# STC SE7562SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Stratus Tool Technologies LLC
- Description: Install adapter to permit use of a spin-on oil filter.
- Status date: August 6, 2015
- Data sheets: E-252, E-252, E-252, E-252, E-252, E-252, E-252, E-252, E-252, E-252, E-252, E-252, E-252, E-252, E-252, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233, E-233
- Certificate PDF: https://openairdocs.org/files/sha256/14/da/14daf25460ac08682e94e05439ea7e1ad9f833c0122ee6bca9c651f1e1d2942b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FD83A05D59763FB186257EE6005DDBE3.0001
- Page: https://openairdocs.org/stc/SE7562SW

## ADs that name it

None.

## Approved models (47)

- Continental Motors C75-12 (TCDS E-233)
- Continental Motors C75-12B (TCDS E-233)
- Continental Motors C75-12BF (TCDS E-233)
- Continental Motors C75-12BFH (TCDS E-233)
- Continental Motors C75-12F (TCDS E-233)
- Continental Motors C75-12FH (TCDS E-233)
- Continental Motors C75-12FHJ (TCDS E-233)
- Continental Motors C75-12FJ (TCDS E-233)
- Continental Motors C75-12J (TCDS E-233)
- Continental Motors C75-15 (TCDS E-233)
- Continental Motors C75-15F (TCDS E-233)
- Continental Motors C75-8 (TCDS E-233)
- Continental Motors C75-8F (TCDS E-233)
- Continental Motors C75-8FH (TCDS E-233)
- Continental Motors C75-8FHJ (TCDS E-233)
- Continental Motors C75-8FJ (TCDS E-233)
- Continental Motors C75-8J (TCDS E-233)
- Continental Motors C85-12 (TCDS E-233)
- Continental Motors C85-12F (TCDS E-233)
- Continental Motors C85-12FH (TCDS E-233)
- Continental Motors C85-12FHJ (TCDS E-233)
- Continental Motors C85-12FJ (TCDS E-233)
- Continental Motors C85-12J (TCDS E-233)
- Continental Motors C85-14 (TCDS E-233)
- Continental Motors C85-14F (TCDS E-233)
- Continental Motors C85-15 (TCDS E-233)
- Continental Motors C85-15F (TCDS E-233)
- Continental Motors C85-8 (TCDS E-233)
- Continental Motors C85-8F (TCDS E-233)
- Continental Motors C85-8FHJ (TCDS E-233)
- Continental Motors C85-8FJ (TCDS E-233)
- Continental Motors C85-8J (TCDS E-233)
- Continental Motors Inc C90-12F (TCDS E-252)
- Continental Motors Inc C90-12FH (TCDS E-252)
- Continental Motors Inc C90-12FJ (TCDS E-252)
- Continental Motors Inc C90-12FP (TCDS E-252)
- Continental Motors Inc C90-14F (TCDS E-252)
- Continental Motors Inc C90-14FH (TCDS E-252)
- Continental Motors Inc C90-14FJ (TCDS E-252)
- Continental Motors Inc C90-16F (TCDS E-252)
- Continental Motors Inc C90-8F (TCDS E-252)
- Continental Motors Inc C90-8FJ (TCDS E-252)
- Continental Motors Inc O-200-A (TCDS E-252)
- Continental Motors Inc O-200-B (TCDS E-252)
- Continental Motors Inc O-200-C (TCDS E-252)
- Continental Motors Inc O-200-D (TCDS E-252)
- Continental Motors Inc O-200-X (TCDS E-252)

## 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.

Number SE7562SW

This certificate issued to: Stratus Tool Technologies, LLC 90 Glenda Trace Newman, GA 30265

Part 13of the Civil Air Regulations.

Original Product – Type Certificate Number: E-233, E-252

Make: Teledyne Continental Model: C-75 Series; C-85 Series; C-90 Series, O-200 Series Description of Type Design Change:

Install adapter to permit use of a spin-on oil filter in accordance with F. & M. Enterprises’ Installation Instructions for Model TAF Oil Filter, dated October 26, 1998, or later FAA approved revision.

Date of application: January 09, 1989 Date reissued: May 08, 1998, July 13, 2015, August 06, 2015 Date of issuance: March 15, 1989 Date amended: 10/24/1989; 11/17/1989; 11/19/1990; 04/30/1992;

03/01/1999 Rev. 5

Signature Scott A. Horn

Title Manager, Fort Worth Aircraft Office, Southwest Region

FAA Form 8110-2 (8/13) Page 1

Number: SE7562SW Date of Issuance: March 15, 1989 Reissuance Date: August 06, 2015

Compatibility of this modification with airframe equipment and structural clearances must be determined by the installer. Engines modified in accordance with this STC will not differ in performance or operating limitations for unmodified engines.

Installation of the modified engine in the airframe is considered to be a minor change by definition in accordance with FAR Part 21.93. Due to the nature of the modification, no further FAA approval is required for the airplane.

Only the following filters are eligible for this installation:

Champion No. Ch48108 A.C. No. OF-53A

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.

-END-

FAA Form 8110-2 (8/13) Page 3

**SUPPLEMENTAL TYPE CERTIFICATE, FAA FORM 8110-2 (CONTINUED)**

To (Name of transferee)

(Address of transferee)

(Number and street)

(City, State, and ZIP Code)

From (Name of grantor)

(Address of grantor)

(Number and street)

(City, State, and ZIP Code)

FAA Form 8110-2 (8/13) Page 2

## Every issue (1)

- August 6, 2015: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/14/da/14daf25460ac08682e94e05439ea7e1ad9f833c0122ee6bca9c651f1e1d2942b)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.