STC ST00116MC

Supplemental Type Certificate Number ST00116MC

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: Cessna Type Certificate Number: A22CE Model: 560

Installation of an Avionics Upgrade consisting of a Data-Link System, a High Frequency Radio System, and a Tactical Air Navigation System, in accordance with L-3 TCS Master Drawing List 8794-500-10702, Revision C, dated August 26, 2014, or later FAA approved revision.

This design change is valid only for Cessna 560 airplanes, serial number range 560-0260 through 560-0538 (Citation Ultra) and 560-0539 through 560-0750 (Citation Ultra Encore) as stated in the applicable AFMS.

(Limitations and Conditions continued on page 3 of 4)

Date of Application: December 9, 2013 Date Reissued: May 4, 2023 Date of Issuance: August 26, 2014 Date Amended:

Signature

Title Loyd R. Hamilton ODA-750173-SW Administrator

Supplemental Type Certificate Number ST00116MC

To (Name and address of transferee)

From (Name and address of grantor)

Number: ST00116MC Date of Re-Issuance: May 4, 2023 Limitations and Conditions: (Continued) The Data-Link, HF Radio, and/or TACAN may be installed individually or in any combination.

FAA Approved Airplane Flight Manual Supplements:

L-3 TCS Document No. 8794-500-10705, Revision B, approved August 26, 2014 (Data-Link), L-3 TCS Document No. 8794-500-10703, Revision B, approved August 26, 2014 (HF Radio), L-3 TCS Document No. 8794-500-10707, Revision C, approved August 26, 2014 (TACAN), or later FAA approved revisions are a required part of this STC when the applicable item is installed.

FAA Approved Instructions for Continued Airworthiness (ICA):

L-3 TCS Document No. 8794-500-10706, Revision B, dated August 26, 2014 (Data Link), L-3 TCS Document No. 8794-500-10704, Revision C, dated August 26, 2014 (HF Radio), L-3 TCS Document No. 8794-500-10708, Revision B, dated August 26, 2014 (TACAN), or later FAA accepted revisions are a required part of this STC when the applicable item is installed.

The installer must determine whether this design change is compatible with previously approved modifications. This STC is compatible with West Star Aviation, Inc. STC Number ST02568CH, issued May 23, 2008.

If the holder agrees to permit another person to use this certificate to alter a 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 560 series airplane is as follows:

a. The type certification basis for 560 series airplanes is shown on TCDS A22CE 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, December 9, 2013, is as shown in TCDS A22CE plus later amendment levels for the following paragraphs:

(Certification Basis continued on page 4 of 4)

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).

Number: ST00116MC Date of Re-Issuance: May 4, 2023 Certification Basis: (Continued)

Regulations at the latest amendment 25-0 through 25-137

25.301, 25.303, 25.305, 25.307, 25.341, 25.571, 25.581, 25.601, 25.603, 25.605, 25.607, 25.609, 25.613, 25.619, 25.625,

25.771, 25.773, 25.777, 25.789, 25.853, 25.1307, 25.1316, 25.1323, 25.1325, 25.1327, 25.1331, 25.1333, 25.1351,

25.1381, 25.1431, 25.1501, 25.1523, 25.1529, 25.1581, 25.1585, and 25.1587.

Regulations at an intermediate amendment

25.869 at Amdt. 25-113; 25.981 at Amdt. 25-102; and 25.1353 at Amdt. 25-113.

Regulations at the amendment level in TCDS A22CE

25.611, 25.1301, 25.1309, 25.1322, and 25.1357.

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