# STC SR01204SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Aerometals, United States
- Description: Fabrication of AMC AMC369H92827 pin, clevis-rotor brake
- Applied: February 7, 2003
- Status date: March 1, 2005
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H3WE](https://openairdocs.org/tcds/H3WE)
- Certificate PDF: https://openairdocs.org/files/sha256/96/aa/96aad0d56800f246fac398eb21c3eb71ad42100e05fb1dd673e5ff36c769cade
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/09690F2B77B9A85B86256FBF006E10D0.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR01204SE

## ADs that name it (0)

None.

## Approved models (7)

- MD Helicopter Inc. 369D ([TCDS H3WE](https://openairdocs.org/tcds/H3WE))
- MD Helicopter Inc. 369E ([TCDS H3WE](https://openairdocs.org/tcds/H3WE))
- MD Helicopter Inc. 369FF ([TCDS H3WE](https://openairdocs.org/tcds/H3WE))
- MD Helicopter Inc. 369HE ([TCDS H3WE](https://openairdocs.org/tcds/H3WE))
- MD Helicopter Inc. 369HM ([TCDS H3WE](https://openairdocs.org/tcds/H3WE))
- MD Helicopter Inc. 369HS ([TCDS H3WE](https://openairdocs.org/tcds/H3WE))
- MD Helicopter Inc. 500N ([TCDS H3WE](https://openairdocs.org/tcds/H3WE))

## 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.

United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SR01204SE This certificate, issued to Aerometals 3920 Sandstone Drive El Dorado Hills, CA 95762 Part 6 of the Civil Air Regulations.

Original ProductType Certificate Number: H3WE Make: MD Helicopters, Inc.

Model: 369HE/HM/HS, 369D/E/FF, and 500N

Description of the Type Design Change: Fabrication of AMC AMC369H92827 pin, clevis-rotor brake in accordance with AMC Master Drawing List No. MDL-AMC-014, Revision B, dated February 26, 2003, or later Federal Aviation Administration (FAA) approved revision. The rotor brake clevis pin must be installed in accordance with AMC Installation Instructions MI-02003, Revision A, dated February 14, 2003, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design applies to the rotorcraft models listed above only. 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 of those other previously approved modifications, including changes in type design, will introduce no adverse effects upon the airworthiness of that rotorcraft. A copy of this Certificate must be maintained as part of the permanent record of the modified rotorcraft.

This is a direct replacement part, and the FAA has determined that no Instructions for Continued Airworthiness are required.

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: February 7, 2003 Date reissued: March 1, 2005 Date of issuance: April 10, 2003 Date amended:

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

## Every issue (1)

- March 1, 2005: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/96/aa/96aad0d56800f246fac398eb21c3eb71ad42100e05fb1dd673e5ff36c769cade)

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