STC ST00009IB

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate . The STC’s supporting documentation (drawings, inst ructions, specifications, flight manual supplements, etc.) is the property of the ST C holder.

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

Number: ST00009IB

This certificate issued to: Embraer Engineering & Technology Center, USA, Inc.

1400 General Aviation Drive Melbourne, FL 32935

Part 25 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: T00011AT Make: Embraer Model: EMB-135BJ Description of Type Design Change:

Installation of a high speed data system, in accordance with Master Document List Number TR0139, Revision I, dated October 10, 2018, or later FAA approved revisions. This STC was originally issued as a validation of Brazilian CST (STC) No. 2009S07-11, and transferred to a United States based Design Approval Holder (DAH) on October 29, 2019.

1. The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft.

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.

Continued on Page 3

Date of Application: 09/12/2018 Date Reissued: 10/29/2019 Date of Issuance: 11/29/2018 Date Amended:

By Direction of the Administrator Signature

Title: (for) Christina M. Underwood Manager, Atlanta ACO Branch

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

Transfer the ownership of Supplemental Type Certificate Number: ST00009IB

To (Name and address of transferee)

From (Name and address of grantor)

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

STC Number: ST00009IB

Limitations and Conditions: (Continued from Page 1)

3. Instruction for Continued Airworthiness (ICA), document number ICA-001, Revision D, dated October 10, 2018, or later FAA accepted revision is required for this installation.

4. Required markings and placards in the circuit breaker panel, SHED DC BUS 1 Section:

1. In close proximity to the 5 A breaker: “SDU 1”;

2. In close proximity to the 10 A breaker: “HPA/DLNA”;

3. In close proximity to the 5 A breaker: “CAP”

5. A copy of this Certificate shall be maintained as part of the permanent records of the modified aircraft.

6. Prior ANAC and/or FAA accepted or approved versions of the aforementioned documents can be used to sustain existing installations.