What it approves
Installation of Hughes Satellite Connectivity and Wifi Cabin Distribution System
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST04812NY This certificate issued to: ALOFT AeroArchitects 21652 Nanticoke Avenue Georgetown, DE 19947 25 of Federal Aviation Regulations.
Original Product Type Certificate Number: A21EA-1 Make: MHI RJ Aviation ULC Description of Type Design Change: Model: See Continuation Sheet 04
1. Installation of Hughes Satellite Connectivity and Wifi Cabin Distribution System on MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700, 701 & 702) and CL-600-2D24 (Regional Jet Series 900) Aircraft per AmphenolCIT Master Data List No. 900-111604 Rev NC, or later FAA approved revision. See continuation sheets 02 through 05.
1. The installer must determine whether this design is compatable with previously approved modifications.
See continuation sheets 02 through 05.
Date of Application: 05/31/2023 Date Reissued: 12/08/2025 Date of Issuance: 02/25/2025 Date Amended:
Title: Dan Skibinski STC Administrator, ODA-955292-NE Possession of this Supplemental Type permission acceptable to the FAA. (Ref. 14 CFR 21.120).
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST04812NY Effective Date: 12/08/2025
TransferEndorsement Transfer the ownership of Supplemental Type Certificate Number:
To (Name and address of transferce):
From (Name and address of grantor);
Possession of this Supplemental Type permission acceptable to the FAA. (Ref. 14 CFR 21.120).
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST04812NY Effective Date: 12/08/2025 Description of Type Design Change: (Continued)
2. ICA: Comply with ALOFT AeroArchitects Instructions for Continued Airworthiness (ICA), documents, or later FAA-accepted revisions:
Configuration 1/2: TM-8487-ICAW-01, revision 003, dated February 10, 2025 Configuration 3/4/5: TM-8487-ICAW-02, revision 001, dated January 03, 2025
3. ALS: Comply with the FAA-Approved Airworthiness Limitations Sections (ALS) in documents:
Configuration 1/2: TM-8487-ICAW-01, revision 003, dated February 10, 2025 with Appendix A revision 002, dated November 07, 2024, FAA-Approved December 02, 2024.
Configuration 3/4/5: None.
3. EWIS ICA: The FAA has reviewed the applicant's assessment of existing Electrical Wiring Interconnection System Instructions for Continued Airworthiness (EWIS ICA) and found that additional EWIS ICA tasks are required:
Configuration 1/2: TM-8487-EWIS-01, revision 002, dated November 07, 2024, FAA-Approved February 25, 2025.
Configuration 3/4/5: None.
4. AFMS: Comply with the FAA-Approved ALOFT AeroArchitects Airplane Flight Manual Supplement (AFMS), documents:
Configuration 1/2/3/4/5: AFMS-8487-P342-001, revision 002, dated January 15, 2025, FAA-approved February 25, 2025.
Limitations and Conditions: (Continued)
2. 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.
Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST04812NY Effective Date: 12/08/2025 Limitations and Conditions: (Continued)
3. Prior to activation of a Wireless Cabin Distribution System, it must be shown that the aircraft is compatible with transmitting portable electronic devices (TPED) per FAA policy statement PS-AIR-25-13-R1.
4. Operational approval to permit use of Transmitting Portable Electronic Devices (TPED) must be obtained separately from this STC. Use of FAA InFO 13010 is an acceptable means.
5. Configuration 3 - Aircraft Effectivity List document 900-110741 specifies groups of aircraft that have been evaluated as part of the STC certification. Prior to installation of Configuration 3, verify aircraft SN has been certified per Aircraft Effectivity List.
6. This STC is in compliance with 14 CFR 36.7, Acoustical Change for transport category large airplanes.
7. AMOC. Per FAA ACO AMOC Approval Letter: 752-25-00025, Log 24-39 The inspection program of the ICA & ALS of this STC is approved as an Alternate Method of Compliance (AMOC) to Airworthiness Directive (AD) 2021-22-24 for the areas affected by the STC. All provisions of AD 2021-22-24 that are not specifically referenced in these ICA & ALS remain fully applicable and must be complied with accordingly.
Aircraft Models (Continued):
CL-600-2C10 (Regional Jet Series 700, 701 & 702) CL-600-2D24 (Regional Jet Series 900) The STC's supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the properly of the STC holder.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST04812NY Effective Date: 12/08/2025 Certification Basis:
1. Based on 14 CFR §§21.101 and 21.115, and the FAA policy for non-significant changes in FAA Order 8110.48, the certification basis for the MHI RJ Aviation ULC CL-600-2C10 and CL-600-2D24 for this design change modification is as follows:
a. The type certification basis for this aircraft is shown on Type Certificate Data Sheet (TCDS) A21EA-1 for parts not altered nor affected by the design change
b. The certification basis for parts altered or affected by the design change since the reference date of project application is based upon Part 25 & 26 as amended through Amendment 25-98 and 26-7 as listed in the TCDS, with the exceptions listed below.
Regulations at the amendment level in TCDS: 14CFR §§
25.29, 25.111, 25.115, 25.119, 25.121, 25.123, 25.251, 25.301, 25.303, 25.305, 25.307, 25.331,
25.333, 25.335, 25.341, 25.351, 25.365, 25.561, 25.571, 25.581, 25.601, 25.603, 25.605,
25.607, 25.609, 25.611, 25.613, 25.623, 25.625, 25.629, 25.771, 25.773, 25.777, 25.789,
25.831, 25.841, 25.863, 25.901, 25.981, 25.1301, 25.1309, 25.1322, 25.1351, 25.1353, 25.1357,
25.1381, 25.1401, 25.1419, 25.1431, 25.1501, 25.1519, 25.1525, 25.1529, 25.1541, 25.1581,
25.1583, 25.1585, 25.1587, H25.2, H25.4, 26.11, 26.47 Regulations above the amendment level in TCDS: 14 CFR §§
25.853 [25-116], 25.869 [25-113], 25.899 [25-123], 25.981 [25-125], H25.5 [25-123]
c. Applicable provisions of 14 CFR part 26 included in the certification basis and listed above.
For any future Part 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections as listed in the TCDS.
ELOS: §25.251(b) Vibration and Buffeting: ODA-GED-P342-25.251(b) ELOS: §25.773(a)(2): Pilot Compartment View: ODA-GED-P342-25.773(a)(2) END
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.