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Piaggio P-180 Avanti II
Please Call
  • YEAR
    2010
  • LOCATION
    United States - FL, North America + Canada
  • S/N
    1210
  • REG
    N481BR
  • TTAF
    2,346

Aircraft Highlights

  • One owner since new
  • Low time
  • Late model
  • Fresh “B” Check & Maintenance complied though September 2017
  • Excellent paint & interior
  • Corporate use only!

AIRFRAME

TOTAL TIME AIRFRAME & ENGINES: 2,346
LANDINGS: 2,067

ENGINES

Pratt & Whitney PT6A-66B
3,600 Hour TBO (850 hp)

PROPELLERS:
Hartzell HC-E5N-3A/AL (5 – Blade)
Rockwell Collins Proline 21
Three 8”x10” Color Liquid Crystal Displays (LCD). The Primary Flight Displays (PFD) are located on the pilot’s and copilot’s panel with an Enhanced Multi-Function Display (MFD) on the center panel.

All displays can provide compass, radar information, and engine parameters. The MFD has enhanced capabilities and is able to display a variety of graphical information. The weather display may be overlaid on either the arc or map format. The PFD’s also display lateral navigation information in conjunction with the compass information.

Vertical deviation, distance, display, autopilot/flight director annunciations, and navigation bearings are also displayed on the PFD. Dual Collins AHC-3000 Attitude Heading Reference Systems supply attitude and magnetic or true heading information to the PFD. Engine parameters will be displayed at the top of the MFD, including N1, N1 reference, thrust mode, ITT, ignition selected annunciation, N2, oil temp, oil pressure, fuel quantity, fuel flow and fuel temperature. Below the engine display is a window which may display extended FMS data or an integrated electronic checklist. The lower portion of the MFD displays navigation in either a full compass rose, partial compass arc, present position (PPOS) map format or a planning map format. Situational awareness presentations (weather detection, TAWS, and TCAS) may be overlaid on either the arc or PPOS map formats.
Temperatures (TAS, RAT, SAT and ISA deviation) are displayed at the bottom of the MFD. Electronic approach and taxi charts and uplinked graphical weather may also be displayed on the MFD. The Collins Flight Management System FMS-3000’s provides multiple waypoint navigation solution blended from available GPS, VOR, and DME sources, suitable for en-route, terminal, and non-precision approach navigation. Both lateral and vertical modes may be displayed on the Flight Director and may be fully coupled to the autopilot. Airway flight planning, plain language identifiers and airport communication and navigation frequency lookup features are included. Present position referenced geopolitical and airspace boundaries, and airways may be overlaid on any
of the FMS formats. The CDU-3000 (Control Display Unit) provides an alternate method for controlling the radio sensors, in lieu of the RTU-4200 (Radio Tuning Unit). An optional Performance Data Base is available which will enable ground-based predicted performance, including automatic computation of takeoff reference speeds.

RADIO MANAGEMENT SYSTEM: Rockwell Collins RTU-4200, CDU-3000
COMMUNICATIONS: Dual Rockwell Collins VHF-4000 w/8.33 kHz spacing
VHF/ADF NAVIGATION: Rockwell Collins NAV-4000 VOR/ILS/MKR/ADF receiver
VHF NAVIGATION: Rockwell Collins NAV-4000 VOR/ILS/MKR receiver
FLIGHT GUIDANCE SYSTEM: Dual Rockwell Collins FGC-3003 Autopilot, Yaw Damper & Flight Director
EFIS: Rockwell Collins 3-Tube Integrated System
RADAR: Rockwell Collins RTA-852 Turbulence Detection Color Radar System
TRANSPONDER: Dual Rockwell Collins TDR-94D Mode S Diversity w/ Enhanced
Surveillance capability
DME: Rockwell Collins DME-4000 Distance Measuring Equipment
RADIO ALTIMETER: Rockwell Collins ALT-4000 Radar Altimeter
ELECTRONIC CHARTS: Rockwell Collins IFIS 5000 Chartlink permits displaying Jeppesen Electronic
Maps & Charts on MFD (subscription required)
AIR DATA COMPUTER: Dual Rockwell Collins ADC-3000 Air Data Computer
AHRS: Dual Rockwell Collins AHC-4000 Altitude Heading Reference System
FMS / GPS Rockwell Collins FMC-3000 Flight Management System/ Global
Positioning System
GPS SENSOR: Rockwell Collins GPS-4000A GPS Sensor
TCAS: L3 Communications Sky 899 (TCAS I) Terminal Collision
Avoidance System
TAWS: L3 Landmark TAWS 8000 (TAWS B) Terrain Awareness & Warning
System
ELT: Techtest Model 503 (3 frequency) Emergency Locator Transmitter
TELEPHONE: Aircel ST-3100 Phone
INTEGRATED FLIGHT INFORMATION SYSTEM: Rockwell Collins IFIS 5000
ELECTRONIC CHARTS: Rockwell Collins ECH 5000 & OVL 5000
VIP Corporate Interior – Option 3 floorplan (5 + 2 seats), 4 single passenger seats in club arrangement, 1 LH forward seat and RH forward 2-place divan with drawers, Aft fully enclosed lavatory with folding door, sink and water, flushing toilet with belted aft auxiliary passenger seat, dual foldout executive tables, pyramid cabinet with nice chest and miscellaneous storage, 110VAC power outlets in cockpit and passenger cabin, sheepskin covers for
cockpit seats.
Two-tone Paint Scheme, in Whisper Gray Lower, Matterhorn White with Burgundy Accent Stripes
P-180 MTOW Increase (12,100 lbs)
L3 Communications GH-3100 Standby Engine Cluster
Rockwell Collins MDC-3110 Maintenance Diagnostic System
Dual Clocks
Engine Fire Extinguisher
RVSM: Factory Standard
One Corporate Owner Since New
Professionally Managed & Operated
Always Hangared
No known damage history

Piaggio P-180 Avanti II

Please Call
  • YEAR
    2010
  • LOCATION
    United States - FL, North America + Canada
  • S/N
    1210
  • REG
    N481BR
  • TTAF
    2,346
User Image
Mark Connell
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