# STC SR00768SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Simplex Manufacturing Company, United States
- Description: Fabrication of Simplex Model 208 agricultural spray tank system.
- Applied: September 2, 1999
- Status date: January 20, 2000
- 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/e9/79/e9791635ad8cb37387a58d68749d58810d8c1c7f9b81e094a75bfde9bf418ca5
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9C7D6269D5FD96FE85256CC200622605.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00768SE

## ADs that name it (0)

None.

## Approved models (1)

- 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.

Number SR00768SE

This certificate, issued to Simplex Manufacturing Company 13340 NE. Whitaker Way Portland, OR 97230

Part 27 of the Federal Aviation Regulations.

Original ProductType Certificate Number: H2SW Make: Bell Helicopter Textron Model: 407

Description of the Type Design Change: Fabrication of Simplex Model 208 agricultural spray tank system in accordance with Simplex Master Drawing List No. MDL-208, Revision “A,“ dated December 14, 1999, or later Federal Aviation Administration (FAA) approved revision; and installation of this system in accordance with Simplex Installation Document No. 208-102 002-001, dated November 17, 1999, or later FAA approved revision.

This modification must be maintained in accordance with Simplex Maintenance Manual Document No. 208-102 005-001, dated December 2, 1999, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design applies to Bell Model 407 rotorcraft only, equipped with an FAA approved high skid landing gear system. This approval should not be extended to other rotorcraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that helicopter.

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.

(See Continuation Sheet - Page 3) This certificate and the supporting data which is the ba sis for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: September 2, 1999 Date reissued:

Date of issuance: January 20, 2000 Date amended:

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- January 20, 2000: Issued, Current. [certificate](https://openairdocs.org/files/sha256/e9/79/e9791635ad8cb37387a58d68749d58810d8c1c7f9b81e094a75bfde9bf418ca5)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.