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

ADS-B out Replacement / Upgrade of the existing single or dual transponder to include ADS-B functionality according to Minimum Operational Performance Standards.

This module is extremely versatile and has numerous STCs in fixed and rotor wing aircraft. This system is lightweight, compact and fits smaller aircraft, yet has critical care capabilities for larger aircraft as well. 

Installation Air Ambulance Conversion Cessna 525, 525a, 525B and 525C

Spectrum Aeromed is recognized as a world leader in creating customized and durable, highly functional air medical transport equipment that complies with aviation regulations. All engineering and design of our air ambulance life support systems comes from working hand-in-hand with air medical personnel worldwide.

GARMIN GPS 400W/500W installationRevision 1 supersedes the previous issue of this STC to delete the modelS550 from the applicability list for correction. Certification Basis Certification Basis as per EASA TCDS IM.A.207 Issue 2 from 5 March 2009 Limitations Master Document List "2054628 DOC" issue 1 from 17 August 2009Aircraft Flight Manual Supplement "2054628-AM" issue 1 from 11 August2009Instructions for Continued Airworthiness "2054628-CA" issue 1 from 11August 2009or later revisions of the above listed documents approved by EASA Conditions The limitations according to Aircraft Flight Manual Supplement2054628-AM are applicable.

Installation of Rockwell Collins, Inc. Aircraft Information Management (AIM) System

Modification of a Rockwell Collins, Inc. File Server Unit (FSU)

Modification of Rockwell Collins, Inc. VHF-4000 and VHF-4000E installations

Installation of Garmin GTN 725

Modification of a Rockwell Collins, Inc. Global Positioning System (GPS)installation