# STC SE4315NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Timberman Allen E, United States
- Description: Replacement of the original engine oil screen with an external mounted full flow oil adapter and spin-on filter.
- Applied: February 24, 1988
- Status date: July 30, 1993
- Product: Engine
- Certification basis: Part 21
- Data sheets: [TCDS E-252](https://openairdocs.org/tcds/E-252)
- Certificate PDF: https://openairdocs.org/files/sha256/62/f0/62f094912476fa42d6a4ab8ea83b9430ab9731ca07439ac24110c08b068f5da5
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F505310D000F45B5862579CA00716009.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SE4315NM

## ADs that name it (0)

None.

## Approved models (1)

- Teledyne Continental Motors O-200-A ([TCDS E-252](https://openairdocs.org/tcds/E-252))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SE4315NM This certificate issued to: Allen E. Timberman Part 13 of the CiVil Air Regulations.

Original Product - Type Certificate Numben: E-252 Make: Continental Model: 0-200-A Description of Type Design Change: Replacement of the original engine oil screen with al external mounted full flow oil adapter and spin-on filter in accordance with FAA sealed copies of Timberman Master Drawing List No. AT-3-200-DL, dated March 31, 1988, and Installation Instructions No. OF-16-0200, dated March 31, 1988, or later FAA Approved revisions.

Limilaluns and bindilicApproval of this change in type design applies to the above model Continental 0-200-A engines. This approval should not be extended to other engines of this model on which 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 aircraft. (See Continuation Sheet page 3) Timberman Limitations and Conditions: of Type Certificate Data Sheet Number E-252 for Continental Model 0-200-A engine remain applicable.

The installation of an engine modified in accordance with this STC will require a determination by the installer that no interference is created with existing aircraft system.

Engines equipped with the Timberman spin-on oil filter must continue to be maintained in accordance with the original engine manufacturers maintenance tests ton, as topy of with wist be sed to the engine a tenance represence revision, a copy of which must A copy of this STC must be included in the permanent records of each engine which is modified in accordance with this STC.

This SIC covers the fabrication of all parts associated with this oil filter installation and also the physical modification of the Continental 0-200-A engines. Associated STC No. SA4318NM covers the use of this modified engine on specific airplane models, and also covers the mounting of the oil filter, filter base, and mounting plate on the firewalls of these airplanes.

- END -

**FAA FORM 8110-2-1 (10-69) PAGE 3 OF 3 PAGES**

## Every issue (1)

- July 30, 1993: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/62/f0/62f094912476fa42d6a4ab8ea83b9430ab9731ca07439ac24110c08b068f5da5)

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