# STC SA5202NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Fly In Vacations, United States
- Description: Installation of Avco-Lycoming engine model IO-360-C1D6 modified.
- Applied: February 7, 2002
- Status date: June 2, 2014
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A12SO](https://openairdocs.org/tcds/A12SO)
- Certificate PDF: https://openairdocs.org/files/sha256/bd/0c/bd0cbb80936acf2bfa3f7734b005bcc38dd928535eb3c56c8c5fb82f3dda69cb
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1C88E18E6CCA148E86257CF2004B4B00.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA5202NM

## ADs that name it (0)

None.

## Approved models (2)

- Commander Aircraft Corporation 112 ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))
- Commander Aircraft Corporation 112B ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))

## 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.

United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate N umber SA5202NM This certificate, issued to Fly In Vacations 6395 Parkhill Road Santa Margarita, California 93453 Part 23* of the Federal Aviation Regulations.

*Certification basis is set forth in Type Certificate Data Sheet A12SO Original ProductType Certificate Number: A12SO Make: Commander Aircraft Corporation Model: 112 and 112B Description of the Type Design Change:

Installation of AVCO-Lycoming engine Model I0-360-C1D6 modified in accordance with Supplemental Type Certificate No. SE5203NM for installation of turbocharger and induction air intercooler. Installation shall be in accordance with "Installation Manual, Installation Drawings, and Parts List (P/N RCM-1000)", dated September 5, 1990, or later FAA approved revision. Also, installation of Hartzell HC-E3YR-1RF/F7392 propeller and C-3535- 1(P) spinner in accordance with Installation Instructions, dated January 25, 1998, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design appiies to the above model aircraft only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer 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 the appropriate FAA Approved Airplane Flight Manual Supplement must be maintained as part of the permanent records for the modified aircraft. 1 NOTE 1: For all aircraft modified in accordance with this STC to install the turbocharged induction cooled Lycoming engine Model I0-360-C106, FAA Approved Flight Manual Supplement dated February 2, 1991, or later FAA approved revision must be maintained as part of the permanent records for the modified aircraft.

NOTE 2: For all aircraft modified in accordance with this STC to install the Hartzell HC-E3YR-1RF/F7392 propeller, FAA Approved Flight Manual Supplement dated February 23, 1998, or later FAA approved revision 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.

Date of application: February 7, 2002 Date reissued: June 2, 2014 Date of issuance: June 20, 2003 Date amended: March 6, 1998

Todd Dixon (Signature) Northwest Mountain Regional Manager Denver Aircraft Certification Office (Title)

## Every issue (2)

- June 2, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/bd/0c/bd0cbb80936acf2bfa3f7734b005bcc38dd928535eb3c56c8c5fb82f3dda69cb)
- March 6, 1998: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/c0/88/c088198f9e043b184efd292106784c36d8988eb3e42a7786d658e4e8d165f0f9)

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