# STC SA02414CH-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Hartzell Propeller Inc, United States
- Description: Installation of the Hartzell propeller model HC-C2YR-1BFP/F7497 and Hartzell 835-54(P) or A-2295-5(P) spinner.
- Applied: January 10, 2007
- Status date: August 4, 2010
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 2A3](https://openairdocs.org/tcds/2A3)
- Certificate PDF: https://openairdocs.org/files/sha256/9a/ff/9affb9a5641b86f13601d892f298ddded4a6e863b342f5c20e0b2d3d2a393221
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1ECAB55FF8F602A5862577A00071DAD9.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02414CH-D

## ADs that name it (0)

None.

## Approved models (8)

- Mooney Aircraft Corporation M20A ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20B ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20C ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20D ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20E ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20F ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20G ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20J ([TCDS 2A3](https://openairdocs.org/tcds/2A3))

## 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 2A3 for the complete certification basis).

Original Product–Type Certificate Number: 2A3 Make: Mooney Airplane Company, Inc.

Model: M20A, M20B, M20C, M20D, M20E, M20F, M20G, M20J

Installation of the Hartzell propeller model HC-C2YR-1BFP/F7497 and Hartzell 835-54(P), 103585 or A-2295-5(P) spinner in accordance with Hartzell STC Installation Instructions INST_011007 dated July 12, 2007, or later FAA Approved revisions.

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

(Continued….)

STC SA02414CH-D Date of issuance:

July 12, 2007 Date amended:

Hartzell Propeller Inc.

One Propeller Place Piqua, OH 45356-2634 Date of application : January 10, 2007

Date of issuance : July 12, 2007

Date amended : August 4, 2010

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

( Title)

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

August 4, 2010

Limitations and Conditions continued…

2. Airplane Flight Manual Supplement AFMS_011007_1 is required for M20A, M20B, M20C, M20D, and M20G aircraft.

3. Airplane Flight Manual Supplement AFMS_011007_2 is required for M20E and M20F aircraft.

4. Airplane Flight Manual Supplement AFMS_011007_3 is required for M20J aircraft.

5. Instructions for Continued Airworthiness ICA_011007 are applicable.

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

7. 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… Comment [RL1]: Page: 1

## Every issue (2)

- August 4, 2010: Amended, Current. [certificate](https://openairdocs.org/files/sha256/9a/ff/9affb9a5641b86f13601d892f298ddded4a6e863b342f5c20e0b2d3d2a393221)
- July 12, 2007: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/d6/e1/d6e10030dc40c3e0ae997e401b933d92c48e96a550494e12c217f456c7692258)

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