Supplemental type certificate · Hartzell Propeller Inc

Holder
Hartzell Propeller Inc · United States
Status
Current · Issued
Status date
August 29, 2007
Applied
May 10, 2007
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDSA00009WI

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

What it approves

Installation of the 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 SA02465CH-D This certificate issued to Hartzell Propeller Inc.

One Propeller Place Piqua, OH 45356-2634 Part 23 of the Federal Aviation Regulations.

(See Type Certificate Data Sheet A00009WI for the complete certification basis).

Original Product -Type Certificate Number: A00009WI Make: Hawker Beechcraft Corporation Model: 3000 Description of Type Design Change:

Installation of the Hartzell propeller de-ice components listed in the Limitations and Condition section below in accordance with Hartzell Manual 180 revision 2 dated June 2007, or later FAA Approved revisions.

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

(Continued....)

Date of Application: May May10,2007 Date Reissued:

Date of Issuance: August 29, 2007 Date Amended:

By Direction of the Administrator FEDERAL AVIATIO P3EM (Signature) Brian E. Meyer TOMINISTRATO DAS administrator Hartzell DAS-100082-CE ‹(nite)

FAA PORK 8110-2110-687 PAGE 1 PAGES

United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) STC: SA02465CH-D Date of Issuance: August 29, 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:

4H2271-14 de-ice boots on blades;

3H2360-5 harness;

4H4015-1 slip ring;

1H1150-3 terminal strip;

2H1365 tapped eyelet.

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...

or imprisonment not exceeding 3 vears, or both.

FAA ORM 8110-2-1(10-69) PAGE 3 Of PAGES

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 Corporation3000A00009WI