# STC SA00123DE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Oilamatic Inc, United States
- Description: Installation of Oilamatic preoiler system.
- Applied: August 6, 1994
- Status date: September 6, 1994
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A16CE](https://openairdocs.org/tcds/A16CE)
- Certificate PDF: https://openairdocs.org/files/sha256/34/ef/34ef4844e552f4c7a4c033faa12f2e16116b6a87b4b2661d92529e072bc999f1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/22DB8466922447D685256CC1007DC7BF.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00123DE

## ADs that name it (0)

None.

## Approved models (4)

- Cessna Aircraft Company 207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company 207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company T207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company T207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))

## What the certificate says

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

Inite Crater of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00123DE This certificate issued to: Oilamatic, Inc.

Part 23 of the Federal Aviation Regulations.

Original Product -Type Certificate Number: A16CE Make: Cessna Aircraft Company Model: 207, 207A, T207, T207A Description of Type Design Change:

Installation of Oilamatic Preoiler system in accordance with FAA approved Oilamatic, Inc. Drawing List No.

207400, initial release, dated April 5, 1994, or later FAA approved revision.

1. FAA approved Airplane Flight Manual Supplement Rev. No. N/C, dated August 24, 1994 or later FAA approved revision is required.

2. This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship 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.

3. A copy of this Certificate and Flight Manual Supplement must be maintained as part of the permanent records for the modified aircraft.

Date of Application: August 6, 1994 Date Reissued:

Date of Issuance: September 6, 1994 Date Amended:

FEDERAL By Direction of the Administrator inan ROMAN T. GABRYS, (Signature) Acting Manager "O MINISTRATIO Denver Aircraft Certification Office Northwest Mountain Region, Denver, Colorado (Title)

## Every issue (1)

- September 6, 1994: Issued, Current. [certificate](https://openairdocs.org/files/sha256/34/ef/34ef4844e552f4c7a4c033faa12f2e16116b6a87b4b2661d92529e072bc999f1)

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