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BeechcraftTwin piston · Locarno, Ti, Switzerland

1978 Beechcraft 58P Baron

Price
$281,000
Year
1978
Total time
2,112 hours
Location
Switzerland

Specifications

General

Manufacturer
BEECHCRAFT
Model
58P BARON
Serial Number
TJ-148
Registration #
I-GIPA
Condition
Used
Flight Rules
IFR
Based at
Rome Ciampino

Airframe

Total time
2,112
Basic Empty Weight
9,896.55 lb
Complete Logs
Yes
Empty Weight
4489.3 Lbs
Moment
.39354.45

Propeller

Prop 1 Manufacturer
MCCAULEY
TSOH
11 hrs
Last overhaul
25/09/2014
TBO
2000 hrs/50 years
  • Propellers McCauley 3AF32521, sn 071550 and 071551
  • Installed new in July 2008 Per RAM Aircraft STC.

Avionics

WAAS
Yes
Inverter No. 1 (115/400 AC)
Flytronic
Inverter No. 2 (115/400 AC)
A.I.I.
  • 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
  • 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
  • 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.

Equipment

Oxygen System
Yes
Flight Into Known Icing (FIKI)
Yes
A/C
Yes
  • 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
  • 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

Number of Seats
6
  • 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

Maintenance

  • Airworthiness Review Certificate in progress, to be completed in January 2021
  • Last 100 hrs / annual inspection, to be completed in January 2021

Engine 1

Engine 1 Make/Model
CONTINENTAL TSIO520WB
Engine 1 Time
41 SFRM
Engine 1 TBO
1600

Engine 1 Notes

TSOH
41 hrs
Last overhaul
22/03/2011
TBO
1600 hrs/12 years (24 years in Italy)

Engine 2

Engine 2 Make/Model
CONTINENTAL TSIO520WB
Engine 2 Time
41
Engine 2 TBO
1600

Description

  • 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

Engine 1 Notes

Engines, Continental TSIO-520-WB, sn 518645 and 518649

Engine 2 Notes

Engines, Continental TSIO-520-WB, sn 518645 and 518649

Aircraft record

I-GIPA

Registration

Registration
I-GIPA
Registered as
Beech Baron 58P
Serial number
TJ-148

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