Piaggio P.180 Avanti

P.180 Avanti
Role Executive transport
National origin Italy
Manufacturer Piaggio Aero
Designer Alessandro Mazzoni [1]
First flight 23 September 1986
Introduction 30 September 1990
Status In production
Primary users Italian Air Force
Italian Army
Italian Navy
Avantair (ceased 2013)
Produced 1986–present
Number built 236 (Oct 2018)[2]
Unit cost
US$7.7 million (Avanti EVO, 2017)[3]

The Piaggio P.180 Avanti is an Italian executive transport aircraft with twin turboprop engines mounted in pusher configuration.[4] It seats up to nine people in a pressurized cabin, and may be flown by one or two pilots. The design is of three-surface configuration, having both a small forward wing and a conventional tailplane as well as its main wing, with the main wing spars passing behind the passenger cabin area.

Development

Piaggio P.180 Avanti II empennage and delta fins (only one visible)
Avanti II flight deck
Clean configuration

A 1980s wave of new-generation planes, developed to appeal to Fortune 500 clients, included Piaggio's Avanti and Beech Aircraft Corp.'s very similar Starship.[5][6] Engineering studies for the airplane that would eventually be named Avanti began in 1979 and designs were tested in wind tunnels in Italy and the United States in 1980 and 1981, conducted by Professor Jan Roskam from the University of Kansas (using Wichita State University's wind tunnel and Boeing's transonic wind tunnel in Seattle)[7] along with Professor Gerald Gregorek at Ohio State University (using OSU's 2D pressure wind tunnel).[8][9]

Piaggio's chief engineer, Alessandro Mazzoni,[10] filed in 1982 to patent the Avanti design.[1][11] Beginning in 1983, Gates Learjet partnered with Piaggio to develop a fuselage for the new aircraft (referred to as Gates Piaggio GP-180).[12][13] Learjet's design influence can be seen in the steeply raked windshield and the two large ventral delta fins under the tail.[14] At high angles of attack these delta fins provide a nose-down pitching moment and help to avoid a potential stall,[15][16][17] and they increase stability in flight by damping yaw and Dutch roll.[4]

Gates Learjet's financial problems ended their collaboration in January 1986, but Piaggio continued the project,[14] and the first prototype flew on 23 September 1986.[18] The P.180 Avanti received Italian certification on 7 March 1990[19][20] and American certification was obtained on 2 October 1990.[21][22]

The first 12 fuselages were manufactured in Wichita, Kansas, with H & H Parts and Plessey Midwest, then flown to Italy for final assembly.[19] Avanti Aviation Wichita ran out of money in 1994; the project languished until a group of investors led by Piero Ferrari became involved in 1998. The 100th aircraft was delivered in October 2005 and the 150th in May 2008. Piaggio reported that, as of October 2010, the Avanti and Avanti II fleets had logged over 500,000 flying hours.[23]

An improved Avanti II obtained European and U.S. certification in November 2005. Six months later, 70 planes had been ordered, including 36 by Avantair. Avanti II received type approval for Russia in 2011.[24] The Avanti II featured uprated Pratt & Whitney Canada PT6A-66B turboprop engines and flies about 18 km/h (11 mph) faster, with better fuel economy; and an all-new "glass panel" avionics suite from Rockwell Collins reduced cockpit clutter.[25][26] In addition to heading, attitude and navigation information, flat panel color liquid crystal displays add collision avoidance (TCAS), ground proximity (TAWS) and real-time graphic weather depiction.[27]

The Avanti is marketed as being faster than other turboprops and many midsized jets, with cost efficiency as much as 40 percent better than market-competing jets, as a result of less drag and a lower fuel burn rate.[28][29] Powered by the same Pratt & Whitney Canada PT6A-66 engines as the Beechcraft King Air B200, the Avanti II is 100 knots (190 km/h; 120 mph) faster than that model King Air.[30] Flying magazine judged the Avanti to be the "Fastest Civilian Turboprop Twin" in 2014, saying "Avanti's speed is pretty much on par with Cessna's M2, while providing more space and a lower operating cost."[31]

The first Avanti EVO manufactured at the new $150 million factory at Albenga Airport was delivered in 2016, one year after moving production from its previous Genoa Cristoforo Colombo Airport plant.[32]

Design

The Avanti's turboprop engines are placed on a mid-set, high aspect ratio wing located just behind the cabin. The three-surface design incorporates both a T-tail and a pair of small, fixed forewings having slight anhedral and landing flaps. On the Avanti II these flaps automatically deploy in concert with the main wing flaps. This reduces the load on the tailplane, even when the flaps are deployed, by reducing the pitch-down moment created by the deployment of the main wing flaps. This in turn allows the size of both the tailplane and the main wing to be reduced.[33][34][35][36] This particular three-lifting-surface configuration was patented in 1982.[1]

The Avanti’s forward wing flaps deploy automatically with the main wing flaps to maintain neutral pitch trim.

