# STC SA02605CH

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Kelly Aerospace Thermal Systems LLC, United States
- Description: Installation of Backup Alternator Kit
- Applied: April 22, 2008
- Status date: September 10, 2009
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13)
- Certificate PDF: https://openairdocs.org/files/sha256/8f/ed/8fedfa4c6b29850af08c6e5c496e05a50fe99c2833cb2fbdf58c8db2b95023bf
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/333F5A16181CE8F7862576330051C393.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02605CH

## ADs that name it (0)

None.

## Approved models (2)

- Cessna Aircraft Company 182T ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company T182T ([TCDS 3A13](https://openairdocs.org/tcds/3A13))

## 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.

Part 23 of the Federal Aviation Regulations. (See Type Certificate Data Sheet No. 3A13 for complete certification basis)

Original Product--Type Certificate Number : 3A13 Make : The Cessna Aircraft Company Model : 182T, T182T

Description of Type Design Change: Installation of Backup Alternator Kit in accordance with Kelly Aerospace Installation Instructions as listed on Kelly Aerospace Drawing List NC-08-025, Rev. H, dated June 11, 2009, or later FAA approved revision.

1. A copy of this certificate must be maintained as part of the permanent records for the modified aircraft.

2. FAA Approved Airplane Flight Manual Supplement (G1000 EFIS System), Doc. No. NC-08-027, Revision C, approved September 17, 2008, or later FAA approved revision, is required on board the modified aircraft, or,

3. FAA Approved Airplane Flight Manual Supplement (without G1000), Doc. No. NC-08-091, Revision A, approved September 17, 2008, or later FAA approved revision, is required on board the modified aircraft.

4. Compatibility of this design change with previously approved modifications must be determined by the installer.

5. 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.

Kelly Aerospace Thermal Systems, LLC 1625 Lost Nation Road Willoughby, OH 44094

Date of application : April 22, 2008

Date of issuance : July 25, 2008

Date amended : December 18, 2008, September 10, 2009

( Signature)

Steven L. Lardinois Manager, Systems and Flight Test Branch Chicago Aircraft Certification Office

( Title)

## Every issue (2)

- September 10, 2009: Amended, Current. [certificate](https://openairdocs.org/files/sha256/8f/ed/8fedfa4c6b29850af08c6e5c496e05a50fe99c2833cb2fbdf58c8db2b95023bf)
- July 25, 2008: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/a4/db/a4db82195581081d838db1a0b55ec5177fbbc396d1b086c5e107cae2e38da3ff)

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