STC SA04045CH

Supplemental type certificate · Hartzell Propeller Inc

Holder
Hartzell Propeller Inc · United States
Status
Current · Issued
Status date
January 26, 2016
Applied
April 15, 2015
Product
Aircraft · Small Airplane
Certification basis
Part 21, Part 23, Part 36
Data sheet
TCDSA25SO

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of Hartzell propeller model 5D3-N338A1/78D01B

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.

FAA Form 8110-2 (8/13) Page 1

Part of the Federal A viation Regulations.

Original Product – Type Certificate Number: MDNH:

MRGHO:

Signature

Title

SA04045CH Hartzell Propeller Inc One Propeller Place Piqua, Ohio 45356 23 A25SO PIPER AIRCRAFT, INC.

PA-46-500TP Installation of Hartzell propeller model 5D3-N338A1/78D01B in accordance with Hartzell STC Installation Instruction INST_020215 dated February 15, 2015 or later FAA Approved revisions. Airplane Flight Manual Supplement AFMS_020215 is required. Instructions for Continued Airworthiness ICA_020215 are applicable.

1. The installer must determine whether this change is compatible with previously approved modifications.

2. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

(See Continuation Sheet 3 of 3 pages) 4/15/2015 1/26/2016 Brian E. Meyer STC ODA administrator Hartzell ODA-100082-CE

FAA Form 8110-2 (8/13) Page 2

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

SA04045CH

FAA Form 8110-2 (8/13) Page 3

SA04045CH Hartzell Propeller Inc Date of issuance January 26, 2016

3. Applicability limited to the Pratt & Whitney Canada PT6A-42A engine.

4. Revised Type Certificate Data Sheet information:

Propeller and Propeller Limits:

HARTZELL Constant speed 5D3-N338A1/78D01B

Diameter: 82.5 inches, no reduction permitted

Pitch setting at 30-inch radius: Low: 15.8+/-0.1 degrees Feather: 83.2+/-0.5 degrees Reverse: -11.0+/-0.5 degrees Spinner: Hartzell 105951(P)

5. The original certification basis was used for this STC with the follow exceptions (current amendment levels):

14 CFR 23.907 amendment 23-59 14 CFR Part 36, Appendix G, amendment 36-30

END

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 1

MakeModelData sheet
Piper Aircraft Inc.PA-46-500TPA25SO