STC SA01525WI

This certificate issued to: 3S Certification, LLC.

8200 E 34th St. N.

Building 1200, Suite 1207 Wichita, KS 67226

Part 23 of the F ederal A viation R egulations .

(See Type Certificate Data Sheet A24CE and Page 3 of 3 Continuation Sheet.)

Original Product - Type Certificate N umber : A24CE M ake : Hawker Beechcraft Corporation M odel : 200, 200C, 200T, 200CT, B200, B200C, B200CT, B200T, B200GT, B200CGT, 300, 300LW, B300, B300C

Description of Type Design Change: Installation of AirLock Secure Entry System door lock system in place of original equipment locks for the main cabin door, nose avionics doors, and aft equipment door. Data Required: Hawker Beechcraft Services Master Data List for the Installation of the AirLock Secure Entry System, Document Number 007-5200-L01-00, Revision 1.0, dated December 9, 2008; 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.

Date reissued : February 9, 2010, June 30, 2014

B y direction of the A dministrator

(Signature) Steve K. Simpson ODA administrator ODA(AIR)-833355-CE (Title)

Date of application : December 12, 2007 Date of issuance : December 17, 2008

Date of Issuance: December 18, 2008 Date Reissued: February 9, 2010 June 30, 2014

Certification Basis Model 200, 200C, 200T, 200CT, B200, B200C, B200CT, B200T, B200GT, B200CGT: In addition to the requirements as shown in Type Certificate A24CE, with respect to the modifications of this STC, the applicant has voluntarily complied with later amendments of some regulations. For this STC, the applicant has complied with the following Sections of the Federal Aviation Regulations, Part 23, effective February 1, 1965, as amended by Amendments stated as follows: 23.301 (Amdt.Original); 23.303 (Amdt. Original); 23.305 (Amdt. Original); 23.307 (Amdt. Original); 23.601 (Amdt. Original) 23.603 (Amdt.Original); 23.611 (Amdt. 23-7); 23.613 (Amdt. Original);

23.783 (Amdt. Original); 23.1301(a)(b) (Amdt. 23-7); 23.1309(a)(b (Amdt. 23-14); 23.1431 (Amdt. Original); 23.1529 (Amdt 23-26).

Certification Basis Model 300, 300LW, B300, B300C: In addition to the requirements as shown in Type Certificate A24CE, with respect to the modifications of this STC, the applicant has voluntarily complied with later amendments of some regulations. For this STC, the applicant has complied with the following Sections of the Federal Aviation Regulations, Part 23, effective February 1,1965, as amended by Amendments stated as follows: 23.301 (Amdt. 23-28);

23.303 (Amdt. Original); 23.305 (Amdt. Original);23.307 (Amdt. Original); 23.601 (Amdt. Original) 23.603 (Amdt.

23-23); 23.611 (Amdt. 23-7); 23.613 (Amdt. 23-23); 23.783 (Amdt. 23-34); 23.1301(a)(b)(c)(d) (Amdt. 23-20);

23.1309(a)(b) (Amdt. 23-34); 23.1431 (Amdt. Original); 23.1529 (Amdt 23-26).

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