Airframe

Total time

·

2,112 hr

MSN

·

TJ-148

Seats

·

6

Flight rules

·

IFR

Registry

·

Italy

Based at

·

Rome Ciampino

Powerplant

Engine

·

CONTINENTAL

Engine 1 SMOH

·

41 SFRM

Propeller

·

MCCAULEY MCCAULEY

Performance (across variants)

Range

·

1,080 nm

Cruise

·

247 kt

Service ceiling

·

32,000 ft

MTOW

·

2,800 kg

Passengers

·

Up to 6

Condition

Used

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.