Aircraft

Aeromeccanica, SA
Aeroporto Cantonale
Gordola  SWITZERLAND
Aircraft Summary
  • Very nice pressurized Baron!
  • Always hangared and in Italy since new
  • Private aircraft
  • Will be sold with valid annual inspection and ARC, in completion November 2024
  • Specifications subject to verification by purchaser


    Airframe:
  • Total Time: 2,112


    Engines:
  • Continental TSIO-520-WB, sn 518645 and 518649
  • TSOH: 41 hrs
  • Last overhaul: 22/03/2011
  • TBO: 1600 hrs/12 years (24 years in Italy)


    Props:
  • McCauley 3AF32521, sn 071550 and 071551
  • TSOH: 11 hrs
  • Last overhaul: 25/09/2014
  • TBO: 2000 hrs/50 years
  • Installed new in July 2008 Per RAM Aircraft STC.
Avionics
  • GMA340 Audio Panel, Marker Beacon
  • Avidyne IFD-440, 8.33 kHz, 760 channels NAV COM GPS WAAS, touchscreen, WiFi
  • 1 Garmin Garmin GNS430, 8.33 kHz, 760 channels NAV COM GPS NON WAAS
  • King KY196A COM 3, 16 Watts, non WAAS
  • King RDR2000 Color Radar
  • Garmin GTX330 Mode S Transponder
  • Garmin MX20 MFD with Jepp View and Radar Indicator
  • Sandel SN3500 HSI 1
  • Sandel SN3500 HSI 2
  • Bendix IN831A HSI 3
  • Bendix SG832C Compass System 1
  • Bendix SG832C Compass System 2
  • Bendix FCS810 3 Axis Autopilot/Flight Director, Yaw Damper,
  • Altitude preselect, can be operated from both pilot and copilot instrument panel and it is coupled to all 3 HSI's
  • Sandel ST3400 TAWS/RMI
  • King KN63 DME, coupled to its indicator and both Sandel 3500's
  • King KR87 ADF, coupled to both Sandel 3500's
  • Free Flight TRA3500/TRI40 Radar Altimeter with digital indication and altitude alerter with its indicator and coupled to both HSI's
  • Revue Thommen AD323235F Air Data Computer with TAT Probe
  • Trans Cal SSD150-50A Altitude Encoder
  • Shadin Digital Fuel Computer
  • L3 Communication Sky-Watch 497 TCAS I, coupled to both Sandel 3500's
  • L3 Communication WX500 Stromscope, coupled to both Sandel 3500's and on Multi Function Display
  • Artex 406N ELT with Satellite GPS
  • Davtron Clock on Pilot Control Yoke
  • Davtron Clock on Co-Pilot Control Yoke
  • PS-Engineering PAV80 DVD/FM/AM
  • External Camera on tail displaying the landing gear and panorama, with display on headliner, installed with FAA STC
  • Avionics Innovation Audio Amplifier (4 speakers stereo)
  • 2 Attitude Indicators
  • 2 Altimeters
  • Inverter No. 1 (115/400 AC): Flytronic
  • Inverter No. 2 (115/400 AC): A.I.I.
  • Copilot altimeter and airspeed indicator
  • Avionics Master
  • Ground avionics master switch for COM1 and Audio for ground clearance
  • Independent warning system for de-ice system, pitot heat, fuel vent heat, stall warning heat, windshield heat. Warning light indicate if these systems are left on on ground
  • Propeller warning, low thrust detector

  • Avionics description:
  • Information VOR/LOC GPS and Flight Plan 1 and 2 can be visualized either on HSI 1, HSI 2, RMI 1 and Multifunction Display together or separately.
  • TCAS information and stormscope can be visualized on MFD and HSI 1/2 and TAWS.
  • MX-20 has Jeppesen View capability and can display approach and airport charts.
  • Autopilot Heading and NAV modes can be coupled with HSI 1, 2 and 3 performing complete SID, STAR and Flight Plan.
  • TV camera is located in the bottom of the tail cone viewing front/down and gear and propellers too.
  • The stereo system is six headphone/interphone (BOSE System) and can accept signals from PAV-80 and AUX MP3 files.
Modifications and Conversions
  • RAM 325HP ENGINES
  • Surface deice
  • Air conditioning
  • Courtesy table
  • Headset connectors for each occupant
  • Oxygen system
  • Strobe lights
  • Go around switch
  • Unfeathering accumulators
  • Instruments light
  • Control wheel map lights, mike button and ident
  • Double pitot system eating
  • Dual control yoke
  • Oxygen system
  • 196 GA fuel system
  • Strobe 3 lights system
  • Tail light system
  • Propeller thrust detector
  • De-icing warning ground system
  • Mc Cauley propellers, low vibration
Additional Equipment
  • Surface deice, FIKI
  • Air conditioning
  • Courtesy table
  • Headset connectors for each occupant
  • Oxygen system
  • Strobe lights
  • Go around switch
  • Unfeathering accumulators
  • Instruments light
  • Control wheel map lights, mike button and ident
  • Double pitot system eating
  • Dual control yoke
  • Oxygen system
  • 196 GA fuel system
  • Strobe 3 lights system
  • Tail light system
  • Propeller thrust detector
  • De-icing warning ground system
  • New propellers Mc Cauley low vibration.
Interior
  • 6 Seats
  • Light blue leather seats, white and blue side panels
  • Light blue curtains
  • Club seating arrangement with courtesy table
Exterior
  • White with red and light blue accents
  • Remarks
    • Airworthiness Review Certificate in progress, to be completed in January 2021
    • Last 100 hrs / annual inspection, to be completed in January 2021
    • Specifications subject to verification by purchaser