Single /Dual Transponder System ADS-B Upgrade Part 23 aircraft
Overview
Introduction
Description of Change:
The change consists of a replacement/upgrade of the existing transponder/s (Single or dual) to include ADS-B functionality according Minimum Operational Performace Standards (DO-260B MOPS). To comply with the ADS-B (DO-260V) requirements (per CS-ACNS) the unit should hold an EASA equipment authorisation in accordance with ETSO-C166b and ETSO-C112d.
In addition the CS-ACNS requests an ADS-B Fail annunciation. Additional ADS-B Fail annunciator will be installed in instrument panel.
The STC 10059536 involves the following Types of Aircraft
- Aircraft Industries A.S.: L-410 UVP-E / UVP-E20 / UVP-E20 Gargo / UVP-E9 / UVP-E-LW / UVP-LW / MTurbolet /UVP-Turbolet and L-420
- Beechcraft Corporation: 100 / 99 / 99A / A100 / A100A / A99 / A99A / B100 / B99 / C99 / 1900 / 1900C / 1900D / 200/ 200/ 200CT / 200T / 300/ 300LW/A100-1/ A200/A200C/ A200CT/B200/ B200T / B200 / B200C / B200CGT / B300 / B300C
- Raytheon Aircraft company: 390 Premier I and IA
- Embraer S.A.: EMB-110K-1 / -110P1 / -110P2 / EMB-121A / -121A1 / EMB-500 / EMB-505
- M7 Aerospace L.L.C.: SA226TC / SA-227-AC / SA227-BC / SA-227-PC / SA227-CC / SA-227-DC / SA226-AT / SA-226-T / SA226-T(B) / SA227-AT / SA227-TT/ 26AT / 26T
- RUAG Aerospace Services GmbH: Dornier 228-100 / -101 / -200 / -202 / -212
- Short Brothers PLC: SD3-30 / -60 / -60 Sherpa / -Sherpa
- Air Tractor, Inc.: AT-602 / AT-802 / AT-802A
- ASI Aviation: F406
- Eclipse aerospace Incorporated: EA500
- Learjet Inc.: Learjet 23
- Mitsubishi Heavy Industries: MU-2B-10, MU-2B-20, MU-2B-25, MU-2B-26, MU-2B-26A, MU-2B36A, MU-2B-40, MU-2B-60
- Piaggio Aero Industries: P.166, P.166B, P.166C, P.166DL3, P.166DP1, P.166S, Avanti, Avanti II
- Pilatus Aircraft Ltd.: PC-12, PC-12/45, PC-12/47, PC-12/47E
- Piper Aircraft, Inc.: PA-42-100 (Cheyenne 400 LS), PA-42-720 (Cheyenne IIIA), PA-42 (Cheyenne III), PA-42-720R (Cheyenne III)
- Polskie Zaklady Lotnicze SP.: PZL M2800, PLZM2802, PZL M2805
- Socata: TBM700A, TBM700B, TBM700C1, TBM700C2, TBM700N
- Textron Aviation Inc.: 201 / 551 / 525 / 525A / 525B / 525C / 404 / 441 / 510
- Viking Air Limited: DHC-6 Series 1/ 100 / 110 / 200 / 210 / 300 / 310 / 320, DHC-Series 400
Your needs
The initial change consists of:
- TDR-94D XPDR Unit upgrade/replacement
- Installation of an ADS-B Fail / XPDR Fail Annunciator
- Installation of an A429 to Discrete Converter and related logic relays to
- drive the ADS-B Fail Annunciator.
- Interconnection with single GPS/FMS System
The ADS-B Fail / XPDR Fail Annunciator will be installed in the centre instrument panel to inform pilot about the XPDR and ADS-B function failures of the selected XPDR.
Your benefits
The TRD-94D provides the information about the XPDR Failure as a discrete signal which is connected to XPDR Fail annunciator light. The ADS-B function status is transmitted from TDR-94D only via Arinc 429 output. To drive the ADS-B
Fail annunciator light an A429 to Discrete Converter (including logic relays to relay the ADS-B Fail annunciator to the selected transponder) will be installed. The A429 to Discrete Converter is looking for Arinc 429 label 353 (bit 20 - which
defines the ADS-B function status) and converts it to a discrete signal connected to ADS-B Fail annunciator light.
Product Description
Single /Dual Transponder System ADS-B Upgrade Part 23 aircraft
Major Change Project 2101561 - to STC 10059536
Your benefits
The TRD-94D provides the information about the XPDR Failure as a discrete signal which is connected to XPDR Fail annunciator light. The ADS-B function status is transmitted from TDR-94D only via Arinc 429 output. To drive the ADS-B
Fail annunciator light an A429 to Discrete Converter (including logic relays to relay the ADS-B Fail annunciator to the selected transponder) will be installed. The A429 to Discrete Converter is looking for Arinc 429 label 353 (bit 20 - which
defines the ADS-B function status) and converts it to a discrete signal connected to ADS-B Fail annunciator light.