# STC SE00736LA

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Michael Adamson, United States
- Description: Replacement of various fuel and lubrication system parts with items from an IO-470-K engine to permit installation in a Beech model 35-A33 airplane. These changes must be made in accordance with Michael Adamson, Installation Instructions, Continental O-470-M Conversion, Manual #1, Revision N/C, dated January 6, 1999, or later FAA approved revisions.
- Applied: May 13, 1997
- Status date: March 19, 1999
- Product: Engine
- Certification basis: Part 13, Part 21
- Data sheets: [TCDS E-273](https://openairdocs.org/tcds/E-273)
- Certificate PDF: https://openairdocs.org/files/sha256/ef/a7/efa7f5c0fa717fbd88fa91df2c11e537f09c74e997dd106741ed52eca8d79f9e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1DAF0C42B513F50B86256E7F004E37B3.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SE00736LA

## ADs that name it (0)

None.

## Approved models (1)

- Teledyne Continental Motors O-470-M ([TCDS E-273](https://openairdocs.org/tcds/E-273))

## 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

MICHAEL ADAMSON 3695 Avalon Street #30 Riverside, California 92509 Part 13 of the Civil Air Regulations.

E-273 Rev. 36 Teledyne Continental Motors O-470-M, Serial Number 53012-8-M Description of Type Design Change: Replacement of various fuel and lubrication system parts with items from an IO-470-K engine to permit installation in a Beech model 35-A33 airplane. These changes must be made in accordance with Michael Adamson, Installation Instructions, Continental O-470-M Conversion, Manual #1, Revision N/C, dated January 6, 1999, or later FAA approved revisions.

Limitations and Conditions: The approval of this modification in type design applies to the above listed engine only. This approval should not be extended to other engines of this model. This STC is required prior to accomplishing STC SA00735LA. A copy of this STC SE00736LA, and Michael Adamson Installation Instructions, Continental O-470-M Conversion, Manual #1, Revision N/C, dated January 6, 1999, or later FAA approved revision, shall be maintained as part of the permanent maintenance records of the modified engine. (Limitations continued on Page 3)

Date of application : May 13, 1997

Date of issuance : March 19, 1999

Rejean Chartier ( Signature) Manager, Propulsion Branch 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 SE00736LA

The center of gravity location, weight, carburetion type, oil capacity, maximum permissible cylinder temperature, and fuel pressure limits, published in TCDS E-273 Rev. 36 no longer apply to the above engine model and serial number. A revised weight and balance must be computed by weighing the aircraft modified by installation of this engine.

Oil Sump Capacity: (quarts) 10 usable at 18o noseup and 14o nosedown attitudes

Cylinder head maximum temperature: 460o bayonet probe

-END-

## Every issue (1)

- March 19, 1999: Issued, Current. [certificate](https://openairdocs.org/files/sha256/ef/a7/efa7f5c0fa717fbd88fa91df2c11e537f09c74e997dd106741ed52eca8d79f9e)

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