What it approves
INSTALL AVIO BOOK AVIOCAST AIRCRAFT INTERFACE (AID) SYSTEM PROVISIONS
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.
Number: ST04630CH
Part 25 of the Federal Aviation Regulations.
Original Product Type Certificate Number: A16WE Make: Boeing Model: 737-700 Series ; 737-800 Series
Date of Application: July 19, 2023 Date Reissued:
Date of Issuance: January 29, 2024 Date Amended:
Brenda L. Litchfield ODA Administrator Title: Envoy Aerospace, LLC ODA-831240-CE Canard Aerospace Corporation 1157 Valley Park Dr., Suite 115 Shakopee, MN 55379
1) This STC is applicable to all serial numbers for this Make-Model-Series.
2) The installer must determine whether this design change is compatible with previously approved modifications.
3) FAA Approved Airplane Flight Manual Supplement, Canard Aerospace Corporation Doc. No. 46-3685-06, Revision NC, approved January 29, 2024, or later FAA approved revision is required on board the modified aircraft.
4) This installation approval does not include Electronic Flight bag (EFB) computers or the AvioCast AID server.
The operational approval of EFB computers and the AvioCast AID Server should follow the guidance for portable equipment in Advisory Circular (AC) No. 120-76D, or other FAA issued guidance.
5) 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.
Installation of AvioBook AvioCast Aircraft Interface Device (AID) System Provisions in accordance with Canard Aerospace Corporation Document Control Drawing, Dwg. No. 40225, Revision C, dated January 23, 2024, or later FAA-approved revisions.
Number: ST04630CH
(Continuation Sheet) Number: ST04630CH Date of Issuance: January 29, 2024 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 737-700, -800 Series aircraft is as follows:
a. The type certification basis for the Boeing 737-700, -800 Series aircraft is shown on TCDS A16WE for parts not changed or affected by the change.
b. This certification basis for parts changed or affected by the change since the reference date of application is based upon TCDS A16WE. Based on 14 CFR 21.115 and 21.101, and the FAA policy for significant changes in Order 8110.48, the certification basis for this modification was determined to be:
Applicable regulations at the latest amendment 25-0 through 25-77 § 25.29(a)(b) § 25.301(a)(b) § 25.303 § 25.305(a)(b) § 25.307(a) § 25.561(c) § 25.601 § 25.603(a)(b)(c) § 25.605(a) § 25.609(a)(b) § 25.611 § 25.613(a)(b) § 25.619(a)(b)(c) § 25.625(a) § 25.777(a) § 25.789(a) § 25.1301(a)(b)(c)(d) § 25.1307(c) § 25.1309(a)(b)(d)(g) § 25.1351(a) § 25.1353(a)(b) § 25.1357(a)(c) § 25.1431(a)(b)(c) § 25.1529 § 25.1581(a)(b)(d) § 25.1585(a)(b)
Applicable 14 CFR Part 25 regulations at other amendment levels § 25.869(a) [Amdt 25-113]; § 25.981(a) [Amdt 25-125].
Applicable 14 CFR Part 26 regulations at the latest amendment 26-0 through 26-7 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 Part 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections. As of the latest amendment date of this STC, compliance has been found for the following regulations:
14 CFR § 26.11(c) [Amdt. No. 26-7]; § 26.47(c) [Amdt. No. 26-7]. This modification does not affect or create fatigue critical baseline structure.
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