Авионика:
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.
Оборудование:
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.
Экстерьер:
White with red and light blue accents
Интерьер:
6 Seats
Light blue leather seats, white and blue side panels
Light blue curtains
Club seating arrangement with courtesy table
Другие комментарии:
Empty Weight: 4489.3 Lbs
Moment: 39354.45
Weighed July 2013
Specifications subject to verification by purchaser.
TT: 2112 hrs
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)
Propellers 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.
Aircraft SN: TJ-148
