# STC SA00367DE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Oilamatic Inc, United States
- Description: Installation of an Oilamatic Preoiler system.
- Applied: September 30, 1998
- Status date: January 20, 1999
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A21](https://openairdocs.org/tcds/3A21)
- Certificate PDF: https://openairdocs.org/files/sha256/80/9b/809bdfb2cd592b8ed3ab20b82abb0f168306ba16416378d86ffa9272331ab6d7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/35C00838411E785B85256CC1007DC8D0.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00367DE

## ADs that name it (0)

None.

## Approved models (28)

- Cessna Aircraft Company 210 ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210-5 (205) ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210-5A (205A) ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210A ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210B ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210C ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210D ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210E ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210F ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210G ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210H ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210J ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210K ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210L ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210M ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210N ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210R ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company P210N ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company P210R ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210F ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210G ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210H ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210J ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210K ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210L ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210M ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210N ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210R ([TCDS 3A21](https://openairdocs.org/tcds/3A21))

## 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: SA00367DE This certificate issued to: Oilamatic, Inc.

P.O. Box 5284 Englewood CO 80155 Part 3 of the Civil Air Regulations.

Original Product -Type Certificate Number: ЗА21 Make: Cessna Aircraft Company Model: 210, 210A, B, C, D, E, F, G, H, J, K, L, M, N, R, T210F, G, H, J, K, L, M, N & R, P210N & P210R,

(205) 210-5 & (205A) 210-5A Description of Type Design Change:

Installation of an Oilamatic Preoiler system in accordance with Oilamatic, Inc. Drawing List No. 210400, Revision N/C, dated September 30, 1998, FAA Approved January 19, 1999 or later FAA approved revision.

1. FAA Approved Airplane Flight Manual Supplement, Rev N/C, dated January 20, 1999 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. 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.

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

Date of Application: September 30, 1998 Date Reissued:

Date of Issuance: FEDERAL AVIATION January 20, 1999 By instion of the penis oater Date Amended:

Ronald F. May (Signature) Manager TOMINIST RATION Northwest Mountain Region Denver Aircraft Certification Office (Title)

## Every issue (1)

- January 20, 1999: Issued, Current. [certificate](https://openairdocs.org/files/sha256/80/9b/809bdfb2cd592b8ed3ab20b82abb0f168306ba16416378d86ffa9272331ab6d7)

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