Beechcraft
1979 Beechcraft 58p
$179,000
1979 · 4,860 h · United States
Private seller
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-GIPARegistration
- Registration
- I-GIPA
- Registered as
- Beech Baron 58P
- Serial number
- TJ-148
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