# STC SR00851DE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Peregrine, United States - Description: Installation of Automatic Dependent Surveillance - Broadcast (ADS-B) Out functionality using the Garmin GTX 330ES transponder and a qualified position sensor - Applied: November 16, 2015 - Status date: May 6, 2019 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 29 - Data sheets: [TCDS H13EU](https://openairdocs.org/tcds/H13EU) - Certificate PDF: https://openairdocs.org/files/sha256/19/4a/194a80783c5508e5ceb250b66d33e38d7002cef5c53f59572cdb275b78610493 - Approved model list and other attachments: [SR00851DE_AML.pdf](https://openairdocs.org/files/sha256/0d/76/0d767eebde7dd338df1ab50cb559e4eadd494636207155209385a8bb38576e82) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C1F24E047F663AE7862585CB0038409B.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR00851DE ## ADs that name it (0) None. ## Approved models (7) - Airbus Helicopters Deutschland GmbH MBB-BK 117 A-1 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU)) - Airbus Helicopters Deutschland GmbH MBB-BK 117 A-3 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU)) - Airbus Helicopters Deutschland GmbH MBB-BK 117 A-4 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU)) - Airbus Helicopters Deutschland GmbH MBB-BK 117 B-1 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU)) - Airbus Helicopters Deutschland GmbH MBB-BK 117 B-2 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU)) - Airbus Helicopters Deutschland GmbH MBB-BK 117 C-1 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU)) - Airbus Helicopters Deutschland GmbH MBB-BK 117 C-2 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU)) ## 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 (5/14) Page 1 of 2 Part 29 of the Federal Aviation Regulations. Installation of Automatic Dependent Surveillance – Broadcast (ADS-B) Out functionality using the Garmin GTX 330ES transponder and a qualified position sensor, in accordance with the aforementioned AML and the Peregrine Master Drawing List, Document No. E-AM-15-0022, Rev B, dated April 27, 2017, or later FAA-approved revision. 1. The installation must not be incorporated in any rotorcraft unless the installer determines that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the rotorcraft. 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. A copy of this certificate must be maintained as part of the records of the altered rotorcraft. Date of Application: November 16, 2015 Date Reissued: December 19, 2018; May 6, 2019 Date of Issuance: April 28, 2017 Date Amended: Signature Todd Dixon Manager, Denver ACO Branch Compliance and Airworthiness Division SR00851DE Peregrine 7385 S. Peoria Street Unit C4 Englewood, CO 80112 FAA Approved Model List (AML) for ADS-B Out, Document No. SR00851DE, Rev IR, dated April 28, 2017, or later FAA approved revision, lists the approved rotorcraft models, applicable installation data requirements, and specific limitations. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR00851DE FAA Form 8110-2 (5/14) Page 2 of 2 To (Name and address of transferee) From (Name and address of grantor) ### SR00851DE_AML.pdf FAA Approved: \\Todd Dixon\\ Todd Dixon, Manager Denver Aircraft Certification Office Original Issue: April 28, 2017 Approved Model List (AML) For Automatic Dependent Surveillance - Broadcast (ADS-B) Out System using the Garmin GTX 330ES Transponder and Qualified Position Sources Peregrine STC No. SR00851DE FAA APPROVED MODEL LIST For ADS-B Out Airworthiness Approval Peregrine STC NO. SR00851DE Page ii 1 Revision Log Revision Pages Description FAA Approval Date IR 1-9 Initial Release \\Todd Dixon\\ Manager, Denver Aircraft Certification Office Federal Aviation Administration Transport Airplane Directorate Date: 4/28/2017__________________________ Original Issue Apr 28, 2017 FAA APPROVED MODEL LIST For ADS-B Out Airworthiness Approval