1981 Beechcraft Baron 58
| Overview | |
| 1981 Beech 58 Baron - Only 4,664 Hours Total Time Since New, 2248 Hours SFRM (LH & RH), 689 Hours Since New 3-Blade Propellers ( LH & RH), King KFC-200 Auto Pilot, Kin KAS-297 Altitude Pre-Select, Yaw Dampener, Flight Director, HSI, Garmin / AT GNX-80 WAAS Approved GPS, Garmin / AT MX-20 Multi-Function Dip lay, Gamin GTX-345 ADS-B IN and OUT Transponder, Co-Pilot Instrumentation, Dual Yoke, Dual EGT Gauges, Hoskins Fuel Computer, Factory FIKI Featuring a Windshield Hot Plate, Tanis Engine Pre-Heaters, Medco Door Locks, HID Lighting, Club Seating Featuring Leather! | |
| Price: |
$175,000 USD
Reduced by $30,000
(14.6%)
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| Offered By: | Bartelt Aviation |
| Registration: | N3739B |
| S/N: | TH-1198 |
| Location: |
Grand Rapids, Michigan United States 
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| Days Active: | 22 days ago |
| Airframe | |
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Airframe Notes INTERESTED IN FINANCING SOLUTIONS? Reach out to us for one-on-one personalized service. Attractive fixed rates with amortizations up to 20 years available. Low down payment options and customizable amortization schedules are also available. |
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| Total Time: | 4,664 Hours |
| Avionics | |
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King KFC-200 Flight Control System Featuring Heading Coupling and Altitude Hold King KAS-297 Altitude Pre-Select Yaw Dampener King KI-256 Flight Director Attitude Indicator King KI-525 HSI – (Slaved) PS Engineering PMA-8000-SR Audio Panel / 3 LMB / 6-Place Intercom Garmin / AT CNX-80 GPS / COM / NAV – (WAAS Approved) King KY-196 COM King KNS-81 RNAV King KN-63 DME Featuring Nav 1 and Nav 2 Switching King KR-87 Featuring a KI-229 RMI Garmin / AT MX-20 MFD / Moving Map Garmin GTX-345 Transponder / ADS-B Out Compliant Co-Pilot Altimeter Co-Pilot Directional Gyro Dual Electronics International Digital EGT Gauges Hoskins CFS-2000A Fuel Flow Computer Bose Headset Jacks - (6) |
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| Additional Equipment | |
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SUPER FEATURES / MODIFICATIONS / UPGRADES Factory De-Ice System – (FIKI) 3-Blade Hot Props Featuring Polished Spinners Windshield Hot Plate Fuselage Ice Protection Plates – (Custom Aircraft Products) Wing Ice Light Tanis Engine Pre-Heater / Engine Covers Medco Door Locks Control Wheel Clock (Digital) Propeller Synchronizer Knots 2-U HID Landing Lights / Precise Flight Pulse Lights Dual Control Yoke ADDITIONAL OUTSTANDING FEATURES Alternate Static Source Bracket Air Filters Upgraded Wing Tie Down Anchors Double Door / Baggage Door Locks Air Cargo Systems Certified Cargo Net / Anchor Plates Portable Scott Oxygen System LPG Upgraded Tinted Windshield and Side Windows Cabin Window Heat Shield Inserts Rotating Beacon (Vertical Fin) Wing Tip Strobes – (3 Light System) Nose Wheel Taxi Light Bracket Air Filters Cabin Fire Extinguisher External Powner Receptacle 100 Amp Alternators |
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| Engines & Props | |
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Engine 1 Engine 1 Make/Model - CONTINENTAL IO520CB Engine 1 Horsepower - 285 HP Engine 1 TBO - 1700 Engine 2 Engine 2 Make/Model - CONTINENTAL IO520CB Engine 2 Horsepower - 285 HP Props Prop 1 Manufacturer - MCCAULEY Prop 1 Time - 689 SNEW Prop 2 Manufacturer - MCCAULEY Prop 2 Time - 689 SNEW Number of Blades - 3 Prop Notes New Propellers Installed in 1999. |
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| Engine 1 Hours: | 2,248 SFRM |
| Engine 2 Hours: | 2,248 SNEW |
| Interior & Exterior | |
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Number of Seats - 6 Interior Notes Designer Schmidt Grey Leather Seating 6 Place Club Seating Configuration Executive Writing Table – (Stowable) Custom Sheep Skin Seat Covers - (6) |
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White Base Featuring Black and Gold Accents The aircraft is kept in a hangar when not flown. |
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| Other Info | |
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Inspection Status: ANNUAL DUE: Due October 1, 2026 BI-ANNUAL IFR CHECKS DUE: TBA / Fresh Inspections to be coordinated ADDITIONAL INFORMATION The aircraft was inactive between April of 1999 and September of 2025. Aircraft repairs were performed in September 1984 due to inadvertent gear retraction (Per Current Owner) during landing roll out. See airframe log book entry September 11, 1984 for complete details. The fluorescent penetrant and Eddy current inspection of the wing forward spar carry through forward and aft webs (LH & RH) was completed. See the December 13, 2013 airframe log book entry for complete details. The front carry-through structure reinforcement kit was installed on RH Forward Side per AD 09-08-14. See airframe log entry dated February 20, 2014. The RH elevator was repaired. See airframe log book entry dated October 5, 1998 for details. The current owner has several additional aircraft accessories that will be included with the sale of the aircraft. Please consult your sales representative for additional information. |
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