Supplemental type certificate · Hartzell Propeller Inc

Holder
Hartzell Propeller Inc · United States
Status
Current · Issued
Status date
April 13, 2007
Applied
February 7, 2007
Product
Aircraft · Small Multi-Engine
Certification basis
Part 21
Data sheet
TCDS3A20

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

What it approves

Installation of Hartzell propeller de-ice components.

What the certificate saysOCR

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number SA02408CH-D This certificate issued to Hartzell Propeller Inc.

One Propeller Place Piqua, OH 45356-2634 Part 3 of the CivilAirRegulations.

(See Type Certificate Data Sheet 3A20 for the complete certification basis).

Original Product -Type Certificate Number: 3A20 Make: Raytheon Aircraft Company Model: C90GT Description of Type Design Change:

Installation of the Hartzell propeller de-ice components listed in the Limitations and Conditions section below in accordance with Hartzell Manual 180 Revision 1 dated November 2006, or later FAA Approved revisions.

1. Compatibility of this design change with previously approved modifications must be determined by the installer.

Date of Application: February 7,2007 Date Reissued:

Date of Issuance: April 13,2007 Date Amended:

By Direction of the Administrator FEDERAL AVIATION (Signature) Brian E. Meyer TOMINSTRATO Hartzell DAS-100082-CE DAS administrator (Vale) 47

United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) STC SA02408CH-D Date of Issuance: April 13, 2007 Limitations and Conditions: continued...

2. No Airplane Flight Manual Supplement is required.

3. The following Hartzell propeller de-ice components (part numbers) are approved:

4H2271-10 de-ice boots on blades;

3H2092-4 wire hamess;

4H2674-2 slip ring;

1H1150-3 terminal strips;

2H1365 tapped eyelets.

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

21.93(b).

5. 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...

FAA PORM 8210-2-1 (10-69) ВСЕ З ОЕ З PAGED This certificate may be transferred in accordance with FAR Z1.47.

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
Hawker Beechcraft CorporationC90GT3A20