Peregrine STC NO. SR00851DE Original Issue: April 28, 2017 Page 1 2 Introduction This document is the Federal Aviation Administration (FAA) Approved Model List (AML) for Supplemental Type Certificate (STC) Number SR0085 1DE, for installing the Automatic Dependent Surveillance - Broadcast (ADS -B) Out System using the Garmin GTX 330ES Transponder and a qualified Global Position System (GPS) with Wide Area Augmentation System (WAAS) into eligible rotorcraft. Qualified ADS -B Out equipage is listed in Section 4, and a pproved models are listed in Section 5. This AML approves upgrading an existing Garmin GTX 330 to the GTX 330ES. If necessary, this AML also approves upgrading an existing Garmin GNS 400W/500W Series GPS/WAAS position source. This AML is only applicable to the 14 CFR Part 29 civilian rotorcraft, listed in Section 5. Installations in 14 CFR Part 23, Part 25, Part 27 and unlisted Part 29 rotorcraft are not authorized under this AML. Revisions to this AML must be coordinated between the STC holder and the responsible Aircraft Certification Office (ACO), and require FAA approval. 2.1 Prerequisites This AML assumes the following equipment is alrea dy installed on each rotorcraft eligible for this proposed modification. The equipment must be previously installed and properly linked to meet the intended function for the system, as certified under this AML approval. 1. Transponder system, including i. Garmin GTX 330 panel-mounted transponder, and, ii. Technical Standard Order (TSO) Approved transponder antenna that meets TSO -C66 or TSO-C74. 2. A digital altitude encoder that outputs either Gillham code or RS-232 formatted data. 3. GNS 400W/500W Series GPS/WAAS and associated antenna. FAA APPROVED MODEL LIST For ADS-B Out Airworthiness Approval Peregrine STC NO. SR00851DE Original Issue: April 28, 2017 Page 2 2.2 Limitations The following limitations apply to this AML STC. 1. Installation of the following required equipment is outside the scope of this AML STC. This AML STC does NOT include installation approval of the following i. an altitude encoder, ii. a transponder antenna, iii. a GPS/WAAS antenna. 2. Installation of the position sensors listed in Section 4 is outside the scope o f this AML . This AML STC does NOT include installation approval of a GNS 400W/500W Series GPS/WAAS receiver and associated GPS antenna. 3. This AML STC approves software upgrades of the position sensors listed in Section 4. Approved software updates are limited to those specifically identified in Section 4 of this AML. 4. This AML STC includes instructions for upgrading an existing Garmin GTX 330 Transponder to a GTX 330ES Transponder. However, this AML STC does NOT allow or provide instructions for the installation of the Garmin GTX 330 Transponder. 5. This AML STC does NOT allow or provide instructions for installation on a rotorcraft equipped with the following systems: i. Traffic Collision Avoidance System (TCAS) II, and ii. Full Authority Digital Engine Controller (FADEC). FAA APPROVED MODEL LIST For ADS-B Out Airworthiness Approval Peregrine STC NO. SR00851DE Original Issue: April 28, 2017 Page 3 3 Certification Basis The certification basis for each qualified model is specified in the type certificate data sheet (TCDS) and modified by the amendment levels noted in Appendix A. 4 Approved ADS-B Out Equipage This AML STC approves the Garmin GTX 330ES transponder, part number (p/n) 011 -00455-60 and 011-00455-80 (software version 7.04 or later) to be paired with a Garmin GNS 400W/500W Series GPS/WAAS receiver listed in Table 1 below. Table 1: Eligible GNS 400W/500W GPS WAAS Receiver1 Model Number Part Number Description GNC 420AW 011-01059-(__) GPS/WAAS & VHF COM (16W) GNS 430W 011-01060-(__) GPS/WAAS, VHF COM (10W) & VHF NAV (VOR/LOC/GS) GNS 430AW 011-01061-(__) GPS/WAAS, VHF COM (16W) & VHF NAV (VOR/LOC/GS) GPS 500W 011-01062-(__) GPS/WAAS GPS 500W TAWS 011-01063-(__) GPS/WAAS