The forward wing's angle of incidence is slightly greater than that of the main wing, so that it stalls before the main wing, producing an automatic nose-down effect prior to the onset of main wing stall; its five-degree anhedral (negative dihedral) keeps the stream wash interference clear of the engine inlets, the main wing and the tailplane.[34]

Showing the continuously-varying curve of the fuselage cross-section and forward wing

The cabin cross-section varies continuously along the length of the aircraft; the shape approximates an NACA airfoil section, and the slowly changing curve helps prolong laminar flow on the front of the fuselage. Piaggio claims that the fuselage contributes up to 20% of the Avanti's total lift, with the front and rear wing providing the remaining 80%. Due to the unusual fuselage shape, the mid cabin is considerably wider than the cockpit. The front and rear airfoils are custom sections designed by Jerry Gregorek[37] of Ohio State University's Aeronautical and Astronautical Research Laboratory to achieve a drag-reducing 50% laminar flow at cruise. The company claims the overall design of the P180 Avanti II enables the wing to be 34% smaller than on conventional aircraft.[38]

Cabin

The P180 is said to have good fuel efficiency relative to small turbojets flying in the same speed and altitude range. Flight International stated: "The Avanti has no direct turboprop competitors, its closest jet rivals are the Raytheon Premier I and the Cessna Citation CJ2+ ... Piaggio says low-drag laminar flow is maintained to around 50% of the wing chord, compared with around 20–25% for conventional tractor turboprops where propeller wash disturbs the airflow over the wing... specific air range at high altitude is 3.4km/kg (0.84nm/lb) compared with around 2km/kg (0.49nm/lb) for current jets or 2.7km/kg (0.67nm/lb) for other turboprops."[39] By this estimate, mileage is 70% better per fuel unit than comparable jet aircraft, although this greater efficiency is achieved only at a relatively slow 315 KTAS and FL410.[40] P180 Avanti II Specifications now show slightly lower numbers for specific range of 3.1 km/kg (0.76 nm/lb).

Interior noise is lower than conventional turboprop aircraft, because the propellers and engine exhausts are behind the cabin. Piaggio quotes 68 dBA. However, due to the strongly disturbed flow in which the pusher propellers operate, the exterior noise is higher. The exterior noise level and its higher pitched sound has been shown to be the result primarily of the interaction of the turbine engine exhaust flows and the five-bladed pusher propellers (est. +9 dB).[41] On takeoff, the Avanti has been measured at 81.9 dBA sideline noise level, slightly lower than the Beechcraft King Air at 82.8 dBA. This is below FAA stage 3 noise limits, which set a maximum of 89 EPNdB for takeoff.[42][43] However, the P180 has been the subject of noise complaints at airports, such as Aspen–Pitkin County Airport in Colorado[44] as well as Naples Municipal Airport, Florida, where that airport authority determined it was the noisiest aircraft using the facility.[45] Alan Parker, chairman of the Naples Municipal Airport Authority's technical committee, described the Avanti as "irritating loud" and compared the high pitched sound "to fingernails on a chalkboard".[46]

The Piaggio P.180 Avanti has a sea level, standard day, maximum gross weight takeoff distance of 869 m (2,851 ft) and a landing roll of 872 m (2,861 ft).[47]

Deliveries were at a high of 30 in 2008, but only two in 2013.

In 2014 Piaggio announced development of an updated version, called EVO.[48] It uses new Hartzell composite propellers, with blades of scimitar configuration. Its wings carry new winglets; aerodynamic improvements have been incorporated, and an additional 60-gallon (400 lb) fuel tank option to increase range to 1,770 nautical miles (3,280 kilometres; 2,040 miles).[49][50] The company predicts improved climb performance, 250 nm greater range, and 3% reduction in fuel usage. The revised propeller shape, combined with a lower engine speed, promises a 68% reduction in external noise. Avanti EVO type certification was granted by EASA on 28 November 2014,[51] and by the FAA on 6 July 2015.[52] Although projected purchase price was in the $7.4 million range,[53] by May 2017 the actual price was approximately $7.7 million.[54] The first EVO was delivered in April 2015, with five more to follow the same year.[55]

