# STC SR00603DE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: PECO Inc, United States
- Description: Installation of Paravion Technology PR-206/407EV-100 Enhanced Vision System.
- Applied: April 12, 2006
- Status date: June 29, 2020
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/51/48/5148c9a45f064a88c39af7e35c35e83429ef0c35be6f71c2c2e3cddf7ad18725
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/40A860D1F42755B2862585DE005FA500.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00603DE

## ADs that name it (0)

None.

## Approved models (7)

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

Number SR00603DE

This certificate, issued to PECO, Inc.

11241 SE Highway 212 Clackamas, OR 97015

Part 6* of the Civil Aviation Regulations. * Certification Basis is set forth in Type Certificate Data Sheet H2SW Original ProductType Certificate Number: H2SW Make: Bell Model: 206A, 206B, 206L, 206L1, 206L3, 206L4, 407

Description of the Type Design Change: Installation of Paravion Technology PR-206/407EV-100 Enhanced Vision System in accordance with Master Drawing List DL-206/407EV-100, Revision N/C dated April 10, 2006 and FAA approved July 28, 2006, or later FAA approved revision.

1. A copy of this Certificate and FAA Approved Rotorcraft Flight Manual Supplement Number PR - 206/407EV-100M, revision N/C, dated July 28, 2006, or later FAA approved revision must be maintained as part of the permanent records for the modified aircraft.

2. For Instructions for Continued Airworthiness refer to Instructions for Continued Airworthiness, Document No. PR-206/407EV-120M, revision Original, dated 4/10/06 or later FAA accepted revision.

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

4. 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: April 12, 2006 Date reissued September 27, 2017; June 29, 2020

Date of issuance: July 28, 2006 Date amended

FAA FORM 8110-2 (5/14) PAGE 1 OF 2 PAGES By direction of the Administrator

(Signature)

For Manager, Seattle ACO Branch (Title)

Transfer the ownership of Supplemental Type Certificate Number

to (Name of Transferee)

(Address of Transferee)

(Number and Street)

(City, State, and ZIP Code)

from (Name of Grantor) (Print or Type)

(Address of Grantor)

(Number and Street)

(City, State, and ZIP Code)

Signature of Grantor (In Ink):

U.S. GPO: 1987-763-289

## Every issue (3)

- June 29, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/51/48/5148c9a45f064a88c39af7e35c35e83429ef0c35be6f71c2c2e3cddf7ad18725)
- September 27, 2017: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/96/0f/960f9f3a846db276a1f7d0af3732a1075fa37e1ed1e21776cfde646ea61848f4)
- July 28, 2006: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/99/56/9956214077c8d15a65b9109dcf8e3e39d58f920c36304275f1c56a40ddf32228)

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