What it approves
Installation of a Cabin Communication System consisting of a Satellite Communications System and an In-Flight Internet System
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
Supplemental Type Certificate Number ST00129MC
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 a Cabin Communication System consisting of a Satellite Communications System and an In- Flight Internet System, in accordance with L-3 Master Drawing List 50056C00525, Revision C, dated July 20, 2015, or later FAA approved revision. FAA approved Instructions for Continued Airworthiness (ICA), L -3 TCS Document No.
50056C00526, Revision A, dated June 17, 2015, or later FAA accepted revisions are a required pa rt of this STC.
This design change is valid only for Cessna 560 airplanes, serial number range 560-0539 through 560-0750 (Citation Ultra Encore).
(Limitations and Conditions continued on page 3 of 3)
Date of Application: January 26, 2015 Date Reissued: May 4, 2023 Date of Issuance: July 20, 2015 Date Amended:
Signature
Title Loyd R. Hamilton ODA-750173-SW Administrator
Supplemental Type Certificate Number ST00129MC
To (Name and address of transferee)
From (Name and address of grantor)
Number: ST00129MC Date of Re-Issuance: May 4, 2023
Limitations and Conditions: (Continued) The installer must determine whether this design change is compatible with previously approved modifications.
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, January 26, 2015, is as shown in TCDS A22CE plus later amendment levels for the following paragraphs:
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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ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Textron Aviation Inc. | 560 | A22CE |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| May 4, 2023 | Reissued, current | Certificate |
| July 20, 2015 | Issued, earlier issue | Certificate |