# STC SA5533NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Hartzell Propeller Inc, United States
- Description: Installation of Hartzell PHC-J3YF-2UF/FC7663(B,K)-2R propellers and C-3567-1(P) or C-3567-4(P) spinners.
- Applied: January 22, 1991
- Status date: May 25, 2005
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 3A16](https://openairdocs.org/tcds/3A16)
- Certificate PDF: https://openairdocs.org/files/sha256/48/bf/48bf68ee312d686956a19da49602edd323d5c172e0fdcfa6d94898db8292b3df
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E95027461EB1C6538625700D00713328.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA5533NM

## ADs that name it (0)

None.

## Approved models (2)

- Raytheon Aircraft Company 58 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Raytheon Aircraft Company 58A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))

## 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 3A16 for the complete certification basis).

Original Product--Type Certificate Number : 3A16 Make :

Raytheon Aircraft Company 58; 58A; G58

Installation of a Hartzell PHC-J3YF-2UF/FC7663(B,K)-2R propellers and C3567-1(P) or C-3567-4(P) spinner in accordance with Factory Installation HPBE58-1, Revision H, dated April 7, 2005, or Field Installation Instructions HPBE58-1A, Revision H, dated April 8, 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, HPBE58-2, for Raytheon 58, 58A and G58 Baron Airplane, Revision A, dated April 6, 2005, or later FAA approved revision is required.

3. Installation limited to aircraft equipped with Teledyne Continental IO-550-C engines.

(Continued….)

Date of application : January 22, 1991

Date of issuance : March 5, 1992 Date reissued : November 6, 1992

Date amended : November 24, 1998, 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

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

Number SA5533NM

Limitation and Conditions continued…

4. Propellers must be installed as a set.

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)

- May 25, 2005: Amended, Current. [certificate](https://openairdocs.org/files/sha256/48/bf/48bf68ee312d686956a19da49602edd323d5c172e0fdcfa6d94898db8292b3df)

---
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.