with Terrain Awareness & Warning System GNS 530W 011-01064-(__) GPS/WAAS, VHF COM (10W) & VHF NAV (VOR/LOC/GS) GNS 530W TAWS 011-01065-(__) GPS/WAAS, VHF COM (10W) & VHF NAV (VOR/LOC/GS) with Terrain Awareness & Warning System GNS 530AW 011-01066-(__) GPS/WAAS, VHF COM (16W) & VHF NAV (VOR/LOC/GS) GNS 530AW TAWS 011-01067-(__) GPS/WAAS, VHF COM (16W) & VHF NAV (VOR/LOC/GS) with Terrain Awareness & Warning System **NOTE(S)** 1. Garmin GNS 400W/500W Series GPS/WAAS Receiver using main software version 5.20 or later, and GPS software version 5.0 or later is approved for this STC. FAA APPROVED MODEL LIST For ADS-B Out Airworthiness Approval Peregrine STC NO. SR00851DE Original Issue: April 28, 2017 Page 4 5 Approved Model List Item Aircraft Make Aircraft Model TCDS Certification Basis Master Drawing List / Date AFM Supplement Number / Date Instructions for Continued Airworthiness Notes Initial Approval / Amendment Date 1. Airbus Helicopters Deutschland GmbH MBB-BK 117 A-1, MBB-BK 117 A-3, MBB-BK 117 A-4, MBB-BK 117 B-1, MBB-BK 117 B-2, MBB-BK 117 C-1, MBB-BK 117 C-2 H13EU 14 CFR 29 per TCDS as amended by Appendix A Peregrine Doc. No. E-AM-15-0022, Rev B, dated 04/28/17, or later FAA approved revision. Peregrine Doc. No. E-AM-15-0029, Initial Release, dated April 24, 2017, or later FAA approved revision. Peregrine Doc. No. E-AM-15-0028, Initial Release, dated 02/07/17, or later FAA approved revision. (1) Initial Approval Apr 28, 2017 NOTE(S): (1) Eligible serial numbers are those that have been examined, tested, and found to comply with German LBA TC # 3049 (or EASA TC # R.010) approved under the U.S TC#H13EU and found to be in a condition for safe operation. FAA APPROVED MODEL LIST For ADS-B Out Airworthiness Approval Peregrine STC NO. SR00851DE Original Issue: April 28, 2017 Page 5 Appendix A: All Models Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis is as follows: a. As determined by the Type Certificate Data Sheet (TCDS) of the aircraft for parts not changed or not affected by this STC. b. Regulations at the amendment levels listed in Table 1 below for parts changed or affected by the STC since the reference date of STC application, November 16, 2015. Table 2: Certification Basis Including Amendments. Regulations Amdt. § 29.151 29-24 § 29.301 29-0 § 29.303 29-0 § 29.305 29-0 § 29.307 (a) 29-30 § 29.337 29-30 § 29.341 29-0 § 29.471 29-0 § 29.561 (a)(b)(3) 29-38 § 29.601 29-0 § 29.603 29-17 § 29.605 29-17 § 29.607 29-5 § 29.609 29-0 § 29.610 (a)(b)(d) 29-53 § 29.611 29-0 § 29.613 29-30 § 29.619 29-0 § 29.625 29-37 § 29.671 (a) 29-24 § 29.771 (a) 29-24 § 29.773 (a)(1) 29-3 § 29.777 29-0 Regulations Amdt. § 29.863 29-17 § 29.1301 (a)(b)(c)(d) 29-0 § 29.1309 (a)(b)(c)(d)(e)(f)(g) 29-53 § 29.1316 (b) 29-53 § 29.1317 (c) 29-49 § 29.1321 (a)(g) 29-21 § 29.1322 29-12 § 29.1351 (a)(d) 29-42 § 29.1353 (a)(b) 29-15 § 29.1357 (a)(c)(d)(e) 29-24 § 29.1359 (a)(c) 29-42 § 29.1381 29-0 § 29.1431 29-0 § 29.1501 29-15 § 29.1529 29-20 § 29.1541 29-0 § 29.1581 29-15 § 29.1583 (c)(e) 29-24 § 29.1585 (a) 29-24 ## Every issue (3) - May 6, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/19/4a/194a80783c5508e5ceb250b66d33e38d7002cef5c53f59572cdb275b78610493), [SR00851DE_AML.pdf](https://openairdocs.org/files/sha256/0d/76/0d767eebde7dd338df1ab50cb559e4eadd494636207155209385a8bb38576e82) - December 19, 2018: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/56/fb/56fb49f26326b0dbb2930a91fef3c5bc3a99ec76caef2fc4ed251f6102924d53), [SR00851DE_AML.pdf](https://openairdocs.org/files/sha256/0d/76/0d767eebde7dd338df1ab50cb559e4eadd494636207155209385a8bb38576e82) - April 28, 2017: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/3c/85/3c85c90e09b90867c7409e450895ff4dd580c7ba533e463cbfcd2ec5393bfc98), [SR00851DE_AML.pdf](https://openairdocs.org/files/sha256/0d/76/0d767eebde7dd338df1ab50cb559e4eadd494636207155209385a8bb38576e82) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.