# STC SR00444DE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Paravion Technology Inc, United States
- Description: Installation of Engine Relight System.
- Applied: June 1, 2000
- Status date: December 22, 2000
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/5e/62/5e62c1880a87aecc41037a462abb9930c70b20587b9f7f3ba9de547b81dd9cd6
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/371DE335A56D563C85256CC20062256B.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00444DE

## ADs that name it (0)

None.

## Approved models (6)

- Bell Helicopter Textron Canada Limited 206A ([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 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))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SRO0444DE This certificate issued to: Paravion Technology, Inc.

2001 Airway Avenue Fort Collins, CO 80524 Part 27 of the Federal Aviation Regulations.

Original Product -Type Certificate Number: H2SW Make: Bell Helicopter Textron Model: Bell 206A, 206B, 206L, L-1, L-3, L-4 Description of Type Design Change:

Installation of Engine Relight System in accordance with Paravion Technology Master Drawing List DL-206ER-100, revision A, dated November 14, 2000, FAA approved dated December 22, 2000 or later FAA approved revision.

1. Compatibility of this design change with previously approved modifications must be determined by installer.

2. A copy of this Certificate must be maintained as part of the permanent records for the modified rotorcraft.

3. FAA approved Rotorcraft Flight Manual Supplement, PR-206ER-100M, dated December 22, 2000 or later FAA approved revision is required.

4. Instructions for Continued Airworthiness, Report PR-206ER-120M, Rev. 0, dated September 25, 2000, FAA accepted dated November 30, 2000 or later FAA accepted revision is required for this installation.

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

Date of Application: June 1, 2000 Date Reissued:

Date of Issuance: December 22, 2000 Date Amended:

FEDERA By Direction of the Administrator Da i. Consas David T. Grossman, (Signature) Rotorcraft Program Manager *OMINIST RATION Northwest Mountain Region Denver Aircraft Certification Office (Title)

## Every issue (1)

- December 22, 2000: Issued, Current. [certificate](https://openairdocs.org/files/sha256/5e/62/5e62c1880a87aecc41037a462abb9930c70b20587b9f7f3ba9de547b81dd9cd6)

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