STC ST04480AT

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 the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the ST C holder.

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

Number: ST04480AT

This certificate issued to: Telair US, LLC 500-A Gateway Drive Goldsboro, NC 27534

Part 25 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: A16WE Make: Boeing Model: 737-700 Series

Description of Type Design Change: Installation of the Cargo Loading System Modification Kit, P/N 71362-102, in accordance with Master Drawing List, U.S. Cargo Systems Report Number, RPT-3930, Revision 6.0, dated June 9, 2020 or later FAA approved revision.

1. This Cargo Loading System Modification Kit, P/N 71362-102, may only be installed onto a Boeing 737-700 Series aircraft, which has been modified to a freighter aircraft by STC’s ST04479AT Flex-Combi Interior, SA2968SO Main Deck Floor Modification and SA2969SO Main Deck Cargo Door Installation.

2. 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.

(Limitations and Conditions continued on sheet 3 of 3)

Date of Application: February 11, 2020 Date Reissued:

Date of Issuance: July 21, 2020 Date Amended:

Signature

Title (for) Christina M. Underwood, Manager Atlanta Aircraft Certification Office

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Possessi on of this Supplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller.

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

Transfer the ownership of Supplemental Type Certificate Number: ST04480AT

To (Name and address of transferee)

From (Name and address of grantor)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST04480AT

Possessi on of this Supplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller.

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

Date of Issuance: July 21, 2020

3. 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

4. The approval of this modification applies to the above noted airplane model series only.

5. A copy of this STC must be included in the permanent record of the modified aircraft.

6. Maintain in accordance with: FAA Accepted Instructions for Continued Airworthiness (ICA), U.S. Cargo Systems Report, 3931, Rev. 2.0, dated 17 March 2020; or later FAA accepted revisions. These documents must be incorporated into the operator’s maintenance program.

7. Operate in accordance with: FAA Approved PEMCO Airplane Flight Manual Supplement (AFMS) P03-0701, Revision IR, dated 05 May 2020; Weight and Balance, Control and Loading Manual Supplement, Report No.

P03-0700WB, Rev. 2, dated 25 June, 2020; Weight & Balance Manual Supplement, U.S. Cargo Systems Report No. 3967, Rev. 3.0, dated 8 June 2020; or later FAA approved revisions.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101 for significant changes to type design, the certification basis for this change is as follows:

a. The certification basis for parts not changed or not affected by this change is in accordance with Type Certificate Data Sheet, A16WE.

b. The certification basis for parts changed or affected by the change since the reference date of application, November 12, 2018, is based upon part 25 as amended by Amendment 25-145. Based on 14 CFR §§ 21.115 and 21.101, and 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 25-146:

§§25.23, 25.27, 25.301, 25.303, 25.305, 25.307, 25.321, 25.523(b), 25.601, 25.603, 25.605, 25.607, 25.609, 25.613, 25.619,

25.625, 25.793, 25.853, 25.857(e), 25.1301, 25.1519, 25.1529, 25.1583(c)

Regulations at the amendment level in TCDS A16WE:

None

Regulations at an intermediate amendment level:

None

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