STC SA11151SC

United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Project Number ST9560SC-A GRT

Number: SA11151SC

This certificate issued to Aerospace Systems, Inc.

1501 Bond St, #14N Little Rock, AR 72202 Part 25 of the Federal Aviation Regulations.

Original Product – Type Certificate Number : 3A15 Make: Beechcraft Corporation Model: 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, H35, G36, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 36, A36, A36TC, B36TC

Installation of an Electromech EM6025 Heat Duct Blower in accordance with Aerospace Systems, Inc. STC Master Document List No. MDL916018-01, Revision 2, dated 09/06/13, or later FAA approved revision.

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.

An Airplane Flight Manual Supplement is not required.

Date of application: August 22, 2011 Date reissued:

Date of issuance: September 30, 2013 Date amended:

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

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):

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA11151SC Issue Date: September 30, 2013

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

Description of Type Design Change (Continued):

(None)

(None)

Certification Basis:

Based on 14 CFR § 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:

23.1 (a)(b) [amdt 23-34]

23.301(a)(b)(c)(d) [amdt 23-48]

23.303 [amdt 23-0]

23.305(a)(b) [amdt 23-45]

23.307(a) [amdt 23-0]

23.321(a)(b) [amdt 23-45]

23.601 [amdt 23-0]

23.603(a)(b) [amdt 23-23]

23.605(a) [amdt 23-23]

23.607(a)(b) [amdt 23-48]

23.609(a)(b) [amdt 23-0]

23.611 [amdt 23-48]

23.613 (a)(b)(c)(d)(e) [amdt 23-45]

23.625(a) [amdt 23-7]

23.777 (a)(b) [amdt 23-51]

23.853(a)(d,3,ii)(f) [amdt 23-49]

23.863(a)(b)(c)(d) [amdt 23-34]

23.1301(a)(b)(c)(d) [amdt 23-20]

23.1309(a1)(a2)(e) [amdt 23-49]

23.1327(a)(b) [amdt 23-20]

23.1351(a1)(a2i)(b1) [amdt 23-49]

23.1357(a)(b)(c) [amdt 23-43]

23.1359(a)(c) [amdt 23-49]

23.1365(a)(b)(d)(e) [amdt 23-49]

23.1367(a)(b)(c)(d) [amdt 23-0]

23.1431(b) [amdt 23-49]

23.1461(a)(b)(c)(d) [amdt 23-49]

23.1529 [amdt 23-26]

END