S 3G7 Canada Make: Bell Helicopter Textron Model: 206, 206A, 206A-1, 206B, 206B-1, 206L, 206L-1, 206L-3, 206L-4, 407 Date of application: July 15, 2011

Date of issuance: December 21, 2011

( Signature) Michele Maurer, Acting Manager New York Aircraft Certification Office

( Title)

## Every issue (1)

- December 21, 2011: Issued, Current. [certificate](https://openairdocs.org/files/sha256/30/f4/30f4fa7e69842edcfa0c65e3b564f2cc027266685ac3175e8bf488738074ed7e)

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