STC SA03466CH

Supplemental type certificate · Hartzell Propeller Inc

Holder
Hartzell Propeller Inc · United States
Status
Current · Amended
Status date
June 16, 2016
Applied
April 11, 2014
Product
Aircraft · Small Airplane
Certification basis
Part 21, Part 23, Part 36
Data sheet
TCDSA78EU

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 HC-E5A-3A/NC10245B

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

SA03466CH Hartzell Propeller Inc One Propeller Place Piqua, Ohio 45356 23 A78EU PILATUS AIRCRAFT LTD.

PC-12, PC-12/45, PC-12/47, PC-12/47E up to and including S/N 1575 Installation of Hartzell propeller model HC-E5A-3A/NC10245B in accordance with Hartzell STC Installation Instruction INST_030314 dated May 20, 2015 or later FAA approved revisions. Airplane Flight Manual Supplement AFMS_030314 dated April 1, 2014 or later FAA approved revision is required. Instructions for Continued Airworthiness ICA_030314 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) 4/11/2014 10/23/2015 March 16, 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):

SA03466CH

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

SA03466CH Hartzell Propeller Inc Date of issuance October 23, 2015 Date amended: March 16, 2016

3. Revised Type Certificate Data Sheet information:

Propeller and Propeller Limits:

HARTZELL Constant speed HC-E5A-3A/NC10245B

Diameter: 105 inches, no reduction permitted

Pitch setting at 42-inch radius: Low: 14.7+/-0.1 degrees Feather: 80.0+/-0.5 degrees Reverse: -17.5+/-0.5 degrees

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

6. This STC may be installed on aircraft that have had Finnoff Aviation Products, LLC (FAP) STC SA02266LA previously installed, when used with the following documents:

a) STC Installation Instructions INST_110215 dated November 2, 2015 or later FAA approved revisions;

b) Airplane Flight Manual Supplement AFMS_110215 dated November 2, 2015 or later FAA approved revisions;

c) Instructions for Continued Airworthiness ICA_110215 dated November 2, 2015 or later FAA-accepted revisions.

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 · 4

MakeModelData sheet
Pilatus Aircraft LimitedPC-12A78EU
Pilatus Aircraft LimitedPC-12/45A78EU
Pilatus Aircraft LimitedPC-12/47A78EU
Pilatus Aircraft LimitedPC-12/47EA78EU

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
June 16, 2016Amended, currentCertificate
October 23, 2015Issued, earlier issueCertificate