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Beech Baron 58P

Year of Manufacture: 1978 S/N TJ-148

Airframe Total Time 2105 hrs
Continental TSIO-520-WB
Rated 325 Hp from RAM
LH ENGINE TSO 35
RH ENGINE TSO 35
LH PROP 35 HOURS AS NEW
RH PROP 35 HOURS AS NEW

Avionics description
Information VOR/LOC GPS and Flight Plane 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 signal from PAV-80 and AUX MP3 files.

Avionics List:

Audio/marker: Garmin GMA-340
 COM/NAV/GPS1: Garmin GNS-430 (8,33 kHz)
 COM/NAV/GPS2: Garmin GNS-430 (8,33 kHz)
 COM 3: Honeywell KY-196A
 ADF: Honeywell KR-87
 DME: Honeywell KN-63
 Weather Radar: Honeywell RDR-2000
 Transponder: Garmin GTX-330 (Mode S)
 Multi function display: Garmin MX-20 with Jeppsen View
 Radio Altimeter: Free Flight TRA-3500/TRI-40
 Air data computer: Revue Thommen AD323235F (with TATprobe)
 Altitude encoder: TRANS-CAL SSD120-50A
 TAWS/RMI: Sandel ST-3400
 HSI 1: Sandel SN-3500
 HSI 2: Sandel SN-3500
 HSI 3: Bendix IN-831A
 Compass system 1: Bendix SG-832C
 Compass system 2: Bendix SG-832C
 Autopilot/Flight Director 3 axis Bendix FCS-810
 TCAS I: L3 Communication Sky-Watch 497
 Stormscope L3 Communication: WX-500
 ELT: Artex 406-N (Satellite GPS)
 Inverter No. 1 (115/400 AC): Flytronic
 Inverter No. 2 (115/400 AC): A.I.I.  Control wheels clock: 1 Davtron
 Control wheels clock: 2 Davtron
 DVD/FM/AM: PS-Engineering PAV-80
 External camera
 Audio Amplifier Avionics Innovation (four speakers stereo)

Equipment:

 Air Condition Freon system
 Full de-ice system
 Club seating arrangement
 Unfeathering accumulator
 2 Altimeters
 2 Horizon
 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

Notes:

Works performed:
2000 hours inspection
New propellers: July 2008 (STC RAM Aircraft)
Replaced: New batteries July 2012
Fresh annual check December 2014
Propellers and Regulators December 2014
Interior
Six seats club seating arrangement in the rear, light blue leather seats. Six intercom stereo BOSE headphone jacks

Exterior:

White with red and blue stripes