STC SA10339SC

Supplemental type certificate · CenTex Aerospace Inc.

Holder
CenTex Aerospace Inc. · United States
Status
Current · Issued
Status date
October 4, 2004
Applied
October 4, 2004
Product
Aircraft · Single-Engine
Certification basis
Part 1, Part 21, Part 23
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 CenTex Inc. proprietary engine torque indicating system including engine transducer and cockpit indicator in accordance with CenTex Aerospace, Inc. drawing no 008-0000-1000, Rev. A, dated September 2, 2004, or later FAA approved revision. Type design data is contained in CenTex Aerospace, Inc. Master Drawing List 008-0000-0000, Rev. A, dated September 2, 2004 or later FAA approved version. Required instructions for continued airworthiness are contained in CenTex Aerospace, Inc. drawing no 008-0000-1000, Rev. A, dated September 2, 2004, or later FAA approved revision.

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 rNumber SA10339SC This Certificate issued to CenTex Aerospace, Inc.

7805 Karl May Drive Waco, TX 76708-0500

Part 23 of the Federal Aviation Regulations.

Original Product Type Certificate Number : (see attached FAA Approved Model Make : List (AML) approved models Model : and applicable airworthiness regulations)

Description of Type Design Change: Installation of CenTex Inc. proprietary engine torque indicating system including engine transducer and cockpit indicator in accordance with CenTex Aerospace, Inc. drawing no 008-0000- 1000, Rev. A, dated September 2, 2004, or later FAA approved revision. Type design data is contained in CenTex Aerospace, Inc. Master Drawing List 008-0000-0000, Rev. A, dated September 2, 2004 or later FAA approved version.

Required instructions for continued airworthiness are contained in CenTex Aerospace, Inc. drawing no 008-0000-1000, Rev. A, dated September 2, 2004, or later FAA approved revision.

Limitations and Conditions: 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.

Certificate Basis: 14 CFR Part 23 Amendment 23-53

Date of application : September 19, 2003

Date of issuance : October 04, 2004 Date reissued :

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

(Title)

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

FAA APPROVED MODEL LIST (AML)

SA10339SC

Date of issuance: October 4, 2004

CenTex Aircraft Company 7805 Karl May Drive Waco, TX 76708

Item Aircraft Make Aircraft Model Original Type Certificate Number Regulation/ Part 1 Raytheon Aircraft Company 65-90,65-A90 B90, C90, C90A, E90 3A20 FAR 23 2 Raytheon Aircraft Company F90 A31CE FAR 23

FAA Approved:

S . F r a n c e s C o x , M a n a g e r Special Certification Office

Date: October 4, 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 · 6

MakeModelData sheet
Raytheon Aircraft Company65-903A20
Raytheon Aircraft Company65-A903A20
Raytheon Aircraft CompanyB903A20
Raytheon Aircraft CompanyC903A20
Raytheon Aircraft CompanyC90A3A20
Raytheon Aircraft CompanyE903A20