# STC ST04520AT

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Woven Electronics LLC
- Description: Installation of Rockwell Collins GLU-2100 Multi Mode Receivers (MMR)
- Status date: May 25, 2022
- Data sheets: A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A46NM, A46NM, A46NM, A46NM, A46NM, A46NM, A46NM, A46NM, A46NM, A46NM, A46NM, A46NM, A46NM, A46NM, A46NM, A46NM, A46NM, A46NM
- Certificate PDF: https://openairdocs.org/files/sha256/73/f3/73f3d009bed405c4ca9b9e9fb14659f6580ef69776d960dba4822ebd8a3a6e67
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/121F21285077C57C86258855005D8041.0001
- Page: https://openairdocs.org/stc/ST04520AT

## ADs that name it

None.

## Approved models (61)

- Airbus SAS A319-111 (TCDS A28NM)
- Airbus SAS A319-112 (TCDS A28NM)
- Airbus SAS A319-113 (TCDS A28NM)
- Airbus SAS A319-114 (TCDS A28NM)
- Airbus SAS A319-115 (TCDS A28NM)
- Airbus SAS A319-131 (TCDS A28NM)
- Airbus SAS A319-132 (TCDS A28NM)
- Airbus SAS A319-133 (TCDS A28NM)
- Airbus SAS A319-151N (TCDS A28NM)
- Airbus SAS A319-153N (TCDS A28NM)
- Airbus SAS A319-171N (TCDS A28NM)
- Airbus SAS A320-111 (TCDS A28NM)
- Airbus SAS A320-211 (TCDS A28NM)
- Airbus SAS A320-212 (TCDS A28NM)
- Airbus SAS A320-214 (TCDS A28NM)
- Airbus SAS A320-216 (TCDS A28NM)
- Airbus SAS A320-231 (TCDS A28NM)
- Airbus SAS A320-232 (TCDS A28NM)
- Airbus SAS A320-233 (TCDS A28NM)
- Airbus SAS A320-251N (TCDS A28NM)
- Airbus SAS A320-252N (TCDS A28NM)
- Airbus SAS A320-253N (TCDS A28NM)
- Airbus SAS A320-271N (TCDS A28NM)
- Airbus SAS A320-272N (TCDS A28NM)
- Airbus SAS A320-273N (TCDS A28NM)
- Airbus SAS A321-111 (TCDS A28NM)
- Airbus SAS A321-112 (TCDS A28NM)
- Airbus SAS A321-131 (TCDS A28NM)
- Airbus SAS A321-211 (TCDS A28NM)
- Airbus SAS A321-212 (TCDS A28NM)
- Airbus SAS A321-213 (TCDS A28NM)
- Airbus SAS A321-231 (TCDS A28NM)
- Airbus SAS A321-232 (TCDS A28NM)
- Airbus SAS A321-251N (TCDS A28NM)
- Airbus SAS A321-251NX (TCDS A28NM)
- Airbus SAS A321-252N (TCDS A28NM)
- Airbus SAS A321-252NX (TCDS A28NM)
- Airbus SAS A321-253N (TCDS A28NM)
- Airbus SAS A321-253NX (TCDS A28NM)
- Airbus SAS A321-271N (TCDS A28NM)
- Airbus SAS A321-271NX (TCDS A28NM)
- Airbus SAS A321-272N (TCDS A28NM)
- Airbus SAS A321-272NX (TCDS A28NM)
- Airbus SAS A330-201 (TCDS A46NM)
- Airbus SAS A330-202 (TCDS A46NM)
- Airbus SAS A330-203 (TCDS A46NM)
- Airbus SAS A330-223 (TCDS A46NM)
- Airbus SAS A330-223F (TCDS A46NM)
- Airbus SAS A330-243 (TCDS A46NM)
- Airbus SAS A330-243F (TCDS A46NM)
- Airbus SAS A330-301 (TCDS A46NM)
- Airbus SAS A330-302 (TCDS A46NM)
- Airbus SAS A330-303 (TCDS A46NM)
- Airbus SAS A330-321 (TCDS A46NM)
- Airbus SAS A330-322 (TCDS A46NM)
- Airbus SAS A330-323 (TCDS A46NM)
- Airbus SAS A330-341 (TCDS A46NM)
- Airbus SAS A330-342 (TCDS A46NM)
- Airbus SAS A330-343 (TCDS A46NM)
- Airbus SAS A330-841 (TCDS A46NM)
- Airbus SAS A330-941 (TCDS A46NM)

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Title: (for) Christina M. Underwood Manager, Atlanta ACO Branch Compliance and Airworthiness Division Aircraft Certification Service ST04520AT Woven Electronics, LLC 16000 Pines Blvd, #824431 Pembroke Pines, FL-33082-9599 Part 25 the Federal Aviation Regulations See AML FAA Approived Model List (AML) See B/E Aerospace document No. 2-197186-002 Rev. IR or later FAA approved revision for a list of Approved Aircraft Models.

Installation of Rockwell Collins GLU-2100 Multi Mode Receivers (MMR) in accordance with latest FAA Approved Model List (AML) 2-197186-002 revision.

(See Continuation Sheet 3 of 4) April 3, 2019 May 25, 2022 June 16, 2021 4

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

ST04520AT

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

ST04520AT Limitations and Conditions - cont.:

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

2. 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.

