STC ST04470AT

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to th e design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

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

Number: ST04470AT This certificate issued to: Janzair Consulting Services, Inc.

4611 S. University Drive, Ste 242 Davie, FL 33328

Part 25of the Federal Aviation Regulations.

Original Product – Type Certificate Number: A16WE Make: Boeing Model: 737-300, 737-400, 737-500, 737-600, 737-700, 737-700C, 737-800 Series Description of Type Design: Installation of the Honeywell TPA-100B Mode S Transponders and Free Flight SBAS Sensor for ADS-B Out Capability in accordance with Janzair Consulting Services Master Drawing List (MDL) No. 737-3499-1901, Rev. B, Dated December 30, 2019, or later FAA approved revision.

Limitations and Conditions: FAA Approved Airplane Flight Manual Supplement (AFMS) to the Model Boeing 737-300, 737-400, 737-500, 737-600, 737-700, 737-700C, and 737-800 Series Aircraft for the Installation of the Dual Honeywell TRA-100B Mode S Transponders and Dual Freeflight SBAS Sensors for ADS-B Out Capability in accordance with JANZAIR Consulting Services Airplane Flight Manual Supplement (AFMS) No. 737-3499-1910, Rev. IR, Dated January 03, 2020, or later FAA approved revision, is a required part of this STC. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. 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. (Limitations and Conditions continued on page 3 of 3.)

Date of Application: July 12, 2019 Date Reissued:

Date of Issuance: January 10, 2020 Date Amended:

Signature Title Christina M. Underwood Manager, Atlanta ACO Branch

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the propert y of the STC holder.

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

Transfer the ownership of Supplemental Type Certificate Number: ST04470AT

To (Name and address of transferee)

From (Name and address of grantor)

The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the propert y of the STC holder.

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

Number: ST04470AT Instructions for Continued Airworthiness (ICA), Janzair Consulting Services Document No. 737-3499-1904, Rev. A, Dated December 30, 2019, or later FAA approved revision, must be made available to the operator at the time of installation.

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 Boeing 737-300, 737-400, 737-500, 737-600, 737-700, 737-700C, and 737-800 Series aircraft is as follows:

a. The type certification basis for Boeing 737-300, 737-400, 737-500, 737-600, 737-700, 737-700C, and 737-800 Series airplane is shown on TCDS A16WE 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, July 12, 2018, is based upon part 25 as amended by Amendment 25-145. 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 latest amendment 25-0 through 25-145 §§ 25.21 §§ 25.301 §§ 25.303 §§ 25.305 §§ 25.307 §§ 25.365 §§ 25.571 §§ 25.601 §§ 25.603 §§ 25.605 §§ 25.607 §§ 25.609 §§ 25.613 §§ 25.625 §§ 25.1301 §§ 25.1309 §§ 25.1322 §§ 25.1351 §§ 25.1357 §§ 25.1431 §§ 25.1529 §§ 25.1581 §§ 25.1583 §§ 25.1585 §§ 25.1587

Regulations at the amendment level in TCDS A16WE §§ 25.1353

Regulations at the latest amendment 21-0 through 21-91 This modification has been determined by the FAA to be a no acoustic change per 14 CFR §21.93(b).

14 CFR Part 26 Regulations Based on 14 CFR §21.101 (g), applicable provisions of 14 CFR Part 26 are included in the certification basis. For a future 14 CFR Part 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections. As of issuance date of this STC, compliance has been found for the following regulations: 14 CFR § 26.11 and 14 CFR § 26.47.

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