STC SE2393NM

Supplemental type certificate · Turboplus Aircraft Systems, Inc.

Holder
Turboplus Aircraft Systems, Inc. · United States
Status
Current · Reissued
Status date
February 24, 2017
Applied
April 1, 1984
Product
Engine
Certification basis
Part 21, Part 33
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 a magneto pressurization kit assembly and associated system for Bendix Models S6RN-1201 and 1205, and SLICK Models 662, 680, 6210 and 6220.

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.

Number SE2393NM

This Certificate issued to Turboplus Aircraft Systems, Inc.

4117 35th Ave NW Gig Harbor, WA 98335

Part 33 of the Federal Aviation Regulations.

Description of Type Design Change: Installation of a magneto pressurization kit assembly and associated system for Bendix Models S6RN-1201 and –1205, and SLICK Models 662, 680, 6210 and 6220 in accordance with Turboplus, Inc., Installation Instructions Drawing No. 16000 Rev. B, dated March 17, 1987, or later FAA Approved Revision.

NOTE: The above approval includes the option of installing Turboplus Kit Design No. 16000 Rev. B.

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 these models 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 and FAA Approved Flight Manual Supplement 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

E8CE-18

Continental

TSIO-520-C, -G, -H, -L, -M, -P, -R and -AF

Date of application : April 1, 1984

Date of issuance : May 14, 1984

Date reissued : 4/24/86; 10/30/87; 10/25/00;

8/25/05; 10/15/07; 2/24/17 Date amended : 11/15/84; 04/29/87; 10/25/00

(Signature) Manager, Technical and Administrative Support Staff, Los Angeles Aircraft Certification Office (Title)

Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street)

(City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street)

(City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

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 · 8

MakeModelData sheet
Continental Motors IncTSIO-520-AFE8CE
Continental Motors IncTSIO-520-CE8CE
Continental Motors IncTSIO-520-GE8CE
Continental Motors IncTSIO-520-HE8CE
Continental Motors IncTSIO-520-LE8CE
Continental Motors IncTSIO-520-ME8CE
Continental Motors IncTSIO-520-PE8CE
Continental Motors IncTSIO-520-RE8CE

Every issue · 3

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

DateStatusFiles
February 24, 2017Reissued, currentCertificate
October 15, 2007Reissued, earlier issueCertificate
August 25, 2005Reissued, earlier issueCertificate