# STC SA2-880

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Aerocessories Company, United States
- Description: Installation of nacelle changes and exhaust system changes using existing 0-478-B or 0-470-M engines.
- Applied: November 25, 1959
- Status date: May 1, 1973
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A10](https://openairdocs.org/tcds/3A10)
- Certificate PDF: https://openairdocs.org/files/sha256/5a/21/5a216104a3651926d1e0fe957a2c99ffe9b86765d2791e25a379f86f952c5a4e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B61E7CB3C25ED707862579A70060702B.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2-880

## ADs that name it (0)

None.

## Approved models (8)

- Cessna Aircraft Company 310 ([TCDS 3A10](https://openairdocs.org/tcds/3A10))
- Cessna Aircraft Company 310B ([TCDS 3A10](https://openairdocs.org/tcds/3A10))
- Cessna Aircraft Company 310C ([TCDS 3A10](https://openairdocs.org/tcds/3A10))
- Cessna Aircraft Company 310D ([TCDS 3A10](https://openairdocs.org/tcds/3A10))
- Cessna Aircraft Company 310E ([TCDS 3A10](https://openairdocs.org/tcds/3A10))
- Cessna Aircraft Company 310F ([TCDS 3A10](https://openairdocs.org/tcds/3A10))
- Cessna Aircraft Company 310G ([TCDS 3A10](https://openairdocs.org/tcds/3A10))
- Cessna Aircraft Company 310H ([TCDS 3A10](https://openairdocs.org/tcds/3A10))

## 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: SA2-880 This certificate issued to: Aerocessories CO.

1779 Fitzgerald Road Simi, California 93065 Part 3 of the CIVII AST Regulations Original Product - Type bertificate Number: 3A20 Make: Cessne Model: 310, 310B, 310C, 310D, 310E, 310F, 310G, 310H Description of Type Design Change: Installation of nacelle changes and exhaust system changes using existing 0-470-B or 0-470-M engines in accordance with Clark Engineering Service Drawing C103032-500 Revision D dated 1/20/61, or instellation of nacelle changes and exhaust system using I0-470-D engines in accordance with Clark Engineering Service Drawing C103032 Basic Revision D dated 1/20/61.

Limitations and Conditions: SIC SA2-765 engine mount installation is required.

Date of Issuance: Date of Application: November 25, 1959 March 22, 1961 Date Amended: 5/27/69; 5/1/73 Sule missued: 5/19/61; 4/29/63; 5/28/64; Revision 5 EDERAL AVIATION Staministrater * ( Signature ) ton TO MINISTRATO Glen W. Welsh Chief, Engineering and Manufacturing Branch (Title ) 47 FAA FORM 8110-2 (10-68)

## Every issue (1)

- May 1, 1973: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/5a/21/5a216104a3651926d1e0fe957a2c99ffe9b86765d2791e25a379f86f952c5a4e)

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