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Information About

Piaggio Avanti




The ''' produced by Piaggio Aero . It seats up to nine passengers in a generous Pressurized Cabin , and may be flown by one or two Pilots .


CONFIGURATION

The Avanti has Turboprop engines in a Pusher Configuration , placed on a mid- Fuselage , High Aspect Ratio Wing . The wing is located very far aft, behind the cabin, and the highly unconventional design also features a T-tail and a fixed foreplane (not technically a Canard , as it is not used to control the Pitch of the aircraft). This arrangement allows all three wing surfaces to provide lift in the upwards direction, as opposed to a conventional configuration, where the Horizontal Stabilizer creates a downward force, requiring the main wing to produce more lift to balance this force, and thus increasing Induced Drag . The Avanti's aerodynamics and turboprop engines result in an extremely efficient aircraft.

Distinctive design features include a non-constant cross section cabin, the shape of which is a figure of revolution based on a NACA Airfoil section. The mid cabin is therefore considerably wider than the cockpit, and the entire cabin sits ahead of the main wing spar. The wing and canard airfoils are custom sections designed by Dr. Jerry Gregorek of Ohio State University to achieve 50% Laminar Flow at cruise.


HISTORY

The P.180 was wind tunnel tested in Italy and the U.S. in 1980 and 1981. A collaboration with Learjet to develop the aircraft was begun in 1982, ending in 1986, when the prototype first flew. U.S. certification was obtained in 1990. The first 12 fuselages were built in Wichita , with H & H Parts and Plessey Midwest, then flown to Italy for assembly. Avanti Aviation Wichita ran out of money in 1994; the project languished until a group of investors led by Peiro Ferrari became involved in 1998 . The 100th aircraft was delivered in October 2005.

The P.180 makes a distinctive Square Wave noise when passing overhead, similar to the Beech Starship , due to wing wake and engine exhaust effects on the propeller.

A new ''Avanti II'' obtained European and US certification in November 2005. Seventy planes are already ordered (36 by Avantair ).


SPECIFICATIONS (P.180)

  jet Or Prop prop
  plane Or Copter plane
  include 'armament' Field no
  include 'capacity' Field yes
  switch Order Of Units no
  crew one or two pilots
  capacity up to nine passengers 1,999 lb (907 kg) payload
  length Main 1440 m
  length Alt 47 ft 2 in
  span Main 1403 m
  span Alt 46 ft
  height Main 13 ft 1 in
  height Alt 398 m
  area Main m&2
  area Alt ft&2
  empty Weight Main 3,400 kg
  empty Weight Alt 7,500 lb
  useful Load Main 1,862 kg
  useful Load Alt 4,105 lb
  max Takeoff Weight Main 5,262 kg
  max Takeoff Weight Alt 11,601 lb
  engine (prop) Pratt & Whitney Canada PT6A-66
  type Of Prop Turboprop s
  number Of Props 2
  power Main 1,107 kW
  power Alt 1,485 shp thermodynamic, derated to 850 shp
  max Speed Main 737 km/h
  max Speed Alt 398 kt
  cruise Speed Main 644 km/h
  cruise Speed Alt 348 kt
  range Main 2,595 km
  range Alt 1,400 nm) (one pilot, six passengers and IFR reserves
  ceiling Main 12,500 m
  ceiling Alt 41,000 ft
  climb Rate Main 1498 m/s
  climb Rate Alt 2950 ft/min
  loading Main kg/m&2
  loading Alt lb/ft&2
  power/mass Main kW/kg
  power/mass Alt 1465hp/lb




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  has Relations no
  has Lists yes
  see Also no