STC ST04445CH

ST04445CH Honeywell International Inc.

21111 N 19th Ave Phoenix, AZ 85027 Part 25 the Code of Federal Regulations A35EU Airbus A300F4-622R Installation of a Honeywell ADG-300 Wireless Data Loader in accordance with CertifyNation Master Data List, Doc. No. CN19-006MDL-00, Revision 1, dated August 13, 2020, or later FAA approved revision.

1) The installer must determine whether this design change is compatible with previously approved modifications.

2) FAA Approved Airplane Flight Manual Supplement as identified in CertifyNation Master Installation Drawing, CertifyNation Drawing No. MI19-006-00, Revision 5, dated March 30, 2021, or later FAA approved revision is required on board the modified aircraft.

(See Page 5 of 5 for complete Limitations and Conditions.)

June 19, 2018 September 3, 2020; November 10, 2022 August 20, 2020 April 2, 2021 Steven L. Lardinois Manager, Systems Section Chicago ACO Branch 5

ST04445CH

ST04445CH 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 A300F-622R aircraft is as follows:

a. The type certification basis for the Airbus A300F-622R aircraft is shown on TCDS A35EU 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 A35EU. 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 to installation configurations Ml19-006-00-101/-103/-105

14 CFR Part 25 Regulations at the latest amendment 25-0 through 25-44

§ 25.29(a)(b) § 25.603(a)(b) § 25.1309(a)(b)(d)(g) § 25.301(a)(b) § 25.605 § 25.1351(a) § 25.303 § 25.609(a)(b) § 25.1353(a)(b) § 25.305(a)(b) § 25.611 § 25.1357(a)(c) § 25.307(a) § 25.613(a)(b) § 25.1431(a)(b)(c) § 25.365(a)(b)(c)(d) § 25.619(a)(b)(c) § 25.1501(a)(b) § 25.561(c)(d) § 25.625(a) § 25.1581(a)(b)(d) § 25.581(a)(b)(c) § 25.1301(a)(b)(c)(d) § 25.1585(a) § 25.601 § 25.1307(c)

14 CFR Part 25 regulations at other amendment levels

§ 25.853(a) [Amdt 25-116]; § 25.869(a)(4) [Amdt 25-113]; § 25.981(a)(3) [Amdt 25-102]; § 25.1529 [Amdt 25-54].

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. 26-0]. This modification does not affect or create fatigue critical structure.

ST04445CH Applicable to installation configurations MI19-006-00-201/-203

14 CFR Part 25 Regulations at the latest amendment 25-0 through 25-44

§ 25.29(a)(b) § 25.603(a)(b) § 25.1351(a) § 25.301(a)(b) § 25.605 § 25.1353(a)(b) § 25.303 § 25.609(a)(b) § 25.1357(a)(c) § 25.305(a)(b) § 25.611 § 25.1501(a)(b) § 25.307(a) § 25.613(a)(b) § 25.1581(a)(b)(d) § 25.365(a)(b)(c)(d) § 25.619(a)(b)(c) § 25.1585(a) § 25.561(c)(d) § 25.625(a) § 25.601 § 25.1307(c)

14 CFR Part 25 Regulations at the latest amendment 25-0 through 25-144

§ 25.853(a) § 25.1316(a)(b) § 25.1431(a)(b)(c)(d) § 25.1301(a) § 25.1317(a)(b)(c) § 25.1529 § 25.1309(a)(b)(d)(e) § 25.1360(a)(b)

14 CFR Part 25 regulations at other amendment levels

§ 25.571(a)(b) [Amdt 25-45]; § 25.869(a)(4) [Amdt 25-113]; § 25.981(a)(3) [Amdt 25-102].

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. 26-0]; § 26.47(c) [Amdt. No. 26-1].

ST04445CH Date of Issuance: August 20, 2020 Date Reissued: September 3, 2020; November 10, 2022 Date Amended: April 2, 2021

3) This modification requires prior or concurrent application of separate design changes as identified in CertifyNation Master Data List, Doc. No. CN19-006MDL-00, Revision 1, dated August 13, 2020, or later FAA approved revision.

4) This STC is applicable to all serial numbers for this Make-Model.

5) This installation does not include Electronic Flight Bag (EFB) computers. Operational approval of the EFB computers should follow the guidance in Advisory Circular (AC) No. 120-76D, or other FAA approved guidance.

6) 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.

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