# STC SA02319CH-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Hartzell Propeller Inc, United States
- Description: Installation of a Hartzell HC-J3YF-1RF/F7691+2 propeller and C-4582-(P) spinner.
- Applied: April 29, 2005
- Status date: February 6, 2009
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21, Part 23
- Data sheets: [TCDS 3A21](https://openairdocs.org/tcds/3A21)
- Certificate PDF: https://openairdocs.org/files/sha256/f8/79/f879404a5ebe1634186191f8a44a6a017216df5dfac354ca2b4b2395fbb11f9f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EA4FEE672B2B471B862575660058EA35.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02319CH-D

## ADs that name it (0)

None.

## Approved models (10)

- Cessna Aircraft Company 210F ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210G ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210H ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210J ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210F ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210G ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210H ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210J ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210K ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210L ([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.

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: 210F, 210G, 210H, 210J, T210F, T210G, T210H, T210J, T210K, T210L

Installation of a Hartzell HC-J3YF-1RF/F7691+2 propeller or HC-J3YF-1RF/F7691B+2 propeller in accordance with Installation Instructions INST_050205 dated May 2, 2005, or later FAA Approved revisions.

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

(Continued….)

STC SA02319CH-D Amended February 6, 2009 Limitation and Conditions continued… Hartzell Propeller Inc.

One Propeller Place Piqua, OH 45356-2634 Date of application : April 29, 2005

Date of issuance : September 21, 2006

Date amended : July 3, 2007, February 6 , 2009

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

( Title)

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

2. FAA Approved Airplane Flight Manual Supplement, AFMS_050205, dated May 2, 2005, or later FAA approved revision is required.

3. Installation limited to aircraft equipped with Teledyne Continental IO-520-A, IO-520-J, TSIO-520-C or TSIO-520- H engines.

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

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.

6. Instructions for Continued Airworthiness ICA_050205 are applicable.

Certification Basis: No change from original CAR 3 requirements as described in Type Certificate Data Sheet 3A21, plus 14 CFR 23.1529

…END…

## Every issue (2)

- February 6, 2009: Amended, Current. [certificate](https://openairdocs.org/files/sha256/f8/79/f879404a5ebe1634186191f8a44a6a017216df5dfac354ca2b4b2395fbb11f9f)
- July 3, 2007: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/08/74/0874657254ec0a4b7ed79d4b0df4104027c5924e7e4bd830b528141a1b2d3260)

---
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.