1974 Beechcraft Baron 58

Matriculado argentino u$225.000

FICHA TÉCNICA:

  • 1974 Baron 58 s/n TH-511
  • MOTORES CONTINENTAL IO-520-C7B:
    #1: 287440-R DURG: 1124.7
    #2: 816855-R DURG: 748.0
  • HELICES HARTZELL PHC-J3YF-2CUF:
    #1: ED-391 DURG: 363.0
    #2: ED-5478B DURG: 362.0
  • 177 gal. GAMI injectors, Dual Yoke, VG’s, G430, Century IV AP, Bendix RDR 160, 406 MHz, ELT, Pulse Light.

CONTROLS:

  • Dual flight controls
  • Electrical pitch trim on left hand control wheel
  • Central console include

POWER CONTROL:

  • Propeller pitch control
  • Electric flaps control
  • Anual pitch trim
  • Ailerons trim
  • Rudder trim
  • Alternate static source control
  • Landing gear retraction and extension control

AIRFRAME:

  • Metal structure and skin paneling
  • Anti-corrosion protection treatment
  • Pitch control through elevator with trim
  • Yaw control through rudder with trim
  • Electric flaps
  • Bank control through ailerons and spoilers with trim on left aileron
  • Retractable gear with actuation
  • Hydraulic disc brakes
  • Large access door on the starboard aft side
  • Front storage compartment (not pressurized with external access door)
  • Emergency exit
  • Tie-down attachments
  • Jacking points

AIRFRAME TOTAL TIME:

  • 177,3 hours since new
  • Engines:  Cont. Engine IO-520-C Propeller:  Hartzell
  • Exterior: White with blue and red stripes.
  • Fuel: AV Gas
  • Oil: Aero shell 100 (12 quarts per engine)

LOADING:

  • Basic empty weight: 3721.90 lbs
  • Maximum ramp weight: 5400 lbs
  • Maximum takeoff weight: 5400 lbs
  • Useful Load:1664.10 lbs
  • Full Fuel:177 gallons

FUEL EQUIPMENT:

  • 2 bladder fuel tank per wing
  • Engine driven mechanical fuel pump
  • Standby electrical fuel pump
  • Fuel tank selector
Descargar Ficha Técnica