# STC SA00972LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Richard F Honn, United States
- Description: Installation of Teledyne Continental Motor Pressurized Magnetos, Kit No. EQ6565. T337G s/n P3370001-P3370292, except P3370109 & P3370196; P337H S/N 3370293-3370356, & P3370196
- Applied: April 11, 2000
- Status date: November 10, 2009
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A6CE](https://openairdocs.org/tcds/A6CE)
- Certificate PDF: https://openairdocs.org/files/sha256/dd/41/dd417bb9b8d72bf2a167bd84933e2116f59dc54973dcb7e2b75f9bd29134bebe
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DD29136554F7ECC28625769A006D40C3.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00972LA

## ADs that name it (0)

None.

## Approved models (2)

- Cessna Aircraft Company P337H ([TCDS A6CE](https://openairdocs.org/tcds/A6CE))
- Cessna Aircraft Company T337G ([TCDS A6CE](https://openairdocs.org/tcds/A6CE))

## 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 EXPRSSWAY CT GAYLORD, MICHIGAN 49733 Part 23 of the Federal Aviation Regulations.

A6CE

Cessna

T337G, S/N P3370001-P3370292, except P3370109 & P3370196; P337H S/N P3370293-P3370356, & P3370196 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.

Limitations and Conditions: The approval of the change in type design is restricted to the aircraft identified above and are otherwise unmodified. This a pproval should not be extende d to aircraft of this model on which other previously appr oved modifications are incorporated unless it is determined that the interrelationship between this ch ange and any previously approve d modifications will introduce no adverse effect upon the airworthiness of that aircraft.

This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: April 11, 2000

Date of issuance: April 25, 2000

Date reissued: July 18, 2000, November 10, 2009

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

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 (STC No.)

## Every issue (1)

- November 10, 2009: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/dd/41/dd417bb9b8d72bf2a167bd84933e2116f59dc54973dcb7e2b75f9bd29134bebe)

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