# STC SA04114CH

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Hartzell Propeller LLC, United States
- Description: Installation of Engine Preheat Kit, P/N TA3123-1 for 115 volt application
- Applied: April 21, 2016
- Status date: March 25, 2024
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A00007SE](https://openairdocs.org/tcds/A00007SE)
- Certificate PDF: https://openairdocs.org/files/sha256/b3/7d/b37d672150c68d018b3c23c14d9c6126d868e674b09aa2cc4f59154a67824be5
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194655406420240404132407.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA04114CH

## ADs that name it (0)

None.

## Approved models (1)

- Daher Aircraft Design LLC Kodiak 100 ([TCDS A00007SE](https://openairdocs.org/tcds/A00007SE))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

SEAL AVATO Department of Transportation United States of America Federal Aviation Administration TORIMISTRATOS Supplemental Type Certificate Number: SA04114CH This certificate issued to: Hartzell Propeller LLC One Propeller Place Piqua, OH 45356 Part 23 of the Code of Federal Regulations.

Original Product Make: Daher Aircraft Design, LLC Type Certificate Number: A00007SE Model: Kodiak 100 Description of Type Design Change:

Installation of Engine Preheat Kit, p/n TA3123-1 for 115 volt application in accordance with Aircraft Preheat Kit drawing TA3123-1 Revision F, dated January 10, 2024 or later FAA approved revisions and Preheat Kit Installation Instruction TNF3123 Revision C, dated November 7, 2023 or later FAA approved revisions, or Installation of Engine (See Continuation Sheet 3 of 3) Limitations and Conditions:

1. The installer must determine whether this design change is compatible with previously approved modifications.

2. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

Date of Application: April 21,2016 Date Reissued: November 10,2023 Date of Issuance: July 13,2016 Date Amended: March 25, 2024 By Direction of the Administrator Signature.

Paul (Vu) Nguyen Title: Central Certification Branch Compliance & Airworthiness Division (Ref, 14 CFR 21.120).

United States of America Department of Transportation Federal Aviation Administration TORM STRATOS Supplemental Type Certificate (Continuation Sheet) Number: SA04114CH Date Amended: March 25, 2024 (Continued from Page 1: Description of Type Design Change) Preheat Kit, p/n TA3123-2 for 230 volt application in accordance with Aircraft Preheat Kit drawing TA3123-2 Revision F, dated January 10, 2024 or later FAA approved revisions, and Preheat Kit Installation Instruction TNF3123 Revision C, dated November 7, 2023 or later FAA approved revisions.

(Continued from Page 1: Limitations and Conditions)

3. FAA accepted Instructions for Continued Airworthiness (ICA) document # TCA 1000 Revision D, dated August 7, 2023 or later FAA approved revisions, and Operating Guide document # TPG1000 Revision F, dated August 7 or later FAA approved revisions are required.

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

- END - This

## Every issue (2)

- March 25, 2024: Amended, Current. [certificate](https://openairdocs.org/files/sha256/b3/7d/b37d672150c68d018b3c23c14d9c6126d868e674b09aa2cc4f59154a67824be5)
- July 13, 2016: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/11/c8/11c88fcaee17c14dfec4001d22e90544745c50990cc47a7361e43ccebeb7135a)

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