STC ST04427AT

Title: (for) Christina M. Underwood Manager, Atlanta ACO Branch Compliance and Airworthiness Division Aircraft Certification Service ST04427AT Woven Electronics, LLC 16000 Pines Blvd #824431 Pembroke Pines, FL 33082-9599 25 Federal Aviation Regulations A16WE Boeing 737 -600/700/700C/800/900/900ER Installation of the Rockwell Collins Automatic Dependent Surveillance – Broadcast (ADS-B) Out System on the Boeing 737 -600/700/700C/800/900/900ER Series Aircraft in accordance with Master Drawing List (MDL) 2-193114-001, Rev. A, Dated May 9, 2018, or later FAA approved revision.

(See continuation sheets 3 and 4) October 13, 2017 June 14, 2022 June 14, 2018 4

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ST04427AT Limitations and Conditions (continued)

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. 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, 2-193114-805, Rev IR, Dated June 05, 2018, or later FAA approved revision is a required part of this STC.

Instructions for Continued Airworthiness (ICA) document 2-193114-804, Rev. A, dated May 9, 2018 or later FAA approved 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 737 -600/700/700C/800/900/900ER series aircraft is as follows:

a. The type certification basis for Boeing 737 -600/700/700C/800/900/900ER series aircrafts are shown on TCDS A16WE for parts not changed or not affected by the change.

ST04427AT

b. The certification basis for parts changed or affected by the change since the reference date of application, October 13, 2017 is based upon part 25 as amended by Amendment 25-144. 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 25-142

25.23(a), 25.301(a)(b), 25.303, 25.305(a), 25.561(c), 25.601, 25.603(b)(c), 25.853(a),

25.863(a), 25.1381(a)(1), 25.1431(a)(c), 25.1529

Regulations at an intermediate amendment

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

Regulations at the amendment level in TCDS A16WE

25.307(a), 25.611, 25.1301(a)(b)(c)(d), 25.1309(b)(d), 25.1322, 25.1351(a)(1),

25.1357(a)(c), 25.1581 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 regulation: 14 CFR 26.11 and

26.47.

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