3. Instructions for Continued Airworthiness (ICA) as listed in the FAA Approved Model List (AML) document and the Airplane Flight Manual Supplement (AFMS) as listed in the FAA Approved Model List (AML) must be made available to the operator at the time of installation.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

ST04520AT Certification Basis:

Based on 14CFR 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for each model is as specified in the FAA Approved Model List (AML) 2-197186-002.

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**

--------------------------END--------------------------- 4 4

### AML_ST04520AT.pdf

B/E Aerospace 9100 NW 105th Circle Medley, FL 33178 USA Doc. No.: 2-197186-002 Rev.: IR Page 1 of 5

APPROVED MODEL LIST, Installation of the Rockwell Collins Multi Mode Receivers (MMR) on various 14 CFR Part 25 Airbus Aircraft FAA Project: ST16136AT-T F AA APPROVED: ____________________________ (for) Manager, Atlanta ACO kjk Branch Federal Aviation kjh Administration Atlanta, Georgia D ATE: ______________ 6/16/21

A

PPROVED MODEL LIST Doc. No.: 2-197186-002 Rev.: IR Page 2 of 5

**1.0 AML REVISION LOG**

REV PAGES DESCRIPTION APPROVAL/DATE IR 1 - 5 I nitial Release Date: _________

**APPROVED MODEL LIST**

FAA APPROVED DATE: ________________

Doc. No.: 2-197186-002 Rev.: IR

Page 3 of 5

**2.0 INTRODUCTION**

This document is the FAA Approved Model List (AML) for Supplemental Type Certificate (STC) No. ST04520AT for the installation of the Rockwell Collins Multi Mode Receivers (MMR) on eligible aircraft.

Revisions to this AML must be coordinated between the STC holder and the responsible ACO, and requires FAA approval.

6/16/21

**APPROVED MODEL LIST**

FAA APPROVED DATE: ________________

Doc. No.: 2-197186-002 Rev.: IR

Page 4 of 5

3.0 CERTIFICATION BASIS The certification basis for each model qualified for this installation is detailed below.

Item Aircraft Make Aircraft Model TCDS Certification Basis Required Approved Data and Added Model Specific Limitations AML Initial Approval Date AML Amendment Date 1 Airbus A330 Series A46NM 14 CFR Part 25 of the Federal Aviation Regulations: Amendments 25-1 through 25-145.

(see *Notes)

Master Drawing List (MDL):

2-197186-001, Rev. B or later FAA approved revision Airplane Flight Manual Supplement:

2-197186-805 Installation Instructions:

2-197186-801 Instructions for Continued Airworthiness:

2-197186-804 Software:

OPS: RCU4B0009000600

Date:

___________

2 Airbus A319/A320/ A321 Series A28NM 14 CFR Part 25 of the Federal Aviation Regulations: Amendments 25-1 through 25-145.

(see *Notes)

Master Drawing List (MDL):

2-197186-001, Rev. B or later FAA approved revision Installation Instructions:

2-197187-801 Instructions for Continued Airworthiness:

2-197187-803 Software:

OPS: RCU4B0009000600

Date:

___________

6/16/21 6/16/21 6/16/21

**APPROVED MODEL LIST**

FAA APPROVED DATE: ________________

Doc. No.: 2-197186-002 Rev.: IR

Page 5 of 5 *Notes:

Certification Basis for Modification:

AML Item 1 Regulations at the latest amendment 25-1 through 25-145

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), 25.1329(i), 25.1431(a)(c), 25.1529,

25.1581 This modification has been determined to be a no acoustic change in accordance with 21.93(b) Regulations at an intermediate amendment

25.1353(a)(b)(d) Amdt. 25-113 Regulations at the amendment level in TCDS A46NM

25.307(a), 25.611, 25.1301(a)(b)(c)(d), 25.1309(a)(b)(d), 25.1351(a)(1), 25.1581

AML Item 2 Regulations at the latest amendment 25-1 through 25-145

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), 25.1329(i), 25.1431(a)(c), 25.1529 This modification has been determined to be a no acoustic change in accordance with 21.93(b) Regulations at an intermediate amendment

25.1353(a)(b)(d) Amdt. 25-113 Regulations at the amendment level in TCDS A28NM

25.307(a), 25.611, 25.1301(a)(b)(c)(d), 25.1309(a)(b)(d), 25.1351(a)(1), 25.1581

6/16/21

## Every issue (2)

- May 25, 2022: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/73/f3/73f3d009bed405c4ca9b9e9fb14659f6580ef69776d960dba4822ebd8a3a6e67), [AML_ST04520AT.pdf](https://openairdocs.org/files/sha256/71/a7/71a7a2d319ffc9d3596fc7d54b087762f98e4aaea78228207adb57a05a9a9a9a)
- June 16, 2021: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/f3/1e/f31ed71a9a363240cdb117346f89b93c68eb9a5d28dbc8c045c00e459fc95141), [AML_ST04520AT.pdf](https://openairdocs.org/files/sha256/71/a7/71a7a2d319ffc9d3596fc7d54b087762f98e4aaea78228207adb57a05a9a9a9a)

---
From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.
