Авионика:
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
Оборудование:
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
Экстерьер:
White with Blue and Gold Accents, repainted by Kornprecht in Germany November 18, 2008 at TT: 7827:29
Condition 8/10
Интерьер:
Beige leather, beige carpet, 5 seats
Condition 6/10
Другие комментарии:
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, scheduled to be completed in October 2020
ARC to be renewed with annual inspection
Aircraft will be delivered with current annual inspection
Specifications subject to verification by purchaser
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
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
