STC SA02181AK

Supplemental type certificate · Hartzell Propeller Inc

Holder
Hartzell Propeller Inc · United States
Status
Current · Amended
Status date
June 29, 2016
Applied
May 16, 2000
Product
Aircraft · Small Airplane
Certification basis
Part 21
Data sheet
TCDSA37CE

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-B3TN-3AF(Y)/T10890CN-2, HC-B3TN-3AF(Y)/T10890CNK-2, and HC-B3TN-3AF(Y)/T10890CNB-2 three-bladed propeller assembly

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

SA02181AK Hartzell Propeller Inc.

One Propeller Place Piqua, Ohio 45356 23 A37CE Textron Aviation Inc.

208; 208A; 208B Installation of Hartzell propeller model HC-B3TN-3AF(Y)/T10890CN-2, HC-B3TN-3AF(Y)/T10890CNK-2, and HC-B3TN-3AF(Y)/T10890CNB-2 three-bladed propeller assembly in accordance with Descriptive Data List No. 208-3BP-DL dated October 10, 2001, or later FAA approved revision.

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) 5/16/2000 10/16/2001 November 8, 2001 September 11, 2003 June 29, 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):

SA02181AK

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

SA02181AK Hartzell Propeller Inc Date of amendment June 29, 2016

3. Airplane Flight Manual Supplement, document number 208-3BP-AFMS dated October 17, 2001, or later FAA approved revision is required.

4. Maintenance Manual Supplement, document number 208-3BP-MMS dated May 12, 2000, or later FAA approved revision is required.

5. This modification did not increase the propeller noise level and was not considered an acoustical change as defined in 14 CFR

21.93(b).

6. Limited to aircraft equipped with PT6A-114 and PT6A-114A engines only.

7. Revised Type Certificate Data Sheet information:

Propeller and Propeller Limits:

Hartzell aluminum three-bladed, constant speed, full feathering, reversible Models: HC-B3TN-3AF(Y)/T10890CN-2 (No propeller ice protection) HC-B3TN-3AF(Y)/T10890CNK-2 (Electric de-ice system on propeller) HC-B3TN-3AF(Y)/T10890CNB-2 (Fluid anti-ice system on propeller)

Diameter: 106 inches maximum, 104 inches minimum

Pitch setting at 42-inch radius: Low: 8.0+/-0.2 degrees Feather: 79.0+/-1.0 degrees Reverse: -21.0+/-0.5 degrees Start-lock: -3.2+/-1.0 degrees (if installed)

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 · 2

MakeModelData sheet
Textron Aviation Inc.208A37CE
Textron Aviation Inc.208BA37CE