The use of automated external defibrillators (AED) is essential to increase the chances of survival in case of a cardiac arrythmias such as ventricular fibrillation (VF) and non-perfusing ventricular tachycardia (VT) when used in the first 10 minutes.

AMC1 CAT.IDE.A.220 (b) (4) stipulates that the aircraft operators should carry automated external defibrillator (AED) on board all aircraft equipped with a first-aid kit and required to carry at least one cabin crew.

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 the Honeywell Mark VI Enhanced Grounfd Proximity Warning System EASA.IM.A.S.01479 FAA STC SA00842WI-D

Installation of Collins TCAS-4000 Traffic Alert and Collision Avoidance System (TCAS-II).

Installation of Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS).

ATP aircraft - Provision of dual portable Electronic FlightBag (EFB)The installation of the EFB provision comprises of2 window mountsconsisting of a swivel and a tablet holder, 2 EFB control panels, onedata integration centre and 2 C/B’sfor 28VDC to the EFB systems.

Installation of Norton radome kit No. 2090XS.

Installation of Ground Utility Winterization Kit consisting of engine heaters, a battery warmer, cockpit heaters and a cabin outlet for a cabin heater.

Installation of Garmin GNS 430AW/GNS 530AW EASA.A.S.03768