STC ST9765SC-D

Supplemental Type Certificate Number ST9765SC-D

This certificate issued to: L3Harris Technologies Integrated Systems L.P.

7500 Maehr Road Waco, TX 76705

Part 25 of the Federal Aviation Regulations.

Original Product Make: The Boeing Company Type Certificate Number: A1NM Model: B767-306

The installation of a First-Class Interior in accordance with L-3 Communications Integrated Systems L.P. Drawing List Section 2.1 of Report 33263-00004, Revision A, dated May 1, 2007 or later FAA approved revision and L-3 Airplane Flight Manual Supplement, dated May 1, 2007 or later FAA approved revision.

1. Instructions for Continued Airworthiness (ICA) dated May 1, 2007 or later FAA -approved revision have been accepted by FAA Aircraft Evaluation Group (AEG).

(Limitations and Conditions continued on page 3 of 3)

This certificate and the supp orting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Ad ministrator of the Federal Aviation Administration.

Date of Application: January 11, 2007 Date Reissued: May 4, 2023 Date of Issuance: May 1, 2007 Date Amended: May 9, 2007, January 25, 2011

Signature

Title Loyd R. Hamilton ODA-750173-SW Administrator

Supplemental Type Certificate Number ST9765SC-D

To (Name and address of transferee)

From (Name and address of grantor)

Number: ST9765SC-D Amendment 2 Date of Re-Issuance: May 4, 2023

Limitations and Conditions: (Continued)

2. Descriptive data pertaining to this design change are considered inadequate for duplication in other products.

This approval is limited to only the installation made in the Boeing Model B767-306, Serial Number 30393 aircraft. This STC does not permit manufacturing of parts for multiple installations.

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 Model 767-306 interior installation modification is as follows:

a. The type certification basis for Boeing Model 767-300 series 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, January 11, 2007, is based upon part 25 as amended by Amendment 25- 119. 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 25-119

25.115, 25.119, 25.121, 25.301, 25.303, 25.305, 25.307, 25.321, 25.331, 25.333, 25.337, 25.341, 25.471, 25.561,

25.581, 25.601, 25.605, 25.607, 25.609, 25.611, 25.613, 25.615, 25.619, 25.625, 25.783, 25.785, 25.789, 25.791,

25.793, 25.811, 25.812, 25.813, 25.815, 25.817, 25.851, 25.853, 25.854, 25.855, 25.858, 25.869, 25.981, 25.1301,

25.1307, 25.1309, 25.1355, 25.1357, 25.1411, 25.1415, 25.1419, 25.1421, 25.1423, 25.1431, 25.1433, 25.1438,

25.1441, 25.1443, 25.1445, 25.1449, 25.1529, 25.1541, 25.1561.

Regulations at an intermediate amendment None.

Regulations at the amendment level in TCDS A1NM

25.21, 25.29, 25.111, 25.351, 25.365, 25.571, 25.603, 25.787, 25.803, 25.1351, 25.1353, 25.1435, 25.1439, 25.1447,

25.1557, 25.1581, 25.1583, 25.1585, 25.1587.

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A Type Certificate holder who allows a person to use the Type Certi ficate to manufacture a new aircraft, aircraft engine, or propeller must provide that person with a written licensing agreement acc e ptable to the FAA. (Ref. 14 CFR 21.55).