STC ST04526AT

Supplemental type certificate · Archeion Holdings LLC

Holder
Archeion Holdings LLC · United States
Status
Current · Issued
Status date
September 16, 2021
Applied
January 22, 2020
Product
Aircraft · Large Airplane
Certification basis
Part 3, Part 21, Part 25, Part 26
Data sheet
TCDSA46NM

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of Avionica satLINK MAX with optional Personality Module (avPM) in the Cabin Compartment overhead, and optional avRDC MAX QAR in the EE Bay

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.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

ST04526AT Archeion Holdings, LLC.

9941 W. Jessamine Street Miami, FL 33157 Part 25 the Federal Aviation Regulations A46NM Airbus A330-200/-300 series Installation of Avionica satLINK MAX with optional Personality Module (avPM) in the Cabin Compartment overhead, and optional avRDC MAX QAR in the EE Bay in accordance with Master Data List 181640-MDL Rev-D, dated July 30, 2021 or later FAA approved revisions, to provide 2 Iridium SATCOM ATS Voice channels, 1 Iridium SATCOM ATS Datalink FANS 1/A+ Data channel for Flight Deck use (CPDLC at RCP240 & ADS-C at RSP180), & 1 optional AOC Voice channel for cabin crew use...

(See continuation on sheet 3 of 4) “FAA approved Airplane Flight Manual Supplement for Archeion Holdings LLC, 181640-AFMS Revision A, dated September 15, 2021, or later FAA approved revisions, is a required part of this STC.”

(See Continuation Sheet 3 of 4) January 22, 2020 September 16, 2021 (for)Christina Underwood, Manager Atlanta Aircraft Certification Office 4

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

ST04526AT

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

ST04526AT Description of Type Design Change (continued): Existing aircraft systems optional interface/integration include the Flight Deck Audio System (i.e. Pilot Crew Headsets), MCDUs [or IDUs], ATSU ACARS, FDR (Key Event recording), in addition to other Archeion STC installations. In Configuration 1, the satLINK MAX unit is installed with avRDC MAX QAR unit, & the aircraft systems are interfaced with the avRDC MAX QAR unit. In Configuration 2, the satLINK MAX unit is installed as a standalone & provides independent aircraft systems interface.

Limitations and Conditions (continued): “For maintenance and inspections, apply the following Archeion Holdings Instructions for Continued Airworthiness or later FAA accepted revisions, as applicable:

181640-ICA-1, Revision B, dated July 09, 2021, Installation of an Avionica LLC.

satLINK MAX System.

181640-ICA-2, Revision B, dated July 09, 2021, Installation of Avionica satLINK MAX System per MDL section 3.0.

181645-ICA-1, Revision B, dated July 09, 2021, for the fuselage repair after removal of an Avionica LLC. satLINK MAX System Iridium Antenna 181645-ICA-2, Revision B, dated July 09, 2021, for the Removal of the Inmarsat SATCOM System.

This modification has been substantiated to be a no acoustic change per 14 CFR §21.93(b).

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that interrelationship between this change and any other previously approved modifications, including integration to other Archeion STC’s, will produce no adverse effect upon the airworthiness of that airplane. 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.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

ST04526AT 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 Airbus A330-200/-300 Series is as follows:

a. The type certification basis for Airbus A330-200/-300 series airplanes is shown on TCDS A46NM for parts not changed or affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, January 22, 2020 is based upon 14 CFR Part 25 as amended by Amendment 25-145. Based on Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment 25-0 through 25-145 §25.1 (b), Orig. §25.29 (b), Amdt. 25-72 §25.301, Amdt. 25-23 §25.303, Amdt.

25-23 §25.305 (a)(b), Amdt. 25-86 §25.307 (a), Amdt. 25-139 §25.561 (c)(d), Amdt.

25-91 §25.571 (a)(b), Amdt. 25-72 §25.581, Amdt. 25-23 §25.601, Orig. §§25.603, Amdt. 25-46 §25.605 (a), Amdt. 25-46 §25.607, Amdt. 25-23 §25.609, Orig.

§25.611, Amdt. 25-123 §25.613 (a)(b)(c), Amdt. 25-112 §25.631, Amdt. 25-23 §25.771(a), Amdt. 25-4 §25.789 (a), Amdt. 25-46 §25.853 (a), Amdt. 25-116 §25.869 (a)(1,3), Amdt. 25-123 §25.899 (a)(1,3)(b), Amdt. 25-123 §25.981 (a)(3)(d), Amdt. 25-125 §25.1301 (a)(1,2,3,4)(b), Amdt. 25-123 §25.1309 (a)(b)(c)(d)(e)(f), Amdt. 25-123 §25.1322 (e)(1), Amdt. 25-131 §25.1351 (a)(1)(2), Amdt. 25-72 §25.1353 (a)(c), Amdt. 25-123 §25.1357 (a)(c), Amdt. 25-123 §25.1360 (a)(b), Amdt.

25-123 §25.1363 (a)(b), Orig. §25.1381 (a)(b), Amdt. 25-72 §25.1419 (a), Amdt.

25-129 §25.1431 (a)(b)(c)(d), Amdt. 25-113 §25.1529, Amdt. 25-54 §25.1541, Orig.

§25.1581, Amdt. 25-72 §25.1585 (a)(b), Amdt. 25-105

14 CFR Part 26 regulations: Based on 14 CFR § 21.101(g), applicable provisions of 14 CFR Part 26 are included in the certification basis. For any future 14 CFR 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections. As of the issuance date of this STC, compliance has been found for the following regulations: 14 CFR §§ 26.11 (Amdt 26-0), 26.47 (Amdt 26-1).

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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.

No AD in this release names this STC

Approved models · 16

MakeModelData sheet
Airbus SASA330-201A46NM
Airbus SASA330-202A46NM
Airbus SASA330-203A46NM
See all 16 models