# STC SR00486DE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Dart Aerospace USA Inc., United States
- Description: Installation of mounting hardware in accordance with Paravion Technology Master Drawing List DL-407LS-100, Revision N/C, dated April 01, 2002, FAA approved dated January 27, 2003 or later FAA approved revision, and approval for the aircraft to be operated by a single pilot from the left crew seat.
- Applied: March 11, 2002
- Status date: August 22, 2023
- Product: Aircraft, Rotorcraft
- Certification basis: Part 27
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/50/0e/500e09ab74bf8b9429e3afe90a92971990471e20c3876b9e9e241d378edf49f7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105124954620231012140423.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR00486DE

## ADs that name it (0)

None.

## Approved models (1)

- 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.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Page 1 of 2 SR00486DE Dart Aerospace USA, Inc 3845 NE 30th Avenue Hillsboro, OR 97124 Part 27 the Federal Aviation Regulations H2SW Bell Helicopter Textron 407 Installation of mounting hardware in accordance with Paravion Technology Master Drawing List DL-407LS-100, Revision N/C, dated April 1, 2002, FAA approved dated January 27, 2003, or later FAA approved revision, and approval for the aircraft to be operated by a single pilot from the left crew seat.

March 11, 2002 August 22, 2023 January 27, 2003 for Manager, West Certification Branch

1. This approval should not be extended rotorcraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that rotorcraft.

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

3. FAA approved Rotorcraft Flight Manual Supplement, PR-407LS-100M, dated January 27, 2003, or later FAA approved revision is required.

4. Instruction for Continued Airworthiness, Report PR-407LS-120M, Revision 0, dated December 5, 2002, FAA accepted dated January 7, 2003, or later FAA accepted revision is required for this installation.

5. For left seat operation of equipment originally intended to be operated by the pilot from rhe right crew seat, provisions must be made to insure that such equipment can be equally operable from the left crew seat with similiar controls.

6. 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.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Page 2 of 2 SR00486DE

## Every issue (2)

- August 22, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/50/0e/500e09ab74bf8b9429e3afe90a92971990471e20c3876b9e9e241d378edf49f7)
- January 27, 2003: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/bc/65/bc650a21a61c3e76b9549b64d56ce86c7aeef524bb69129e7b9ba711d43e1d9e)

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