# STC SA00719LA

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Hartzell Propeller Inc, United States
- Description: Installation of a Hartzell PHC-C3YF-1RF/F8468A(B,K)-6R constant speed propeller.
- Applied: May 21, 1998
- Status date: May 25, 2005
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15)
- Certificate PDF: https://openairdocs.org/files/sha256/1a/2f/1a2fb71aff5d52345023fc4a290c5448d9c4a3cbdb1f329e3e84affea6b93542
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B51E907A0B4E46DF8625700D0070FE19.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00719LA

## ADs that name it (1)

- [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005. Named in the applicability

## Approved models (2)

- Raytheon Aircraft Company A36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company G33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))

## 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 3A15 for the complete certification basis).

Original Product--Type Certificate Number : 3A15 Make : Raytheon Aircraft Company Model : A36; G36

Installation of a Hartzell PHC-C3YF-1RF/F8468A(B,K)-6R constant speed propeller per HPA36-1, Factory Installation of a Hartzell PHC-C3YF-1RF/F8468A(K)-6R Propeller and A-2295-2(P) Spinner on Raytheon A36, G36 (Bonanza) Aircraft, Revision F, dated April 8, 2005 and HPA36-1A, Instructions for Field Installation of Hartzell PHC-C3YF- 1RF/F8468A(K)-6R Propellers on Raytheon A36, G36 (Bonanza) Aircraft, Revision F, dated April 8, 2005, or later FAA Approved revision.

Installation of March Aviation Co., Supplement No. HPA36-2, Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement to the Raytheon A36, G36 Bonanza POH & FAA Approved AFM, dated December 31, 1998, or later FAA Approved revision, is required as part of this installation.

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

2. FAA Approved Airplane Flight Manual Supplement, HPA36-2, Raytheon A36, G36 Bonanza POH & FAA Approved AFM, Revision A, dated April 6, 2005, or later FAA Approved revision is required.

3. 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.

(Continued….)

Date of application : May 21, 1998

Date of issuance : December 31, 1998 Date reissued : February 5, 1999

Date amended : May 25, 2005

( Signature) Thaddeus D. Krolicki, Jr.

Manager, Propulsion Branch Chicago Aircraft Certification Office

(Title)

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

Number SA00719LA

Limitation and Conditions continued…

Engine: Continental IO-550-B only

Propeller and Propeller Limits: Hartzell PHC-C3YF-1RF/F8468A(B,K)-6R Hub Model: PHC-C3YF-1RF Blade Model: F8468A(B,K)-6R Diameter: 80 inches Maximum 78 inches Minimum

Pitch Setting at 30 inch station:

High: 36.0 ± 1.0 degrees Low: 13.0 ± 0.2 degrees

Spinner: Hartzell A-2295-2(P) Spinner mounting kit A-2476-7

Governor: Woodward D210760 or McCauley C290D3-X/T23

Note: Noise Characteristics: This modification did not increase the noise level of the airplane and was not considered an “acoustical change” as defined in 14 CFR 21.93(b), Amendment 21-75.

…END…

## Every issue (1)

- May 25, 2005: Amended, Current. [certificate](https://openairdocs.org/files/sha256/1a/2f/1a2fb71aff5d52345023fc4a290c5448d9c4a3cbdb1f329e3e84affea6b93542)

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