Supplemental type certificate · Hartzell Propeller Inc

Holder
Hartzell Propeller Inc · United States
Status
Current · Issued
Status date
February 15, 2008
Applied
November 7, 2007
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21
Data sheet
TCDSA14CE

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 model HC-B4TN-5F/T10173AN(B,K)-12.5.

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: SA02539CH-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 A 14CE for the complete certification basis).

Original Product -Type Certificate Number: A14CE Make: Hawker Beechcraft Corporation Model: B100 Description of Type Design Change:

Installation of the Hartzell propeller model HC-B4TN-SF/T10173AN(B,K)-12.5 in accordance with Hartzell Installation Instructions INST 110707 dated November 7, 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: Nov. 7,2007 Date Reissued:

Date of Issuance: February 15,2008 Date Amended:

By Direction of the Administrator FEDERAL AVIATION 13-25 Signature) Brian E. Meyer TOMINSTRATIO Hartzell DAS-100082-CE DAS administrator (hitle) or imprisonment not exceeding 3 years, or both PAR PORN 8110-2 (10~68) PAGE T DE 3 PANES

United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) STC SA02539CH-D Date of Issuance: February 15, 2008 Limitations and Conditions: continued...

2. Airplane Flight Manual Supplement AFMS_110707 is required.

3. Propellers must be installed as a set (on both engines).

4. Instructions for Continued Airworthiness ICA_110707 is applicable.

5. This modification did not increase the noise level and was not considered an acoustical change as defined in 14 CFR 21.93(b).

6. 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 imprizennent not exceeding 3 years, or both.

FAR FORM B110-2-1(10-69) PACE 3 of 3 pacee

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 CorporationB100A14CE