Beechcraft 55 Baron

CHF 83'669
€ 89'000

Quadro generale

Sommario
Tipo:	Propulsione singola
Costruttore:	Beechcraft
Modello:	55 Baron
Anno di costruzione:	1961
Numero di registrazione:	HB-GEA
Ubicazione/sede:	Svizzera
Prezzo:	€ 89'000 (~ CHF 83'669)
Tutti i dettagli

Rivenditore
Aeromeccanica S.A Aeroporto Cantonale di Locarno 6596 Gordola Svizzera Tel.: +41-91-2103128 Fax: +41-91-7450037
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Dettagli

Sommario
Tipo:	Propulsione singola
Costruttore:	Beechcraft
Modello:	55 Baron
Anno di costruzione:	1961
Numero di registrazione:	HB-GEA
Ubicazione/sede:	Svizzera
Prezzo:	€ 89'000 (~ CHF 83'669)

Avionica

Garmin GMA340 Audio Panel 2 each Garmin GNS430 NAV COM GPS Garmin GI106A NAV 2 Idnicator King KI204 VOR ILS Co-Pilot Garmin GTX330 Transponder S King KR87 ADF with RMI King KN62A DME King ED461 EHSI (Electronic HSI) King SG465 Symbol Generator King KSG105 Directional Gyro AIM289-4M3 Copilot Slaved Directional Gyro AIM254-11-A Flux Detector King KA51B Slaving Accessory King KMT112 Flux Detector ARC40910 Slaving Meter Castleberry 305-2BI Pilot DC Attitude Gyro Ameri King AK-350 Alticoder Winter Slip Indicator WX1000+ Stormscope Marathon PC50 Inverter 1 ARC DV20B Inverter 2 B703IFW Inverter Failure Light King KA33-01 Cooling Blower Mitchell Century IIIB Autopilot S-TEC ST-360 Altitude Preselect/Alerter Roll, Pitch and Trim Servos Turn Coordinator King KA118 and King KA57 Autopilot Adapters ST-500 AC/DC Converter P324R 24 Volts Alternator R25400 Voltage Regulators Kannad 406AF Compact ELT TRX1500A TAS Hand Microphone

Esterno
White with Blue and Gold Accents, repainted by Kornprecht in Germany November 18, 2008 at TT: 7827:29 Condition 8/10

Interiore
Beige leather, beige carpet, 5 seats Condition 6/10

Altre segnalazioni

Maximum Take Off Weight: 4880 lbs Empty Weight: 3666.09 LBS 140 USG (530 Liters) fuel capacity December 1981 at TT: 5202:07 hours, 3 fuel cells, main left hand and two auxiliary replaced December 2007 at TT: 7821.1, Replaced both ailerons, both elevators and right elevator trim rod with new parts in accordance with FAA STC SA02172CH January 2009 at TT: 7827.29, Replaced wing bolts June 2015 at TT: 7905:43 Inspected wing bolts June 2020 reinspected wing bolts Engine mounts removed, inspected and reinstalled at engine overhaul 1000 hours inspection performed April 7, 2001 at TT: 7120:10 hours During annual inspection in 2020: Removed all worn out surface de-ice boots Removed and reinstalled fuel bladder tanks for internal wing inspection and leak check Refurbished bulkhead upholstery Inspected wing bolts Exhaust system of both engines overhauled by Gomolzig Annual inspection in progress, not completed ARC expired See photos of work in progress: Windshield currently removed for resealing Landing light lenses removed for refurbishment Avionics and instruments partially removed to allow windshield removal and reinstallation Interior side panels removed for replacement of insulation with new type. New insulation available with the aircraft Wing bolts replacement due. New bolts available with the aircraft Specifications subject to verification by purchaser

Very nice oldtimer! First production year of the Baron 55 Cruising speeds: 225 mph at 75 percent power (2450 rpm) at 7,000 feet 220 mph at 65 percent power (2450 rpm) at 10,500 feet 1,225 miles range (45% power, 10,000 ft., 140 gal.) (Includes full allowance for fuel used during warm-up, taxi, take-off and climb to altitude with a 45-minute fuel reserve at maximum-range speed) Rate of climb at sea level (rated power) 1,700 fpm, two engines at 4,880 lbs 340 fpm, single engine at 4,880 lbs 455 fpm, single engine at 4,500 lbs 660 fpm, single engine at 4,000 lbs Service ceiling (rated power) 20,000 ft, two engines at 4,880 lbs 7,600 ft, single engine at 4,500 lbs 10,850 ft, single engine at 4,000 lbs 76 mph stall speed (zero thrust), flaps 28 deg. down 910 ft take off distance (20 deg. flaps) ground run At sea level, zero wind, standard temperature) 1,175 ft landing distance (28 deg. flaps) grond run

Serial Number TC-64 Imported from USA to Switzerland in July 1969 with 3402:00 hours TT: 7960 hours Engines, Continental IO-470-L, SN: CS-91831-4-L, 260 HP at 2625 RPM Manufactuerd in 1965 TT: 4437 hours TSOH: 96 hours Overhauled October 4, 2012 with new Continental cylinder kits TBO: 1500 hours Crankshaft replaced in June 2000 at TT: 3304:01 according MSB 00-5B Engines, Continental IO-470-L, SN: 297884-R Factory rebuilt in 1999 TT: 1516 hours TSOH: 96 hours Overhauled October 4, 2012 with new Continental cylinder kits TBO: 1500 hours 3 Bladed Propeller Harthell PHC-C3YF-2UF, SN: EB7659B Manufactured in 2012 Installed new in April 2013 TT: 96 Hours

Long range fuel tanks Later style nose Co-Pilot Brakes Dual Control Joke Janitrol Cabin Combustion Heater Propeller Alcohol Anti-Icer Surface De-Ice Boots with pressure container in the nose baggage compartement, currently inoperative. Boots have been removed Airwolf Oil Filter Kit AFC-K008-C, STC SA00079N4 installed on both engines Rosen Sun Visors Single Piece Windshield, Great Lakes FAA STC SA95GL Tinted Windows Cleveland main wheels and brakes, FAA STC Ailerons, Elevators, Elevator Trim Rod, FAA STC SA02172CH