STC ST04460AT

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 property of the ST C holder.

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

Number: ST04460AT

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: A1NM Make: Boeing Model: 767-300 Series

Description of Type Design Change: Installation of the Main Deck Cargo Loading System in accordance with B767-300 BCF Master Drawing List for 69000-Series Cargo Handling System, U.S. Cargo Systems Report Number RPT-3890, Revision 3.0, dated July 10, 2019 or later FAA approved revision.

Limitations and Conditions: 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. Type Certificate (TC), A1NM with FAA approved Boeing Service Bulletin 767-00-0039 must be installed in conjunction with this installation. A copy of this STC must be included in the permanent records of the modified aircraft.

(Limitations and Conditions continued on sheet 3 of 3)

Date of Application: November 12, 2018 Date Reissued:

Date of Issuance: September 19, 2019 Date Amended:

Signature

Title Christina M. Underwood, Manager Atlanta Aircraft Certification Office

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 th e property of the STC holder.

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

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: ST04460AT

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 th e property of the STC holder.

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

Date of Issuance: September 19, 2019 Date Amended:

Aircraft must be loaded, with this cargo loading system installed, in accordance with the B767-300 BCF P/N 69000-Series MDCLS Weight & Balance Manual Supplement, U.S. Cargo Systems Report Number RPT-3919, Revision 1.0, dated September 16, 2019 or later FAA approved revision, in conjunction with the previously approved weight and balance or cargo loading instructions for this aircraft. B767-300BCF Main Deck Cargo Loading System 69000 Series Instructions for Continued Airworthiness (ICA), U.S. Cargo Systems Report, RPT-3871, Revision 3.0, dated September 18, 2019 or later FAA accepted revision must be made available to the operator at the time of installation. 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.

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 767-300 series main deck cargo loading system is as follows:

a. The type certification basis for Boeing Model 767-300 airplanes is shown on TCDS A1NM 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, 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 25-145:

§§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(a)(b),

25.619, 25.621, 25.625, 25.793, 25.853, 25.857(e), 25.1301, 25.1519, 25.1529, 25.1541, 25.1557, 25.1583(c)

Regulations at the amendment level in TCDS A1NM:

None

Regulations at an intermediate amendment level:

None

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