STC SE3782NM

Supplemental type certificate · Western Skyways Aircraft Modifications Inc.

Holder
Western Skyways Aircraft Modifications Inc. · United States
Status
Current · Reissued
Status date
March 8, 2023
Applied
February 1, 1988
Product
Engine
Data sheet
TCDSE8CE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of an intercooler in the engine air induction system.

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: SE3782NM Possession on this Supplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC ’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STC holder. An STC holder who allows a person to alter an aircraft, aircraft engine, or propeller must provide that person with written permission acceptable to the FAA. (Ref. 14 CFR 21.120).

FAA Form 8110-2 (6/20) SUPERSEDES PREVIOUS EDITION Page 1 of 2

This certificate issued to: Western Skyways Aircraft Modifications Inc.

333 West Boulevard, Suite 400 Rapid City, SD 57701

Part 13 of the Civil Air Regulations. Effective June 11, 1976.

Original Product Type Certificate Number: E8CE

Make: Continental Aerospace Technologies, INC.

Model: TSIO-520M Installation of an intercooler in the engine air induction system per Riley International Corp. Master Drawing List R17801, Revision N/C, dated February 19, 1988, or later FAA approved revisions.

The approval of this change in type design requires installation of STC No. SA3781NM and is restricted to the basic engines of the specified models that are otherwise unmodified. This approval should not be extended to other engines of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that 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.

The STC ’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STC holder. An STC holder who allows a person to alter an aircraft, aircraft engine, or propeller must provide that person with written permission acceptable to the FAA. (Ref. 14 CFR 21.120).

FAA Form 8110-2 (6/20) SUPERSEDES PREVIOUS EDITION Page 2 of 2

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 · 1

MakeModelData sheet
Continental Aerospace Technologies Inc.TSIO-520-ME8CE

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
March 8, 2023Reissued, currentCertificate
May 20, 2019Reissued, earlier issueCertificate