# STC SA03078CH

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Hartzell Propeller Inc, United States
- Description: Installation of Hartzell HC-(C,I,F)3YR-1(A)RF/F8068(K) or HC-(C,I,F)3YR-1(A)RF/F7693F(K)+2 propeller
- Applied: November 2, 2010
- Status date: May 4, 2012
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS A42EU](https://openairdocs.org/tcds/A42EU)
- Certificate PDF: https://openairdocs.org/files/sha256/5a/f2/5af2838644542b2fb9c6c7976b87756fb4b1a58879a982849413894f918ccf7b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5511728CF4BE411C86257A170068B840.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA03078CH

## ADs that name it (0)

None.

## Approved models (7)

- Cessna Aircraft Company 182S ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182T ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company FR182 ([TCDS A42EU](https://openairdocs.org/tcds/A42EU))
- Cessna Aircraft Company R182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company T182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company T182T ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company TR182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))

## 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 Aircraft Specification 3A13 or A42EU for the complete certification basis).

Original Product–Type Certificate Number: 3A13, A42EU Make: Cessna Aircraft Company Model: R182, FR182, TR182, T182, 182S, 182T, and T182T.

Installation of Hartzell HC-(C,I,F)3YR-1(A)RF/F8068(K) or HC-(C,I,F)3YR-1(A)RF/F7693F(K)+2 propeller in accordance with Installation Instructions H1010-3 Revision IR, dated February 9, 2012, or later FAA approved revisions. See Installation Instructions H1010-3 Revision IR, for specific engine and serial number eligibility.

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

2. FAA Approved Airplane Flight Manual Supplement AFMS H1010- 9 Revision IR, FAA approved May 4, 2012, or later FAA approved revision is required.

3. Instructions for Continued Airworthiness H1010-4 Revision IR, dated February 14, 2012 are applicable.

(Continued….)

STC SA03078CH Date of issuance:

Hartzell Propeller Inc.

One Propeller Place Piqua, OH 45356-2634 Date of application : November 2, 2010

Date of issuance : May 4, 2012

By direction of the Administrator Original Signed By:

Timothy Smyth

( Signature) Timothy Smyth Manager, Propulsion Branch Chicago Aircraft Certification Office

( Title)

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

May 04, 2012

Limitation and Conditions continued…

4. This modification was shown to comply with FAR 36, Appendix G in an FAA approved noise test. The certified take-off noise level for this modification at 3100 lb maximum gross weight is 77.5 dB(a) for airplanes equipped with the Hartzell HC-(C,I,F)3YR-1(A)RF/F8068(K) propeller, or 78.1 dB(a) for airplanes equipped with the Hartzell HC-(C,I,F)3YR-1(A)RF/F7693F(K)+2 propeller. No determination has been made by the Federal Aviation Administration that the noise levels of this airplane are or should be acceptable or unacceptable for operation at, into, or out of, any airport.

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.

…END…

## Every issue (1)

- May 4, 2012: Issued, Current. [certificate](https://openairdocs.org/files/sha256/5a/f2/5af2838644542b2fb9c6c7976b87756fb4b1a58879a982849413894f918ccf7b)

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