# STC SA00496SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Oregon Aircraft Design LLC, United States
- Description: Installation of Oregon Aircraft Design Engine Mount Heat Shields.
- Applied: November 3, 1997
- Status date: December 20, 2000
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS 3A17](https://openairdocs.org/tcds/3A17), [TCDS 3A24](https://openairdocs.org/tcds/3A24), [TCDS 5A6](https://openairdocs.org/tcds/5A6)
- Certificate PDF: https://openairdocs.org/files/sha256/ec/10/ec10d513aebcf81527448e75e233b7a20ccea20aeae7cb6af7e4d683bc4b0310
- Approved model list and other attachments: [AML SA00496SE.pdf](https://openairdocs.org/files/sha256/6c/17/6c17b1c71ffc8d0bf78cfa56ba422682b3316ff2b25b4694fcee2c87dc88510c)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E402F5B784AD050485256CC1007DC967.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00496SE

## ADs that name it (0)

None.

## Approved models (42)

- Cessna Aircraft Company 180 ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180A ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180B ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180C ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180D ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180E ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180F ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180G ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180H ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180J ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180K ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182A ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182B ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182C ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182D ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182E ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182G ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182H ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182J ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182K ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182L ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182M ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182N ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182P ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182Q ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182R ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 185 ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185A ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185B ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185C ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185D ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company A185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company A185F ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company R172E ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company R172F ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company R172G ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company R172H ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company R172J ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company R172K ([TCDS 3A17](https://openairdocs.org/tcds/3A17))

## 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.

Number SA00496SE This certificate, issued to Oregon Aircraft Design, LLC 31338 N.W. Hillcrest P. O. Box 1516 North Plains, OR 97133 Part * of the * Regulations.

Original ProductType Certificate Number: *See attached FAA Approved Model List Make: No. SA00496SE for a list of approved aircraft Model: models and applicable airworthiness regulations.

Description of the Type Design Change: Install Oregon Aircraft Design Engine Mount Heat Shields in accordance with Oregon Aircraft Design Drawing Lists and Installation Instructions per the attached Federal Aviation Administration (FAA) Approved Model List (AML) No. SA00496SE, dated January 21, 1998, or later FAA approved revisions.

Limitations and Conditions: Approval of this change in type design applies to the aircraft models listed on FAA AML No. SA00496SE only. This approval should not be extended to other aircraft on which other 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. A copy of this Certificate and FAA AML SA00496SE must be maintained as part of the permanent records for the modified aircraft.

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.

This certificate and the supporting data which is the ba sis for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: November 3, 1997 Date reissued:

Date of issuance: January 21, 1998 Date amended: December 20, 2000

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

### AML SA00496SE.pdf

**PAGE 1 OF 1 FAA APPROVED MODEL LIST (AML) SA00496SE FOR**

OREGON AIRCRAFT DESIGN ISSUE DATE: JANUARY 21, 1998

**ITEM AIRPLANE MAKE**

**AIRPLANE MODEL TYPE**

**CERTIFICATE NUMBER**

**CERTIFICATION**

**BASIS FOR**

**ALTERATION**

**FAA SEALED**

**DRAWING LIST**

**INSTALLATION**

**INSTRUCTIONS AML**

**AMENDED DATE**

NUMBER REV NUMBER REV 1 CESSNA R172E, R172F, R172G, R172H, R172J, R172K 3A17 CAR 3, dated May 15, 1956 DL 172XP 6/25/03 II 172XP 6/25/03 7/30/03 2 CESSNA 180, 180A- 180H, 180J, 180K 5A6 CAR 3, dated November 11, 1949 DL 182 5/12/99 II 182 5/12/99 6/4/1999 3 CESSNA 182, 182A- 182R 3A13 CAR 3, dated November 1, 1949 DL 182 5/12/99 II 182 5/12/99 6/4/1999 4 CESSNA A185E, A185F, 185, 185A-185E 3A24 CAR 3, dated May 15, 1956 DL 185 5/12/99 II 185 5/12/99 6/4/1999

FAA APPROVED: __________________________________________ DATE: _______________________________ Acting Manager, Seattle Aircraft Certification Office

Amended: 10/14/1998, 11/5/1998, 5/28/1999, 6/4/1999, 10/13/1999, 4/4/2002, 7/30/2003

## Every issue (1)

- December 20, 2000: Amended, Current. [certificate](https://openairdocs.org/files/sha256/ec/10/ec10d513aebcf81527448e75e233b7a20ccea20aeae7cb6af7e4d683bc4b0310), [AML SA00496SE.pdf](https://openairdocs.org/files/sha256/6c/17/6c17b1c71ffc8d0bf78cfa56ba422682b3316ff2b25b4694fcee2c87dc88510c)

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