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.
Approved models · 2
Every issue · 5
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| November 16, 2016 | Reissued, current | Certificate |
| September 23, 2013 | Reissued, earlier issue | Certificate |
| September 23, 2013 | Amended, earlier issue | Certificate |
| March 26, 2010 | Amended, earlier issue | Certificate |
| September 14, 2009 | Issued, earlier issue | Certificate |