STC SA10364SC

Supplemental type certificate · Blackhawk Modifications Inc.

Holder
Blackhawk Modifications Inc. · United States
Status
Current · Issued
Status date
November 24, 2004
Applied
November 24, 2004
Product
Aircraft · Single-Engine
Certification basis
Part 3, Part 21
Data sheet
TCDS3A20

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of Pratt & Whitney Canada PT6A-135A engines and McCauley 4HFR34C762/94LMA-4 or 4HFR34C768/94LMA-4 propellers in accordance with Blackhawk Modifications, Inc. Drawing No. 19005-01, Rev. IR, dated March 15, 2004, Installation Instructions, or later FAA approved revision. FAA approved AFMS Document No. 19005, Rev. IR, dated November 24, 2004, or later FAA approved revision is required.

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.

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Project Number ST7954SC-A, (PWH) Number SA10364SC This Certificate issued to Blackhawk Modifications, Inc.

a Nevada Corporation 1800 E. Sahara Drive Las Vegas, NV 89108

Part 3 of the Civil Air Regulations.

Original Product Type Certificate Number : 3A20 Make : Raytheon Aircraft Co.

Model : C90; C90A; E90

Description of Type Design Change: Installation of Pratt & Whitney Canada PT6A-135A engines and McCauley 4HFR34C762/94LMA-4 or 4HFR34C768/94LMA-4 propellers in accordance with Blackhawk Modifications, Inc.

Drawing No. 19005-01, Rev. IR, dated March 15, 2004, “Installation Instructions”, or later FAA approved revision.

FAA approved AFMS Document No. 19005, Rev. IR, dated November 24, 2004, or later FAA approved revision is required.

Limitations and Conditions: The shaft horsepower is limited to 550. Each engine mount must be removed from the airplane, cleaned, and Non-Destructive Test (NDT) inspected for fatigue cracks per TP20-00-00 before reinstallation.

Airplanes with less than 500 hours total time are exempt from the NDT inspection of the engine mounts. Compatibility of this design change with previously approved modifications must be determined by the installer. 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.

Date of application : August 6, 2004

Date of issuance : November 24, 2004 Date reissued :

( Signature) S. Frances Cox Manager, Special Certification Office Southwest Region

(Title)

FAA Form 8110-2-1(10-69) Page 2 of 3

FAA Form 8110-2-1(10-69) Page 3 of 3

Number SA10364SC Date of Issuance: November 24, 2004

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 · 3

MakeModelData sheet
Raytheon Aircraft CompanyC903A20
Raytheon Aircraft CompanyC90A3A20
Raytheon Aircraft CompanyE903A20