# STC SR01169LA

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Aerometals, United States
- Description: Installation of Aerometals High Speed Acturator Assemblies, P/N 369X27001
- Applied: June 1, 2000
- Status date: July 13, 2001
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H3WE](https://openairdocs.org/tcds/H3WE)
- Certificate PDF: https://openairdocs.org/files/sha256/2c/7b/2c7b63cf65582435ffce342b99a84d30fd7281081628e26750b6cd5bb739d1ee
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F45A7B0D835B4042862573D8006AE1BC.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR01169LA

## 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

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR01169LA This certificate issued to: Aerometals 3920 Sandstone Drive El Dorado Hills, CA 95762 Purt *67 of the Tivil Air Pegulaliens. *Certification basis is set forth in Type Certificate Data Sheet H3WE* Original Product Type Certificute Number: H3WE Abuke: McDonnell Douglas Helicopter Co.

Model: 369D, E, FF, HE, HS, HM and 500N Description of Type Design Change: Installation of Aerometals High Speed Actuator Assemblies, PIN 369X27001 in accordance with FAA Approved Aerometals Master Drawing List (MDL) No. 35, Revision "D" dated March 20, 2001, or later FAA Approved Revisions.

Limitations and Conditions: The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The approval of this modification applies to the above noted aircraft model series only. A copy of this STC must be included in the permanent records of the modified aircraft. 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 June 2000 Date Reissued:

Date of Issuance: July 13,2001 Dute unended:

FEDERAL AVIATION By Direction of the Administrator Pan therati * (Signature) TOMINISTRATO Manager, Systems & Equipment Branch Los Angeles Aircraft Certification Office (Title)

## Every issue (1)

- July 13, 2001: Issued, Current. [certificate](https://openairdocs.org/files/sha256/2c/7b/2c7b63cf65582435ffce342b99a84d30fd7281081628e26750b6cd5bb739d1ee)

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