# STC SR01696SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Aerometals, United States
- Description: Fabrication of Main Rotor Hub Fairing and Support Assembly AMC Part Numbers AM369D21004 and AM369D21005
- Applied: July 18, 2005
- Status date: December 11, 2008
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H3WE](https://openairdocs.org/tcds/H3WE)
- Certificate PDF: https://openairdocs.org/files/sha256/8b/95/8b95f25cfd548ea0b1e17be2b1d78cbfb0ee1f965f14dfe9d805803588226705
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/99999EA93D41B25286257560007C5E28.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR01696SE

## ADs that name it (0)

None.

## Approved models (4)

- 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. 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 SR01696SE 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: 369D, 369E, 369FF, 500N

Description of the Type Design Change: Fabrication of Main Rotor Hub Fairing and Support Assembly AMC Part Numbers AM369D21004 and AM369D21005 in accordance with AMC Master Drawing List No. MDL-AMC-027, Revision IR, dated March 28, 2006, or later Federal Aviation Administration (FAA)- approved revision. The Main Rotor Hub Fairing and Support Assembly must be installed in accordance with AMC Installation Instructions AMC MI-05005, Revision IR, dated August 3, 2005, 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.

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: July 18, 2005 Date reissued: December 11, 2008 Date of issuance: August 31, 2006 Date amended:

FAA FORM 8110-2(10-68) By direction of the Administrator Original Signed by Phil Forde

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

## Every issue (2)

- December 11, 2008: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/8b/95/8b95f25cfd548ea0b1e17be2b1d78cbfb0ee1f965f14dfe9d805803588226705)
- August 31, 2006: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/a2/ef/a2ef7843dd60450a647791714d7902b52b41e7941b3f09da1b1a9464aa0057ff)

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