1978 Beechcraft 58P Baron Multi Engine

Airframe

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.

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 & copilot instrument panel & it is coupled to all 3 HSI’s

Sandel ST3400 TAWS/RMI

King KN63 DME, coupled to its indicator & both Sandel 3500’s

King KR87 ADF, coupled to both Sandel 3500’s

Free Flight TRA3500/TRI40 Radar Altimeter with digital indication & altitude alerter with its indicator & 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 & 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 &airspeed indicator

Avionics Master

Ground avionics master switch for COM1 & 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 & 2 can be visualized either on HSI 1, HSI 2, RMI 1 & Multifunction Display together or separately.

TCAS information & stormscope can be visualized on MFD & HSI 1/2 & TAWS.

MX-20 has Jeppesen View capability & can display approach & airport charts.

Autopilot Heading & NAV modes can be coupled with HSI 1, 2 & 3 performing complete SID, STAR & Flight Plan.

TV camera is located in the bottom of the tail cone viewing front/down & gear & propellers too.

The stereo system is six headphone/interphone (BOSE System) & can accept signals from PAV-80 & AUX MP3 files.

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 & 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 & blue side panels

Light blue curtains

Club seating arrangement with courtesy table

Exterior

White with red & light blue accents

Additional Info

Empty Weight: 4489.3 Lbs

Moment: 39354.45

Weighed July 2013

Annual inspection & ARC will be renewed prior delivery.