# STC SA00121DE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Oilamatic Inc, United States
- Description: Installation of Oilamatic Preoiler system.
- Applied: August 6, 1993
- Status date: August 17, 1994
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A12CE](https://openairdocs.org/tcds/A12CE)
- Certificate PDF: https://openairdocs.org/files/sha256/d1/44/d144e6e71fd4c94642aea6fcdc95bd966952e7fca285ab0874a8d5f8979994e7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0EFCC62D27ADFA3D85256CC1007DC7BD.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00121DE

## ADs that name it (0)

None.

## Approved models (3)

- Hawker Beechcraft Corporation 60 ([TCDS A12CE](https://openairdocs.org/tcds/A12CE))
- Hawker Beechcraft Corporation A60 ([TCDS A12CE](https://openairdocs.org/tcds/A12CE))
- Hawker Beechcraft Corporation B60 ([TCDS A12CE](https://openairdocs.org/tcds/A12CE))

## 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: SA00121DE This certificate issued to: Oilamatic, Inc.

Part 23 of the Federal Aviation Regulations.

Original Product Type Certificate Number: A12CE Make: Beech Aircraft Corporation Model: 60, A60, B60 Description of Type Design Change:

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

B60400, initial release, dated July 1, 1994, or later FAA approved revision.

1. FAA approved Airplane Flight Manual Supplement Rev. No. N/C, dated August 17, 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, 1993 Date Reissued:

Date of Issuance: August 17, 1994 Date Amended:

FEDERAL AVIATION By Direction of the Administrator sechr RICHARD E. JENNINGS (Signature) Manager HOMINIST RATION Northwest Mountain Region, Denver, Colorado Denver Aircraft Certification Office (Title)

## Every issue (1)

- August 17, 1994: Issued, Current. [certificate](https://openairdocs.org/files/sha256/d1/44/d144e6e71fd4c94642aea6fcdc95bd966952e7fca285ab0874a8d5f8979994e7)

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