# STC SE3864NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: American Aviation Inc, United States
- Description: Installation of American Aviation intercooler and associated systems.
- Applied: December 30, 1986
- Status date: November 1, 1998
- Product: Engine
- Certification basis: Part 21
- Data sheets: [TCDS E9CE](https://openairdocs.org/tcds/E9CE)
- Certificate PDF: https://openairdocs.org/files/sha256/3c/d6/3cd6b9c40c2a35f84cc9e6d03556734c881fc000ec83c29abdfada36f52c53a0
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8AE8DA708C6F5FDE85256CC2005A754A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SE3864NM

## ADs that name it (0)

None.

## Approved models (8)

- Teledyne Continental Motors TSIO-360-A ([TCDS E9CE](https://openairdocs.org/tcds/E9CE))
- Teledyne Continental Motors TSIO-360-AB ([TCDS E9CE](https://openairdocs.org/tcds/E9CE))
- Teledyne Continental Motors TSIO-360-B ([TCDS E9CE](https://openairdocs.org/tcds/E9CE))
- Teledyne Continental Motors TSIO-360-BB ([TCDS E9CE](https://openairdocs.org/tcds/E9CE))
- Teledyne Continental Motors TSIO-360-C ([TCDS E9CE](https://openairdocs.org/tcds/E9CE))
- Teledyne Continental Motors TSIO-360-CB ([TCDS E9CE](https://openairdocs.org/tcds/E9CE))
- Teledyne Continental Motors TSIO-360-H ([TCDS E9CE](https://openairdocs.org/tcds/E9CE))
- Teledyne Continental Motors TSIO-360-HB ([TCDS E9CE](https://openairdocs.org/tcds/E9CE))

## What the certificate says

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

Anita States DE America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SE3864NM This certificate issued to: American Aviation, Inc.

10555 Airport Drive Coeur d'Alene Airport Hayden Lake, ID 83835 Part 13 of the Civil Air Regulations, Original Product -Type Certificate Number: E9CE Make: Teledyne Continental Model: TSIO-360-A, AB, B, BB, C, CB, H and HB Description of Type Design Change: Installation of American Aviation, Inc., intercooler and associated systems in accordance with American Aviation, Inc., Report 81-1 or later FAA approved revision. The engines modified in accordance with this document may only be installed in aircraft modified per STC Number SA3863NM.

Engine operating limits are specified in American Aviation, Inc., FAA Approved Airplane Flight Manual Supplement which is required by STC Number SA3863NM.

Limitations and Conditions: Approval of this change in type design applies to the above model engines only.

This approval should not be extended to other engines 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 effect upon the airworthiness of that engine. A copy of this Certificate must be maintained as part of the permanent records for the modified engine.

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: December 30, 1986 Date Reissued:

Date of Issuance: July 8, 1987 Date Amended: 11/30/95; 11/01/98 FEDERAL AVIATION B By Direction of the Administrator .

Cavans fasion TOMINIS Y RATION Acting Manager, Seattle Aircraft (Signature) Certification Office (Title)

## Every issue (1)

- November 1, 1998: Amended, Current. [certificate](https://openairdocs.org/files/sha256/3c/d6/3cd6b9c40c2a35f84cc9e6d03556734c881fc000ec83c29abdfada36f52c53a0)

---
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.