STC SA03352CH

This certificate issued to

Part 23 of the F ederal A viation R egulations . (See Page 3 for complete certification basis)

Original Product --Type Certificate N umber :

Activation of an 802.11 a/b/g and n Wi-Fi System in accordance with Standard Aero Master Data List 1026715. Revision (B), dated April 20, 2015 or later FAA approved revision.

1) The installer must determine whether this design change is compatible with previously approved modifications.

2) FAA Approved Airplane Flight Manual Supplement document number 1026824, Rev (A) dated January 20, 2015, or later FAA approved revision is a required part of this modification.

3) If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.

This certificate and the supporting data, which is the basis for approval, shall remain in ef fect until surrendered, suspended, revoked or a termination date is otherwise established by the A dministrator of the F ederal A viation A dministration.

Elliott Aviation 6601 74th Avenue, Building A Milan, IL 61264

A60CE M ake : Embraer S.A.

M odel : EMB-505 Date of application : May 22, 2014

Date of issuance : June 26, 2015 Date reissued : July 29, 2015

B y direction of the A dministrator Original Signed By:

Manzoor H. Javed for

(Signature) Karol Mordasiewicz Manager, Airframe and Administrative Branch Chicago Aircraft Certification Office

(Title)

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

Supplemental Type Certificate Number: SA03352CH Date of issuance: June 26, 2015 Date of amendment:

Date of reissue: July 29, 2015

Certification Basis (continued)

Based on 14 CFR §§ 21.15, 21.101 and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Embraer S.A. EMB-505 Activation of an 802.11 a/b/g and n Wi-Fi System is as follows:

a. The type certification basis for Embraer S. A. EMB-505 is shown on TCDS A60CE 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 application, May 22, 2014, is based upon TCDS A60CE. 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:

Regulations at the amendment level in TCDS A60CE

23.1(a, b)(23-34), 23.1301(a-d)(23-20), 23.1309(a, b)(23-49), 23.1431(a, c)(23-49), 23.1529(23-26) 23.1581(a, c)(23-50).

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