Variants

Two Avantis leaving assembly for testing
P.180 Avanti
First production variant.
P180 M
Military version with a combination passenger/freighter configuration for use as a VIP and light utility transport.
P.180 RM
Variant for use in radio calibration.
P.180 AMB
Air ambulance variant.[56]
P.180 APH
Aerial cartography.
P.180 Avanti II
Variant with improved avionics and engines.[20]
EVO
Variant with 400kt TAS and higher useful load.[57]
Multirole Patrol Aircraft (MPA)
Initially called Maritime Patrol Aircraft, MPA is a variant of the Avanti II with a larger wingspan and bigger fuel tanks.[58] As with the EVO propulsion system, MPA uses more powerful Pratt & Whitney Canada PT6A-66B engines and Hartzell five-blade scimitar propellers.[59] MPA electronics include the Albatros mission mystem from Saab Group and Pro Line Fusion avionics from Rockwell Collins.[60]
P.1HH HammerHead at Paris Air Show 2013
Piaggio-Selex P.1HH Hammerhead
Medium-altitude long-endurance unmanned aerial vehicle based on the Avanti II airframe, with an increased wingspan and the ability to carry up to 1,100 pounds (500 kg) of weapons.[61] The P.1HH HammerHead Mission Management System is based on the Selex ES (now Leonardo S.p.A.) skyISTAR solution.[62][63] The vehicle's first flight took place in December 2013 from Trapani–Birgi Italian Air Force base.[64][65][66]
The Italian Air Force signed an agreement with Piaggio Aerospace to buy three Unmanned Aerial System P.1HH HammerHead (six aircraft and three ground control stations) with delivery starting from the early months of 2016.[67][64][65] United Arab Emirates Air Force ordered eight P.1HH aircraft.[68][69] On May 31, 2016 the first P.1HH prototype crashed off the Sicilian coast,[70][71] delaying flight testing for thirteen months during construction of a second prototype. Piaggio flew the second prototype at Birgi military airport on 5 July 2017[72] The UAE will take delivery of six P.1HHs in 2018 and the remaining two in 2019: the first European MALE UAV.[73]
P.2HH
Piaggio develops with Leonardo, the Italian and UAE Armed Forces a P.1HH successor for 2023, with a new wing, more composite materials, and re-thought systems.[73]

Operators

Civil

The Avanti is operated by charter companies and small feeder airlines, and is also used as a business aircraft. The fractional aircraft operator Avantair was Piaggio's largest client, with a fleet of 57 Avanti aircraft,[28] before they went bankrupt and the fleet was liquidated.[74][75]

In May 2017, 220 aircraft were in operation around the world,[76] with 89 being first-generation Avanti, 126 second-generation Avanti II and 6 Avanti EVO models.[77]

A Piaggio Avanti San Diego-to-Charleston flight in 2003, piloted by Joe Ritchie with co-pilot Steve Fossett, set National Aeronautic Association and Fédération Aéronautique Internationale transcontinental speed records with an average speed of 475.2 knots (880.1 km/h; 546.9 mph),[78] breaking the previous Los Angeles to New York turboprop record of 395.21 knots set by Chuck Yeager in 1986 in a Piper Cheyenne 400LS. Elapsed time for the Avanti’s coast-to-coast trip was 3:51:52.[79]

Government

Bulgaria
Canada
Italy
Poland
  • Polish Medical Air Rescue (LPR) – 2 (1 x Avanti, 1 x Avanti II)[93]
Russia
  • Federal State Unitary Enterprise "State ATM Corporation" – 1 (1 x Avanti II)[94]
United Arab Emirates

Specifications (P180 Avanti EVO)

Planform view of the Avanti, highlighting its unusual design
Front view

Data from Aviation Week[97]

General characteristics

  • Crew: 1
  • Capacity: 7–9
  • Length: 14.4 m (47.3 ft)
  • Wingspan: 14.0 m (46.0 ft)
  • Height: 4.0 m (13.0 ft)
  • Wing area: 16.0 m2 (172 sq ft)
  • Aspect ratio: 12.3
  • Empty weight: 3,799 kg (8,375 lb)
  • Max takeoff weight: 5,488 kg (12,100 lb)
  • Fuel capacity: 1,271 kg (2,802 lb)
  • Max Landing weight : 5,216 kg (11,500 lb)
  • Max Zero Fuel weight : 4,445 kg (9,800 lb)
  • Cabin : 17.5 ft long, 5.8 ft high, 6.1 ft wide (3.5 ft floor)
  • Foreplane area: 2.19 m² (23.59 ft²)[34]
  • Horizontal stabilizer area: 3.83 m² (41.27 ft²)[34]
  • Powerplant: 2 × Pratt & Whitney Canada PT6A-66B turboprop, 630 kW (850 shp) each ISA+28C Flat Rated

