STC SA10969SC

Supplemental type certificate · Textron Aviation Inc

Holder
Textron Aviation Inc · United States
Status
Current · Issued
Status date
December 1, 2016
Applied
November 19, 2009
Product
Aircraft · Single-Engine
Certification basis
Part 3, 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 upgraded hardware to the Rockwell Collins Pro Line 21 FMS-3000 to provide Localizer Performance with Vertical Guidance (LPV)

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.

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title SA10969SC Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 3 Civil Air Regulations 3 Installation of upgraded hardware to the Rockwell Collins Pro Line 21 FMS-3000 to provide Localizer Performance with Vertical Guidance (LPV) in accordance with master drawing list 338-00-0001, revision IR, dated January 27, 2010, or later approved FAA revision. Airplane flight manual supplement, document 338-00-0014, revision IR, dated February 8, 2010, or later approved FAA revision, is required.

Hawker Beechcraft Corporation C90GTi The installer must determine whether this design change is compatible with previously approved modifications. 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. This installation is limited to airplane serial numbers listed in BHE & Associates document 338-00-0002, revision IR, dated January 21, 2010, or later FAA approved revision.

(see continuation sheet 3 of 3) December 1, 2016 November 19, 2009 February 22, 2010 3A20 Mark Fuller STC ODA administrator ODA-100129-CE

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

FAA Form 8110-2 (5/14) Page 3 of

SA10969SC Date of Issuance: February 22, 2010 Date Reissued: December 1, 2016

Certification Basis:

The Certification Basis for this installation is per Type Certificate Data Sheet 3A20, including the following:

CAR 3 effective May 5, 1956 (Amdt. 3-1, 3-2, 3-8)

3.0, 3.20, 3.292, 3.295, 3.335, 3.381 a, 3.382, 3.384 a, 3.655 a, 3.685, 3.749, 3.750, 3.755 a, 3.777, 3.779

FAR Part 23

23.1301 (Amdt. 23-20)

23.1309 a,b,c,d,e (Amdt. 23-49)

23.1311 (Amdt. 23-49)

23.1321 a, e (Amdt. 23-49)

23.1322 b, c, e (Amdt. 23-43)

23.1357 a,b,c,d (Amdt. 23-43)

23.1359 c (Amdt. 23-49)

23.1365 a,b,d,e (Amdt. 23-49)

23.1367 a,b,c,d (Amdt. Original)

23.1381 (Amdt. Original)

23.1431 a, b (Amdt. 23-49)

23.1529 (Amdt. 23-26)

23.1555 a (Amdt. 23-50)

APPENDIX G (Amdt. 23-37)

Special condition 23-108-SC, "Protection of Systems for High Intensity Radiated Fields (HIRF)"

-- END -- 3

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 CorporationC90GTi3A20

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
December 1, 2016Issued, currentCertificate
February 22, 2010Issued, earlier issueCertificate