STC ST04442AT

Title: (for) Christina M. Underwood Manager, Atlanta ACO Branch Compliance and Airworthiness Division Aircraft Certification Service ST04442AT Woven Electronics, LLC 16000 Pines Blvd #824431 Pembroke Pines, FL 33082-9599 Part 25 Federal Aviation Regulations A1NM Boeing 767-200/-300/-300F Series Installation of the Rockwell Collins Automatic Dependent Surveillance - Broadcast (ADS-B) Out System on the Boeing 767-200/-300/-300F Series Aircraft in accordance with Master Drawing List (MDL) 2-197693-001, Rev C, Dated November 04, 2019, or later FAA approved revision.

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determine by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. (continued on page 3) January 5, 2017 July 11, 2022 March 18, 2019 December 5, 2019 3

ST04442AT 3

ST04442AT Limitations and Conditions (continued)

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 Approved Airplane Flight Manual Supplement for the Rockwell Collins Automatic Dependent Surveillance - Broadcast (ADS-B) Out System 2-197693-805, Rev A, Dated December 5, 2019, or later FAA approved revision is a required part of this STC.

Instructions for Continued Airworthiness (ICA), document 2-197693-804, Rev C, dated November 4, 2019 or later FAA accepted revision must be made available to the operator at the time of installation.

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 767-200/-300/-300F series aircraft is as follows:

a. The type certification basis for Boeing 767-200/-300/-300F series aircraft are shown on TCDS A1NM for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, January 05, 2017 is based upon Part 25 as amended by Amendment 25-143. 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 this modification was determined to be:

Regulations at the latest amendment 25-0 through 25-143

25.23(a), 25.301(a)(b), 25.303, 25.305(a), 25.337, 25.561(c), 25.581(a)(b), 25.601, 25.603(b)(c), 25.605

(a), 25.607, 25.609(a), 25.613(a)(b)(c), 25.789(a), 25.841(a)(3), 25.853(a), 25.863(a), 25.1351(a)(1),

25.1381(a)(1), 25.1431(a)(c), 25.1529, 25.1541(b), 25.1581. This modification has been determined by the FAA to be a no acoustic change per 21.93(b).

Regulations at an intermediate amendment

25.571 Amdt 25-96, 25.869(a)(4) Amdt. 25-113, 25.1353(a)(b)(d) Amdt. 25.113

Regulations at the amendment level in TCDS A1NM

25.307(a), 25.611, 25.1301(a)(b)(c)(d), 25.1309(a)(b)(d), 25.1322, 25.1357(a)(c)

14 CFR Part 26 Regulations Based on 14 CFR §21.101(g), applicable provision 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 issuance date of this STC, compliance has been found for the following regulations: 14 CFR §26.11 and 26.47.

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