# STC SR01942SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Aerometals, United States
- Description: Fabrication of AMC Tail Rotor Pitch Control Assemblies.
- Applied: July 12, 2007
- Status date: December 11, 2008
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H3WE](https://openairdocs.org/tcds/H3WE)
- Certificate PDF: https://openairdocs.org/files/sha256/13/dd/13dd4a84ac5dbce812c9bc3f10774177513a4078b134a27656120975bc315898
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/18C548C48A4253B286257560007C5FA2.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR01942SE

## ADs that name it (0)

None.

## Approved models (4)

- MD Helicopter Inc. 369A ([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))

## 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 SR01942SE

This certificate, issued to Aerometals 3920 Sandstone Drive El Dorado Hills, CA 95762

Part 27 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: H3WE Make: MD Helicopter Inc.

Model: 369A and 369HM/HS/HE

Description of the Type Design Change: Fabrication of AMC Tail Rotor Pitch Control Assemblies in accordance with AMC Master Data List No. MDL-AMC-028, Revision IR, dated August 18, 2008, or later FAA-approved revision; and installation of this assembly in accordance with AMC Installation Instructions No.

AMC MI-07001, Revision IR, dated June 28, 2007, or later FAA-approved revision.

Limitations and Conditions: Approval of this change in type design applies to the rotorcraft 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 by the installer that the relationship between this change and any of the other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that rotorcraft.

A copy of this certificate must be maintained as part of the permanent record 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: July 12, 2007 Date reissued: December 11, 2008 Date of issuance: November 12, 2008 Date amended:

(Signature)

Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (2)

- December 11, 2008: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/13/dd/13dd4a84ac5dbce812c9bc3f10774177513a4078b134a27656120975bc315898)
- November 12, 2008: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/c3/5b/c35bcdfb9631835190f5df5c992bd4d2753c3861c1b2997720e1567b45fd2e5a)

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