# STC SA02246CH-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Hartzell Propeller Inc, United States
- Description: Installation of a Hartzell HC-C2YF-1BF/F8468A-2 propeller and C-3568-(P) spinner.
- Applied: April 28, 2005
- Status date: March 13, 2006
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 3A21](https://openairdocs.org/tcds/3A21)
- Certificate PDF: https://openairdocs.org/files/sha256/ac/10/ac10e03a3bf9b223d0fafbe0885fe80704c02a283441764e0c1d9973495d25e8
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F3365A6D9D23D89B8625713400573403.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02246CH-D

## ADs that name it (0)

None.

## Approved models (6)

- The Cessna Aircraft Company 210 ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- The Cessna Aircraft Company 210-5 (205) ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- The Cessna Aircraft Company 210-5A (205A) ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- The Cessna Aircraft Company 210A ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- The Cessna Aircraft Company 210B ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- The Cessna Aircraft Company 210C ([TCDS 3A21](https://openairdocs.org/tcds/3A21))

## 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.

One Propeller Place Piqua, OH 45356-2634

Part 3 of the Civil Air Regulations.

(See Type Certificate Data Sheet 3A21 for the complete certification basis).

Original Product–Type Certificate Number: 3A21 Make: Cessna Aircraft Company Model: 210, 210A, 210B, 210C, 210-5, 210-5A

Installation of a Hartzell HC-C2YF-1BF/F8468A-2 propeller and C-3568-(P) spinner in accordance with Installation Instructions INST_042805 dated April 28, 2005, or later FAA Approved revisions.

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

2. FAA Approved Airplane Flight Manual Supplement, AFMS_042805, dated April 28, 2005, or later FAA approved revision is required.

(Continued….)

Date of application : April 28, 2005

Date of issuance : March 13, 2006 Date reissued :

( Signature) Brian E. Meyer DAS administrator Hartzell DAS-100082-CE

(Title)

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

Limitation and Conditions continued…

3. Installation limited to aircraft equipped with Te ledyne Continental IO-470-E or IO-470-S engines.

4. The following optional governors are approved: Woodward/Ontic models 210657, 210415, and A210680.

(Woodward/Ontic governor models 210345 and 210452 are already approved on the aircraft TC 3A21).

5. This modification did not increase the noise level and wa s not considered an acoustical change as defined in 14 CFR 21.93(b).

6. 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.

…END…

## Every issue (1)

- March 13, 2006: Issued, Current. [certificate](https://openairdocs.org/files/sha256/ac/10/ac10e03a3bf9b223d0fafbe0885fe80704c02a283441764e0c1d9973495d25e8)

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