# STC SA02552AK

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Burl's Aircraft LLC, United States
- Description: Installation of Hartzell Model HC-C2YR-1N/NG8301-3 Trailblazer propeller
- Applied: September 2, 2020
- Status date: July 20, 2021
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A-802](https://openairdocs.org/tcds/A-802)
- Certificate PDF: https://openairdocs.org/files/sha256/ef/21/ef217b22f502d8e089cfb92430a74c7245ada5353158b409fdd72adcd4ce7dd9
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B8D03A3865DF78BA8625871B00723D1C.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02552AK

## ADs that name it (0)

None.

## Approved models (2)

- AeroSedan LLC 15AC ([TCDS A-802](https://openairdocs.org/tcds/A-802))
- AeroSedan LLC S15AC ([TCDS A-802](https://openairdocs.org/tcds/A-802))

## 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.

**14 CFR 21.120)**

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 1 OF 2

Number: SA02552AK This certificate issued to:

Installation of Hartzell Model HC-C2YR-1N/NG8301-3 Trailblazer propeller in accordance with Instructions for Continued Airworthiness document number BA-8301-3-ICA, dated June 29, 2021, or later FAA accepted revision.

1. Instructions for Continued Airworthiness (ICA) document number BA-8301-3-ICA, dated June 29, 2021, or later FAA accepted revision, is a required part of this modification.

2. Installation of Lycoming O-360-A1A, O-360-A1D, O-360-A1F, O-360-A1F6, or O-360-A1P engine in accordance of STC SA302NW, or equivalent FAA approval, is a required part of this modification.

3. Minimum tire size of 8.50-6 installed per STC SA1114NW, or other FAA approval, is a required part of this modification.

4. FAA approved Airplane Flight Manual Supplement, document number BA-8301-3-AFMS, dated July 6, 2021 or later FAA approved revision, is a required part of this modification.

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

Burl’s Aircraft, LLC PO BOX 671487 Chugiak, AK 99567 Original Product Type Certificate Number: A-802

Make: AeroSedan, LLC (Aeronca) Model: 15AC and S15AC

Date of application: September 2, 2020

Date of issuance: July 20, 2021 Date reissued:

August A. Asay Title: Manager, Anchorage ACO Branch

Part 23 of Federal Aviation Regulations.

**14 CFR 21.120)**

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 2 OF 2

Number: SA02552AK

## Every issue (1)

- July 20, 2021: Issued, Current. [certificate](https://openairdocs.org/files/sha256/ef/21/ef217b22f502d8e089cfb92430a74c7245ada5353158b409fdd72adcd4ce7dd9)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
