STC SA02253LA

Supplemental type certificate · Textron Aviation Inc

Holder
Textron Aviation Inc · United States
Status
Current · Reissued
Status date
November 16, 2016
Applied
December 21, 2007
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21, Part 36
Data sheet
TCDSA24CE

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

What it approves

Installation of non-powered belly mounted radar equipment.

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 Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 3 SA02253LA Federal Aviation Regulations.

23* * Certification basis set forth in Type Certificate Data Sheet A24CE.

B300, B300C

Installation of non-powered belly mounted radar equipment in accordance with Master Data List 300E368671 Revision 7, dated April 9, 2009, or later FAA approved revision and FAA Approved Flight Manual Supplement, Document No.

130-590031-327, dated September 14, 2009, for the 16,500 lb MTOW configuration; or Document No. 130-590031-341, dated March 19, 2010, for the 15,000 lb MTOW configuration, or later FAA approved revisions.

(see continuation sheet 3 of 3) Hawker Beechcraft December 21, 2007 September 14, 2009 A24CE April 30, 2010; September 23, 2013;

November 16, 2016 March 26, 2010 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

Date of Issuance: September 14, 2009 Date Reissued: November 16, 2016 Date Amended: March 26, 2010

Limitations and Condition (continued):

This STC is applicable to B300 and B300C models with both 15,000 lb. MTOW and 16,500 lb. MTOW, which have Hawker Beechcraft Martime Patrol Aircraft modifications consisting of dual ventral fins, and a larger rudder. For the 16,500 lb. MTOW airplanes, the modifications also include heavy weight landing gear, and extended range fuel tanks. Noise compliance was found to Title 14 CFR part 36, Appendix G, Amendment 36-1 thru 36-24. The installation should not be incorporated into any other aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The approval of this modification applies to the above noted airplane model series only. 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 -- SA02253LA 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 · 2

MakeModelData sheet
Hawker Beechcraft CorporationB300A24CE
Hawker Beechcraft CorporationB300CA24CE

Every issue · 5

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

DateStatusFiles
November 16, 2016Reissued, currentCertificate
September 23, 2013Reissued, earlier issueCertificate
September 23, 2013Amended, earlier issueCertificate
March 26, 2010Amended, earlier issueCertificate
September 14, 2009Issued, earlier issueCertificate