STC SR01675SE

Supplemental type certificate · Aerometals

Holder
Aerometals · United States
Status
Current · Reissued
Status date
December 11, 2008
Applied
October 18, 2005
Product
Aircraft · Rotorcraft
Certification basis
Part 21
Data sheet
TCDSH3WE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Fabrication of AMC Part Number AM369A4516 ( ), N1 Tachometer Indicator and AM369D24518 ( ) N2/NR Tachometer Indicator

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SR01675SE 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: 369A, 369HE, 369HM, 369HS, 369D, 369E, 369FF, 500N

Description of the Type Design Change: Fabrication of AMC Part Number AM369A4516 ( ), N1 Tachometer Indicator and AM369D24518 ( ) N2/NR Tachometer Indicator in accordance with AMC Master Drawing List No.

MDL-AMC-023, Revision A, dated July 5, 2006, or later Federal Aviation Administration (FAA)-approved revision.

The N1 Tachometer Indicator must be installed in accordance with AMC Installation Instructions AMC MI-05006, Revision IR, dated September 22, 2005, or later FAA approved revision. The N2/NR Techometer Indicator must be installed in accordance with AMC Installation Instructions AMC MI-05007, Revision IR, dated September 22, 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.

Date of application: October 18, 2005 Date reissued: December 11, 2008 Date of issuance: May 25, 2006 Date amended: September 12, 2006

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

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 8

MakeModelData sheet
MD Helicopter Inc.369AH3WE
MD Helicopter Inc.369DH3WE
MD Helicopter Inc.369EH3WE
MD Helicopter Inc.369FFH3WE
MD Helicopter Inc.369HEH3WE
MD Helicopter Inc.369HMH3WE
MD Helicopter Inc.369HSH3WE
MD Helicopter Inc.500NH3WE