STC SA01782WI

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47.

FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:

Part of the

Signature

Title 3 SA01782WI 3S Certification, LLC.

8200 E. 34th St. North, Suite 1207 Wichita, KS 67226 Federal Aviation Regulations.23 Installation of Activation of WLAN Provisions and Transmitting Portable Electronic Devices (T-PED)Tolerance Testing.

Data required includes:

1) 3S Certification, LLC. Master Data List (MDL) 3S13-373-1001, Revision IR, Dated: 05/30/2015 or later FAA approved revision. 2) 3S Certification, LLC. Aircraft Flight Manual Supplement (AFMS) 3S13-373-7101, Revision IR, Dated:

05/30/2015 or later FAA approved revision. 3) 3S Certification, LLC. Instructions for Continued Airworthiness (ICA) 3S13-373-6101, Revision 2.0, Dated: 05/07/2015 or later FAA accepted revisions.

1) Compatibility of this design change with previously approved modifications must be determined by the installer.

2) 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.

3) Approval of this change in type design applies to the above model of airplane only.

4) A copy of this certificate and the ICA shall be maintained in the airplane permanent records.

Steve K. Simpson ODA administrator ODA(AIR)-833355-CE Beechcraft Corporation C90GTi 11/21/2014 05/30/2015 3A20

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47.

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47.

FAA Form 8110-2 (5/14) Page 3 of

3 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 the Beechcraft Corporation King Air Model C90GTi Activation of WLAN Provisions and Transmitting Portable Electronic Devices (T-PED)Tolerance Testing is as follows:

a) The type certification basis for the Beechcraft Corporation King Air Model C90GTi is shown on A24CE for parts not changed or not affected by the change.

b) The certification basis for parts changed or affected by the change since the reference date of the application, 11/21/2014, is based upon 14 CFR Part 23 as amended by Amendment 23-62. Based on 14 CFR 21.115 and § 21.101, and the FAA policy for significant changes in the FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment 23-0 through 23-62

23.601 [Amdt. Original], 23.603 [Amdt. 23-23], 23.609(a) [Amdt. Original], 23.771(a) [Amdt. 23-14], 23.773(a)(1)(2) [Amdt. 23-45],

23.777(a)(b) [Amdt. 23-62], 23.853(a) [Amdt. 23-62], 23.1301(a)(b)(c) [Amdt. 23-62], 23.1309(a) [Amdt. 23-62], 23.1322(c)(d)(e) [Amdt. 23-43], 23.1359(a)(c) [Amdt. 23-49], 23.1365(a)(b)(d)(e) [Amdt. 23-49], 23.1367(c)(d) [Amdt. Original], 23.1381(a)(b)(c) [Amdt. Original], 23.1431(a)(b) [Amdt. 23-62], 23.1501 [Amdt. 23-21], 23.1529 [Amdt. 23-26], 23.1581(a)(2)(b)(1)(3)(f) [Amdt.

23-50], 23.1585(j) [Amdt. 23-62] Regulations at the amendment level in TCDS 3A20

- None - Regulations at an intermediate amendment

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