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.

Installation of Airfield Technology AT-950 Flight Inspection System (FIS)

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. 

Air Ambulance Conversion according FAA STC SA02897CH. Certification Basis The Certification Basis for the original product remains applicable tothis certificate/ approval.CS 23 as defined in CRI A-01 and indicated in TCDS EASA.IM.A.502The requirements for environmental protection and the associatedcertificated noise and/ (...) Limitations Installed iaw. Spectrum Aeromed Master Drawing List 6053DL,dated 21 Apr2010Operated iaw. FAA approved AFM-S 6053FMS, dated 26 Oct 2010Maintained iaw. FAA accepted Inst. for ContAW, Manual 6053MM, dated 21Apr 2010or later revisions of the above liste (...) Conditions According limitation section of AFM-S.

Installation of a monorail sunvisor system in accordance with Drawing List 1970000-DL, Revision D, dated April 8, 2011, FAA approved May 24, 2011, or later FAA approved revision.

Modification of the aircraft interior to allow for two configurations, 1.) Observer configuration and 2.) back to the Type Certificated standard Executive configuration in accordance with Straight Flight Master Drawing List Document No. 4979-MDL-01, Revision B, dated June 15, 2010, or later FAA approved revision.

Installation of a Crane Aerospace & Electronics Tire Sensor Assembly

Modification of the aircraft interior to allow for two configurations:1) Observer configuration and2) back to the Type Certificated standard Executive configuration inaccordance with Straight Flight Master Drawing List Document No.4979-MDL-01, Revision B, dated June 15, 2010, or later FAA approvedre...