STC SA01640CH

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA01640CH This certificate issued to: Elliott Aviation Inc.

Quad City Int'I Airport P.O. Box 100 Moline, IL 61266-0100 Part 23 of the Federal Aviation Poegulations. (See Type Certificate Data Sheet A24CE as amended by Special Condition No. 23-115-SC, dated April 2, 2002, Docket No. CE181 for complete certification Basis) Original Product - - Type Certificute Number : A24CE Make: Hawker Beechcraft Corp.

Model: 200, 200C, 200CT, 300, 300L W, B200 B200C, B200CТ, B200T, B300, B300С Description of Type Design Change:

Installation of a Universal Avionics Systems Corp. (UASC) EF1-550 Electronic Flight Instrument System (EFIS) in accordance with Star Aviation Master Data List (MDL) No. R34-0488, Rev. IR, dated January 09, 2009, or later FAA approved revision.

1. FAA Approved Airplane Flight Manual Supplements (AFMS), for the Installation of a UASC EFI-550 EFIS (2 Display Option), Star Aviation Document No. R34-0499, Rev. IR, dated February 02, 2009, or later FAA approved revision, is a required part of this STC.

2. FAA Approved AFMS, for the Installation of a UASC EFI-550 EFIS (4 Display Option), Star Aviation Document No. R34-0500, Rev. IR, dated February 02, 2009, or later FAA approved revision, is a required part of this STC.

(see continuation page)

Date of Application: December 28, 2001 Date Reissued: August 20, 2009 Date of Issuance: May 15, 2002 Date Amended: February 02, 2009 By Direction of the Administrator FEDERAL AVIATIO termed Debates (Signature) Melvin D. Taylor, Manager, TOMNISTRATO Atlanta Aircraft Certification Office (Title)

47.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01640CH Date Reissued: August 20, 2009 September 08, 2008 Date Amended: February 02, 2009 January 27, 2006 August 12, 2003 Limitations and Conditions: (continued):

3. AFMS, Elliott Aviation Report No. FS2006-450, Rev. 1, FAA approved August 2, 2003, or Star Aviation Document No. R34-0499, Rev. IR, dated February 02, 2009 (following STC amendment dated Feb. 02, 2009), or later FAA approved revision, is required onboard aircraft modified in accordance with Configuration (-02) of Star Aviation MDL No. R34-0488, Rev. IR, dated January 09, 2009, or later FAA approved revision.

4. AFMS, Elliott Aviation Report No. FS2006-451, Rev. 1, FAA approved August 2, 2003, or Star Aviation Document No. R34-0500, Rev. IR, dated February 02, 2009 (following STC amendment dated Feb. 02, 2009), or later FAA approved revision, is required onboard aircraft modified in accordance with Configuration (-04) of Star Aviation MDL No. R34-0488, Rev. IR, dated January 09, 2009, or later FAA approved revision.

5. AFMS, Elliott Aviation Report No. FS2006-452, Rev. 1, FAA approved August 2, 2003, or later FAA approved revision, is required onboard aircraft that have the Collins FCS-65H Automatic Flight Control System installed and are modified in accordance with Star Aviation MDL No. R34-0488, Rev. IR, dated January 09, 2009, or later FAA approved revision.

6. AFMS, Elliott Aviation Report No. FS2006-499, Rev. 1, FAA approved January 27, 2007, or later FAA approved revision, is required onboard aircraft modified in accordance with Configuration (-01) of Star Aviation MDL No.

R34-0488, Rev. IR, dated January 09, 2009, or later FAA approved revision.

7. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determine by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that

8. 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.

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