STC ST04563CH

Number: ST04563CH

Part 25 of the Federal Aviation Regulations.

Original Product Type Certificate Number: A46NM Make: Airbus Model: A330-200 Series ; A330-200 Freighter Series ; A330-300 Series

Date of Application: April 8, 2021 Date Reissued:

Date of Issuance: January 23, 2023 Date Amended:

Brenda L. Litchfield ODA Administrator Title: Envoy Aerospace, LLC ODA-831240-CE CertifyNation, LLC W220 N1051 Springdale Road Waukesha, WI 53186

1) This STC is applicable to all serial numbers for these 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, CertifyNation Doc. No. CN20-019AFM-01, Revision 0, approved January 23, 2023, or later FAA approved revision, is required on board the modified aircraft.

4) 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 Honeywell Enhanced Ground Proximity Warning Computer (EGPWC) Upgrade and Runway Awareness and Advisory System (RAAS) Activation in accordance with CertifyNation Master Data List, Doc.

CN20-019MDL-00, Revision 2, dated January 13, 2023, or later FAA approved revision.

Number: ST04563CH

(Continuation Sheet) Number: ST04563CH

Date of Issuance: January 23, 2023 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 Series, A330-200 Freighter Series and A330-300 Series aircraft is as follows:

a. The type certification basis for the Airbus A330-200 Series, A330-200 Freighter Series and A330-300 Series aircraft is shown on TCDS A46NM 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 A46NM. 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 amendment shown on TCDS A46NM § 25.29(a)(b) § 25.301(a)(b) § 25.303 § 25.305(a)(b) § 25.307(a) § 25.561(b)(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) § 25.789(a) § 25.853(a) § 25.869(a)(4) § 25.1301(a)(b)(c)(d) § 25.1309(a)(b)(c)(d)(g) § 25.1321(e) § 25.1322(b)(c)(d) § 25.1351(a) § 25.1353(a)(b)(d) § 25.1431(a)(b)(c)(d) § 25.1501(a)(b) § 25.1529 § 25.1581(a)(b)(d) § 25.1583(h) § 25.1585(a)(b)

Applicable 14 CFR Part 25 regulations at other amendment levels § 25.981(a)(3) [Amdt 25-125] Applicable 14 CFR Part 26 regulations at the latest amendment 26-0 through 26-1 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]. This modification does not affect or create fatigue critical baseline structure.

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