STC SA00901DE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00901DE This certificate issued to: Straight Flight, Inc.

13251 E. Control Tower Road Englewood, CO 80112 Part 23 of the Federal Aviation Regulations.

Original Product - Type Certificate Number: A60CE Make: Embraer S. A.

Model: EMB-505 S/N 50500059 Description of Type Design Change:

Installation of up to Two Externally Mounted Gimbal Systems in accordance with Document No. CW0602- 1014, Master Drawing List (MDL), Phenom 300 Gimbal Installations, Revision N/C dated 8/8/2018, FAA approved 9/19/2018 or later FAA approved revision. Instructions for Continued Airworthiness (ICA), Document No. CW0725-1045, Revision IR dated 8/18/2018, FAA Accepted 9/19/2018, or later FAA accepted revision are required to be made available at installation. FAA Approved Airplane Flight Manual Supplement, Document No. CW0715-1099, Revision IR dated 9/11/2018, FAA Approved 9/19/2018, or later FAA approved revision is required for this modification.

1. You cannot use descriptive data about this design change to duplicate other products. This approval is limited to only the installation made in Embraer S. A. EMB-505, S/N 50500059. This STC does not permit manufacturing of parts for multiple installations.

2. Camera/Sensor equipment is not included in this approval. The FAA has not certified the equipment for which these provisions are intended. You must get additional FAA approval to install this equipment. The FAA must evaluate the installation to ensure it complies with the applicable airworthiness standards.

(Certification Basis on page 3 of 3)

Date of Application: April 3, 2018 Date Reissued:

Date of Issuance: September 19, 2018 Date Amended:

By Direction of the Administrator Signature Kreg R. Voorhies Title ODA Administrator, Cert Works ODA(AIR)-833887-NM

FAA Form 8110-2 (5/14) Page 1 of 3

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SA00901DE To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

Signature of grantor: _ Possession of this Supplemental Type permission acceptable to the FAA. (Ref. 14 CFR 21.120).

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

United States of America Department of Transportation Federal Aviation Administration THINISTRAD Supplemental Type Certificate (Continuation Sheet) Number: SA00901DE Date of Issuance: September 19, 2018 Certification Basis:

Based on 14 CPR $§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Embraer S. A. EMB-505 Gimbal installation is as follows:

a. The type certification basis for Embraer S. A. EMB-505 airplane 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, April 3, 2018, is based upon 14 CFR Part 23, effective February 1, 1965 plus Amendments 23-1 through 23-57, plus additional amendment levels as defined per the TCDS. 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 TCDS Certification Basis (Part 23, Amendments 23-1 through 23-57):

14 CFR Sections: 23.49(a)(2,3-6)(b)(c)(2) Amdt. 23-50; 23.57(c)(1),(3)(i) Amdt. 23-50; 23.61(b)(1) Amdt. 23-34; 23.67(c) Amdt. 23-50; 23.77(c) Amdt. 23-50; 23.141 Amdt. 23-45; 23.143 Amdt. 23-50;

23.175(a)(b)(2)(c) Amdt. 23-50; 177(a,b,d) Amdt. 23-50; 23.201 Amdt. 23-50; 23.203 Amdt. 23- 50; 23.207(a-e) Amdt. 23-50; 23.231 (a) Amdt. - ; 23.251 Amdt. 23-45; 23.301 Amdt. 23-48; 23.303 Amdt. - ; 23.305 Amdt. 23-45; 23.307(a) Amdt. - ; 23.337(a)(1)(b)(1) Amdt. 23-48; 23.341(c) Amdt.

23-48; 23.561(a)(b)(3)(e) Amdt. 23-48; 23.571(c) Amdt. 23-48; 23.573(b) Amdt. 23-48; 23.601 Amdt.

- ; 23.603 Amdt. 23-23; 23.605(a Amdt. 23-23; 23.607 Amdt. 23-48; 23.609 Amdt. - ; 23.611 Amdt.

23-48; 23.613 Amdt. 23-45; 23.619 Amdt. 23-7; 23.625(a) Amdt. 23-7; 23.771(a) Amdt. 23-14;

23.773(a)(1,2) Amdt. 23-45; 23.777(a,b) Amdt. 23-33; 23.783(a) Amdt. 23-49; 23.785(b,i) Amdt. 23- 49; 23.807(a)(1) Amdt. 23-49; 23.815(a) Amdt. 23-46; 23.853(a), (d)(3)(ii) Amdt. 23-49; 23.867 Amdt.

23-49; 23.1301(a-c) Amdt. 23-20; 23.1301(a) Amdt. 23-20; 23.1301(d) Amdt. 23-20; 23.1306 Amdt.

23-61; 23.1309(a) Amdt. 23-49; 23. 1309(a)(3) Amdt. 23-49; 23.1309(a,e,f) Amdt. 23-49; 23.1309(a,b) Amdt. 23-49; 23.1351(a),(b)(1)(ii-iii) (2) ) Amdt. 23-49; 23.1351(b)(1)(i) Amdt. 23-49; 23.1357(a-c) Amdt. 23-43; 23.1359(c) Amdt. 23-49; 23.1365(a-e) Amdt. 23-49; 23.1367 Amdt. - ;23.1501 Amdt.

23-21; 23.1505 Amdt. 23-7; 23.1529 Amdt. 23-26; 23.1541(a,b) Amdt. 23-21; 23.1563(a,b) Amdt. 23- 50; 23.1581 Amdt. 23-50; 23.1583(a) Amdt. 23-50; 23.1585(a) Amdt. 23-50; 23.1587(a), (d)(2,6,7)

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