Performance

  • Maximum speed: 741 km/h; 460 mph (400 kn) FL310 high speed cruise
  • Cruise speed: 589 km/h; 366 mph (318 kn) FL410 long range cruise
  • Minimum control speed: 185 km/h; 115 mph (100 kn) Vmca
  • Range: 2,797 km; 1,738 mi (1,510 nmi) 4 passengers, NBAA IFR, 100-nm alternate
  • Ferry range: 2,834 km; 1,761 mi (1,530 nmi)
  • Service ceiling: 12,000 m (41,000 ft)
  • Time to altitude: 10 min to FL 250
  • Wing loading: 343 kg/m2 (70.3 lb/sq ft)
  • Fuel consumption: 0.220 kg/km (0.779 lb/mi)
  • Power/mass: 230 W/kg (0.14 hp/lb)
  • Takeoff (SL, ISA) : 994 m (3,262 ft)

See also

Aircraft of comparable role, configuration and era

Related lists

References

Notes
  1. 1 2 3 US patent 4746081, Mazzoni, Alessandro, "Aircraft having three lift surfaces", published 1982-05-27, issued 1988-05-24, assigned to Industrie Aeronautiche e Rinaldo Piaggio S.p.A.
  2. Murdo Morrison (12 Oct 2018). "NBAA: Business jet designs that changed the industry". FlightGlobal.
  3. Fred George (May 2017). "2017 Business Airplanes Purchase Planning Handbook" (PDF). Business & Commercial Aviation. Penton. p. 91.
  4. 1 2 "Fuel Miser". Flying Magazine. 30 December 2008. Retrieved 15 January 2012.
  5. Weiner, Eric (5 June 1989). "Innovative Plane Making Its Debut". The New York Times. Retrieved 22 June 2017. Like the Starship, the Piaggio Avanti features a canard and rear-mounted engines. But the Avanti is made mostly of aluminum, not composites. It weighs thousands of pounds less than the Starship and is about 60 m.p.h. faster.
  6. Martin, Ed (29 October 1989). "Business Jets Ready For Takeoff". Chicago Tribune. Knight-Ridder Newspapers. Retrieved 19 June 2017. This is the futuristic Piaggio Avanti. It, and a handful of other avant-garde designs like it are leading American business aviation into the 1990s.
  7. "Dr. Jan Roskam Project Advisor". DARcorp. Design, Analysis and Research Corporation. Retrieved 22 June 2017. Jan Roskam managed the low speed and transonic speed windtunnel programs for the SIAI Marchetti S-211 and Piaggio 180-Avanti.
  8. Roskam, Jan (2002). Roskam's airplane war stories : an account of the professional life and work of Dr. Jan Roskam, airplane designer and teacher. Lawrence, Kan: DARcorporation. pp. 195–198. ISBN 9781884885570.
  9. Cozzolino, A. (20 June 2006). "Research Investment & Commercial Success : Piaggio Aero Industries" (PDF). Sustainable Solutions for New Horizons. Fifth Community Aeronautics Days. Vienna: BMVIT. pp. 11–13. Retrieved 22 June 2017.
  10. "Dr. Alessandro Mazzoni". M3 Aviation Inc. Retrieved 22 June 2017. As Director of Engineering for I.A.M. Rinaldo Piaggio from 1974 to 1991, he designed the P.180 Avanti, and is the US Patent holder (4746081) for the Three Lifting Surface Configuration (3LSC) aircraft.
  11. US patent D280892, Mazzoni, Alessandro, "Aircraft ornamental design", published 1982-06-10, issued 1985-10-08, assigned to Rinaldo Piaggio S.p.A.
  12. Kleinfield, N. R. (14 December 1984). "BUSINESS PEOPLE; GATES LEARJET PICKS 2-DIVISION MANAGER". The New York Times. Retrieved 22 June 2017. Mr. Neal… …will also direct and coordinate the company's role in developing the new Gates Piaggio business aircraft, designated the GP-180.
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  35. Aircraft Configuration Study for Experimental 2-Place Aircraft and RPVs, DTIC, March 1990
  36. Des couacs chez les canards [Quacks in the canards (ducks)] (diagram) (in French), FR, page bottom
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  38. "Efficiency", P.180, Piaggio Aero, archived from the original on 7 May 2006
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  44. Urquhart, Janet (9 September 2011). "Aspen airport gets earful about noisy airplane". Aspen Times. Retrieved 12 June 2017. Operation of the P180 has climbed onto lists maintained by the airport, which tracks noise events and noise complaints, though the aircraft is actually quieter, in terms of decibels, than some private jets, according to Paul Dunholter, noise consultant for the airport. It’s the pitch that’s noticeable.
  45. Miguel-Navarro, Tracy X. (25 April 2010). "Naples airport addressing noise complaints with Avanti aircraft". Naples Daily News. Retrieved 14 December 2011.
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  60. Tomkins, Richard (16 November 2016). "New multirole aircraft shown by Piaggio Aerospace". UPI. Retrieved 13 June 2017. Piaggio Aerospace has rolled out a new multi-role aircraft it is developing with a company from the United Arab Emirates.
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