# STC SR02095SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Aerometals, United States
- Description: Fabrication of a replacement Aerometals Scavenge Pump Assembly.
- Applied: March 19, 2010
- Status date: September 12, 2013
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H3WE](https://openairdocs.org/tcds/H3WE)
- Certificate PDF: https://openairdocs.org/files/sha256/ec/03/ec037ae98b1dc4359ec7267a27d0137d96f305afaab884b4906f9fb4dddf71a9
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/67DF911A0265D26486257BE40069B06A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR02095SE

## ADs that name it (0)

None.

## Approved models (8)

- MD Helicopter Inc. 369A ([TCDS H3WE](https://openairdocs.org/tcds/H3WE))
- 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.

Number SR02095SE

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

Part * of the * Regulations.

* Certification basis set forth in Type Certificate Data Sheet H3WE.

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

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

Description of the Type Design Change: Fabrication of a replacement Aerometals Scavenge Pump Assembly in accordance with Aerometals Master Drawing List Aero-MDL-010, Revision A, dated July 16, 2010, or later Federal Aviation Administration (FAA) approved revision; installation of this assembly in accordance with Aerometals Installation Instructions Aero-Inst-011, Revision NC, dated January 11, 2009, or later FAA-approved revision; and maintenance in accordance with the appropriate MDHI Maintenance Manual and Component Overhaul Manual.

Limitations and Conditions: Approval of this change in type design applies 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 records for 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: March 19, 2010 Date reissued: September 12, 2013 Date of issuance: December 17, 2010 Date amended:

(Signature)

Manager, Seattle Aircraft Certification Office (Title)

## Every issue (2)

- September 12, 2013: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ec/03/ec037ae98b1dc4359ec7267a27d0137d96f305afaab884b4906f9fb4dddf71a9)
- December 17, 2010: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/1a/82/1a8260404ba045f361bbc12a3bbb84bbee84f6de9d2c394e4a6c22af9989d54d)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.