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United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate _____________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. _____________________________________________________________________________________________________________________________________ FAA Form 8110-2(10-68) Page 1 of 3 This certificate may be transferred in accordance with FAR 21.47. Number SA10747SC This Certificate issued to certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirements of Part 23 of the Federal Aviation Regulations. Original Product Type Certificate Number : Description of Type Design Change: Increase gross weight in accordance with Drawing No. 030-0000-0000, Rev. G, or later FAA approved revision. Required Instructions for Continued Airworthiness is contained in Drawing No. 030-0000-1000, Rev. G, or later FAA approved revision. Required Airplane Flight Manual Supplement is contained in Drawing No. 030-0000-1000, Rev.G, or later FAA approved revision. 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. (See continuation sheet 3 of 3) This certificate and the supporting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Hawker Beechcraft Corporation 9709 E. Central Avenue Wichita, KS 67201 3A20 Make : Hawker Beechcraft Corporation Model : C90; C90A; C90GT; C90GTi; E90; 65-A90-1; and 65-A90-4 Date of application: March 03, 2007 Date of issuance: November 20, 2007 Date reissued: November 10, 2009 Date amended: July 21, 2008; January 07, 2009; October 06, 2009 By direction of the Administrator _______________________________________________________ (Signature) S. Frances Cox Manager, Special Certification Office Southwest Region _______________________________________________________ (Title)

SA10747SC REV 3 Reissue Transfer 11-10-09 (1)

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Page 1: SA10747SC REV 3 Reissue Transfer 11-10-09 (1)

United States Of America

Department of Transportation - Federal Aviation Administration

Supplemental Type Certificate

_____________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. _____________________________________________________________________________________________________________________________________ FAA Form 8110-2(10-68) Page 1 of 3 This certificate may be transferred in accordance with FAR 21.47.

Number SA10747SC

This Certificate issued to

certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirements of Part 23 of the Federal Aviation Regulations. Original Product Type Certificate Number : Description of Type Design Change: Increase gross weight in accordance with Drawing No. 030-0000-0000, Rev. G, or later FAA approved revision. Required Instructions for Continued Airworthiness is contained in Drawing No. 030-0000-1000, Rev. G, or later FAA approved revision. Required Airplane Flight Manual Supplement is contained in Drawing No. 030-0000-1000, Rev.G, or later FAA approved revision. 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.

(See continuation sheet 3 of 3)

This certificate and the supporting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Hawker Beechcraft Corporation 9709 E. Central Avenue Wichita, KS 67201

3A20

Make : Hawker Beechcraft Corporation

Model : C90; C90A; C90GT; C90GTi; E90; 65-A90-1; and 65-A90-4

Date of application: March 03, 2007 Date of issuance: November 20, 2007

Date reissued: November 10, 2009 Date amended: July 21, 2008; January 07, 2009; October 06, 2009 By direction of the Administrator _______________________________________________________ (Signature) S. Frances Cox Manager, Special Certification Office Southwest Region _______________________________________________________

(Title)

Page 2: SA10747SC REV 3 Reissue Transfer 11-10-09 (1)

United States Of America

Department of Transportation - Federal Aviation Administration

Supplemental Type Certificate(Continuation Sheet)

___________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. ___________________________________________________________________________________________________________________________________ FAA Form 8110-2-1(10-69) Page 2 of 3 This certificate may be transferred in accordance with FAR 21.47.

Page 3: SA10747SC REV 3 Reissue Transfer 11-10-09 (1)

United States Of America

Department of Transportation - Federal Aviation Administration

Supplemental Type Certificate(Continuation Sheet)

___________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. ___________________________________________________________________________________________________________________________________ FAA Form 8110-2-1(10-69) Page 3 of 3 This certificate may be transferred in accordance with FAR 21.47.

Number SA10747SC

Date of Reissuance: November 10, 2009 Date Amended: October 06, 2009

Certification Basis: 14 CFR part 23 sections 23.1, 23.3, 23.21, 23.23, 23.25, 23.45, 23.49, 23.51, 23.53, 23.63, 23.65, 23.66, 23.67, 23.69, 23.73, 23.75, 23.77, 23.141, 23.143, 23.145(a)(b)(4), 23.161, 23.171, 23.173, 23.175, 23.181(a)(b), 23.335(a)(b)(c), 23.337, 23.343(a)(b), 23.471, 23.473, 23.477, 23.479(a)(2)(b), 23.481(a)(2)(b), 23.483, 23.485, 23.493, 23.499(a)(b)(c), 23.507, 23.509, 23.723, 23.725, 23.727, 23.731, 23.733(a)(b)(c), 23.735(b), 23.907, 23.1041, 23.1043, 23.1045, 23.1507, 23.1519, 23.1563, 23.1581, 23.1583, 23.1585, 23.1587 all to Amendment 23-55. 14 CFR part 36, all to Amendment 36-26. --END--