What it approves
Installation of a Hartzell PHC-C3YF-1RF/F8468A(B,K)-6R constant speed propeller.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may 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…
ADs that name this STC · 1
An AD can apply because an STC is installed, or mention one in its text.