STC SA00005MC-D

This certificate issued to: L-3Vertex Aerospace 555 Industrial Drive South Madision, MS 39110-9073 Part 23 of the Federal Aviation Regulations.

Original Product - Type Certificate Number: A24CE Make: Beechcraft Corporation Model : A200 (C-12C), A200CT(C-12D) Description of Type Design Change:

Installation of Avionics Systems in accordance with Master Data List, Document Number 34-00-0009-00, Revision 8.0, dated 14, 2009 FAA approved November 24, 2009 or later FAA Approved revision. This STC also allows for the optional capability to couple the co-pilots navigational source selection to the flight management computer in accordance with Master Data List, Document Number ECS-210279, Revision G, dated July 8, 2013, FAA approved July 23, 2013 or later Federal Aviation Administration (FAA) approved revision

1. The i nstal l ati on shoul d not be i ncorporated i n any ai rcraf t unl ess i t i s determi ned that the i nterrel ati onshi p between thi s i nstal l ati on and any previ ousl y approved conf i gurati on wi l l not i ntroduce any adverse ef f ect upon the ai rworthi ness of the ai rcraf t. The compatibility of this modification with the installation of previously installed modifications is the responsibility of the installer.

(See continuation sheets 3 of 4 for additional limitations)

Date of application: October 10, 2005 Date of issuance: October 30, 2006 Date reissued : November 14, 2007

Date amended : November 24, 2009, July 23, 2013

(Signature) Derek Morgan Manager Military Certification Office

Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (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 ) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

Number SA00005MC-D

2. Use of this STC requires the following FAA approved manuals, or later FAA approved revisions:

Table 1: Required Manuals for STC Aircraft Configuration Description Document Number Document Date Document Title 1 Avionics System Installation per MDL Document No. 31-00- 0009-00, Revision 8.0 34-07-0009-00, Revision 2.0 Nov. 20, 2009 Airplane Flight Manual Supplement 34-02-0009-00, Revision 2.0 Oct. 4, 2006 Instructions for Continued Airworthiness of New Avionics Systems installed in the Raytheon A200 King Air (C-12C) Series Aircraft” 2 Avionics System Installation per MDL Document No. 31-00- 0009-00, Revision 8.0 And Optional capability to couple the co-pilots navigational source selection to the flight management computer in accordance with Master Data List, Document Number ECS-210279, Revision G 34-07-0009-00, Revision 2.0 Nov. 20, 2009 Airplane Flight Manual Supplement 34-02-0009-00, Revision 2.0 Oct. 4, 2006 Instructions for Continued Airworthiness of New Avionics Systems installed in the Raytheon A200 King Air (C-12C) Series Aircraft” ECS-210700, Revision -- July 23, 2013 Airplane Flight Manual Supplement ECS-210290, Revision A April 16, 2013 Instructions for Continued Airworthiness CoPilot Primary Flight Display Upgrade Hawker Beechcraft A200/A200CT (C-12C/D) Series Aircraft STC Configuration 2

3. The FAA did not review or approve any military modes/functions of the TA-12S GPS receiver or the IFF portion of the Mode S Transponder.

4. 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 the permission.

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