# STC SR00730SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Simplex Manufacturing Company, United States
- Description: Fabrication and Installation of Simplex Model 304 fire attack system.
- Applied: June 4, 1999
- Status date: September 30, 2013
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 29
- Data sheets: [TCDS H79EU](https://openairdocs.org/tcds/H79EU)
- Certificate PDF: https://openairdocs.org/files/sha256/b0/6b/b06bcbe1421b4511faed0d57a3dee82e6b07cc42bfa5824ec3749478bb25727c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/54006D614469CC8686257BFA00579760.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00730SE

## ADs that name it (0)

None.

## Approved models (2)

- Agusta S.p.A. AB412 ([TCDS H79EU](https://openairdocs.org/tcds/H79EU))
- Agusta S.p.A. AB412 EP ([TCDS H79EU](https://openairdocs.org/tcds/H79EU))

## 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 SR00730SE

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

Part 29 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: H79EU Make: Agusta Model: AB412 and AB412 EP

Description of the Type Design Change: Fabrication of Simplex Model 304 Fire Attack System in accordance with Simplex Master Drawing List MDL 304, Revision T, dated June 11, 2013, or later Federal Aviation Administration (FAA) approved revision; and installation in accordance with Simplex Installation Manual 304-102 002-001, Revision K, dated June 25, 2013, or later FAA-approved revision.

Limitations and Conditions: Approval of this change in type design applies to the rotorcraft listed above only, equipped with an FAA-approved high skid landing gear system. This approval should not be extended to other rotorcraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer 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 rotorcraft.

This modification must be maintained in accordance with Simplex Maintenance Manual 304-102 005-001, Revision F, dated August 8, 2012, or later FAA-approved revision, and operated in accordance with Rotorcraft Flight Manual Supplement (RFMS) 304-102 003-002AB, Revision F, dated July 12, 2013, or later FAA-approved revision.

A copy of this Certificate, the Maintenance Manual, and the RFMS must be maintained as part of the permanent records of the modified rotorcraft. 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, 1999 Date reissued:

Date of issuance: September 3, 1999 Date amended: 2/13/04; 7/24/09; 8/18/09; 9/30/13

(Signature)

Manager, Seattle Aircraft Certification Office (Title)

**FAA FORM 8110-2-1 (10-69) PAGE 1 OF 2 PAGES**

## Every issue (3)

- September 30, 2013: Amended, Current. [certificate](https://openairdocs.org/files/sha256/b0/6b/b06bcbe1421b4511faed0d57a3dee82e6b07cc42bfa5824ec3749478bb25727c)
- August 18, 2009: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/d0/2f/d02f003f99aac6e1338360dd8e4dd3085a5eb818d30e5aec1cd6dbd96d1df202)
- July 24, 2009: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/cd/ee/cdee0cf6c4f0cffc0d52e42f7ed85c5a437cb4c9a6429f34db3f63065c0c5253)

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