STC SA10824SC

United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Project Number SA09666SC-A JEP Number: SA10824SC

This certificate issued to Blackhawk Modifications, Inc.

7601 Karl May Drive Waco, TX 76708-5570 Part 23 of the Federal Aviation Regulations.

Original Product Type Certificate Number : A24CE Make : Hawker Beechcraft Model : 200, 200C, 200T, 200CT, A200, A200C, A200CT, B200, B200C, B200T and B200CT Description of Type Design Change: Installation of Pratt and Whitney Canada PT6A-52 Engines in accordance with master Drawing List Dwg. No. 05210050, revision IR, dated November 15, 2007 or later FAA approved revision. Required Instructions for Continued Airworthiness are contained in Document No. 200708-30.

(See continuation sheet 3 of 3) Limitations and Conditions: 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.

Date of application: December 02, 2007 Date reissued:

Date of issuance: March 21, 2008 Date amended: January 11, 2013

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

(Title)

FAA FORM 8110-2-1(10-69) PAGE 2 of 3 PAGES

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee) (Number and street)

(City, State, and ZIP code)

from (Name of grantor)(Print or type)

(Address of grantor) (Number and street)

(City, State, and ZIP code)

Signature of grantor (In ink):

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA10824SC Date of Issuance: March 21, 2008 Date Amended: January 11, 2013

Description of Type Design Change (Continued): FAA approved Airplane Flight Manual Supplement 200708EG, revision IR, dated May 31, 2008, or later FAA approved revision required for Model B200 and B200C airplanes equipped with Raisbeck Engineering “Epic Gold” Package (includes STCs SA3366NM, SA3831NM, SA3519NM and SA4175NM), and Proline 21 Avionics System.

FAA approved Airplane Flight Manual Supplement 200708EP, revision IR, dated May 31, 2008, or later FAA approved revision required for Model 200, 200C, B200 and B200C airplanes equipped with Raisbeck Engineering “Epic Platinum” Package (includes STCs SA2698NM-S, SA3366NM, SA3831NM, SA3519NM and SA4175NM), and Proline 21 Avionics System.

FAA approved Airplane Flight Manual Supplement 200708NR, revision IR, dated May 31, 2008, or later FAA approved revision required for Model 200, 200C, B200 and B200C airplanes equipped with Proline 21 Avionics System.

FAA approved Airplane Flight Manual Supplement 200708R, revision IR, dated May 31, 2008, or later FAA approved revision required for Model 200, 200C, B200 and B200C airplanes equipped with Raisbeck Engineering Ram Air Recovery System STC SA3366NM, and Proline 21 Avionics System.

FAA approved Airplane Flight Manual Supplement 200708T, revision IR, dated March 07, 2008, or later FAA approved revision required for Model 200T, 200CT, B200T and B200CT airplanes.

FAA approved Airplane Flight Manual Supplement 200708M, revision IR, dated march 07, 2008, or later FAA approved revision required for Model A200 (including Military C-12A and C-12C models), A200C (including Military UC-12B model), A200CT (including Military C-12D, C-12F, FWC-12D, RC-12D, RC-12G, and RC-12H models) and B200C (including Military C-12F and C-12R models) airplanes.

Certification Basis: The certification basis for this STC is the same as for the original certification basis for these model airplanes as defined in TCDS A24CE except for:

14CFR 23 Paragraphs 23.1, 23.29, 23.33, 23.45, 23.49, 23.53, 23.63, 23.69, 23.77, 23.141, 23.143, 23.145, 23.47, 23.161,

23.171, 23.173, 23.175, 23.177, 23.181, 23.201, 23.251, 23.301, 23.303, 23.305, 23.307, 23.337, 23.341, 23.361, 23.363,

23.371, 23.471, 23.473, 23.479, 23.572, 23.601, 23.603, 23.605, 23.627, 23.629, 23.901, 23.903, 23.905, 23.907, 23.925,

23.929, 23.939, 23.951, 23.955, 23.1041, 23.1043, 23.1045, 23.1091, 23.1103, 23.1105, 23.1107, 23.1111, 23.1121, 23.1123,

23.1141, 23.1143, 23.1149, 23.1153, 23.1155, 23.1163, 23.1165, 23.1181, 23.1183, 23.1189, 23.1301, 23.1305, 23.1309,

23.1321, 23.1337, 23.1351, 23.1357, 23.1359, 23.1365, 23.1501, 23.1505, 23.1519, 23.1521, 23.1525, 23.1527, 23.1529,

23.1541, 23.1543, 23.1549, 23.1581, 23.1583, 23.1585, 23.1587, 23.1589 which are amended by Amendment 23-57.

14 CFR 34 Paragraphs 34.1, 34.2, 34.3, 34.5, 34.6, 34.7, 34.10, 34.11 which are amended by Amendment 34-3.

14 CFR 36 Paragraphs 36.1, 36.2, 36.9, 36.501, 36.1501, 36.1581 which are amended by Amendment 36-26.

--END--