# STC SE5032NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: TC SKYROCKET LLC, United States
- Description: Installation of Teledyne Cont. Motor pressurized magnetos, kit no. EQ6565.
- Applied: September 20, 1989
- Status date: November 10, 2009
- Product: Engine
- Certification basis: Part 21, Part 33
- Data sheets: [TCDS E9CE](https://openairdocs.org/tcds/E9CE)
- Certificate PDF: https://openairdocs.org/files/sha256/ef/97/ef9782f21dad05718c796ba81934bde7e3f693143a4fd0abcd26412d58237584
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/015BC25EA9B8658E862576730070778E.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SE5032NM

## ADs that name it (0)

None.

## Approved models (2)

- 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))

## 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.

This Certificate issued to TC SKYROCKET LLC 356 Expressway CT Gaylord, Michigan 49735 Part 33 of the Federal Aviation Regulations dated February 1, 1965, as mended by 33-1.

E9CE Continental TSIO-360-C, -CB Description of Type Design Change : Installation of Teledyne Continental Motor Pressurized Magnetos, Kit No. EQ6565, in accordance with FAA Approved R iley International Corporation, Drawing No.

RPM01, Revision N/C, dated October 10, 1990, or later FAA approved revision to this document.

Supplemental Type Certificate (STC) Nos. SE 4505NM and SA5033NM are required as part of this installation.

Limitations and Conditions: The approval of this change in type design is restricted to the engines identified above which have incorporated the above listed STCs and are otherwise unmodified. Engines which have previously approved modi fications shall not be modified by this STC, unless it is determined the interrelationship between this change and any previously approved modifications will introduce no adverse effect upon the airworthiness of the engine. If the holder agrees to permit another person to use this certificate to alter the product, the holder sh all give the other person written evidence of that permission.

Date of application : September 20, 1989

Date of issuance : December 28, 1990

Date reissued : October 4, 1996, March 3, 1998, July 18, 2000, November 10, 2009

( Signature) Supervisor, Technical & Administrative Support Staff Los Angeles Aircraft Certification Office (Ti l )

NOTE:

**DO NOT DELETE THIS PAGE.**

**DO NOT ADD ANY DATA TO THIS PAGE.**

**THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.**

Number

## Every issue (1)

- November 10, 2009: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ef/97/ef9782f21dad05718c796ba81934bde7e3f693143a4fd0abcd26412d58237584)

---
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.