2007 PIAGGIO AVANTI II

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1 PIAGGIO AVANTI II (P180) ASKING PRICE: US$ 2,650,000 YOM 2007 MSN 1133 Background/History Development of the Piaggio P180 Avanti dates back to program launch in Gates Learjet became involved in the project in 1983, but withdrew for economic reasons in Piaggio assumed total control of the program and all tooling was transferred to Italy. The first prototype flew in 1987 and the type was certified by Italian authorities in March 1990.The first production aircraft was rolled out in May 1990 and US FAA certification was granted in October First customer deliveries began in September The innovative Avanti, with its jet-like performance and turboprop-like operating costs, was unfortunately a slow seller in spite of its modern features and advanced design. Production was halted in the mid-90s but the aircraft was re-introduced to the marketplace in 2000 with deliveries beginning once again. The Avanti II was certified by the European Aviation Safety Agency (EASA) in October 2005 and the first aircraft was delivered in December 2005, to enter service shortly after. The Avanti P 180 II aircraft received US FAA certification in March Power The engines are mounted above the wing in all-composite nacelles. The Pratt & Whitney Canada PT6A-66 turboprop engines drive Hartzell five-bladed, constant-speed, fully feathering, reversiblepitch, rear-facing push propellers. The position of the propellers removes the drag of propeller vortices on the wings. Pratt & Whitney PT6-66B engines rated at 850 shp were introduced in 2006, gave a 12kt increase in the cruise speed to the maximum of 398kt at altitudes over 35,000ft. Time between overhauls is 3600 h. ISSUE Page 1

2 Avionics The Avanti II avionics are based on the Rockwell Collins ProLine 21 suite and includes three 10in by 8in liquid crystal displays, an FMS 3000 flight management system and AHS 3000 attitude heading reference system. The radar and navigation systems include the Collins WXR-840 colour radar and a dual Collins VIR-32 VOR, a Collins ADF-462, DME-42 and ALT-55B radar altimeter. Design Features The Avanti P180 is a twin-turboprop business aircraft constructed of aluminium and composite materials. Its unorthodox design is unique for a corporate type aircraft in that it features three flying surfaces-the canard foreplane, main wing and T-tail. This arrangement offers not only the benefits of the canard but also allows the wing to be positioned further aft on the fuselage so that it does not adversely affect cabin interior space. The canard also provides a positive lift component in addition to that produced by the main wing. This design allows the main wing to be reduced in size, resulting in less weight and drag. The pusher engine configuration was chosen to reduce cabin noise. The Avanti employs a retractable tricycle landing gear with a single wheel on the main gear mounts and a dual nose wheel mount. Accommodations The P180 II aircraft is certified for single-pilot operation and seats up to nine passengers. The cabin is 5.8ft high and 6.1ft wide and is fitted with five fully-adjustable cabin leather chairs and a divan. The operational ceiling of the Avanti II is 41,000ft allowing the aircraft to fly above weather systems. The Avanti II cabin is rated at 68dbA speech interference level. The pusher engines direct sound toward the tail of the aircraft, minimising engine noise. The combined design of the wing, engine and fuselage provides a significant reduction in vibration for passenger comfort. With a 9psi differential, the Avanti II s cabin maintains sea-level pressure up to 24,000ft. ISSUE Page 2

3 GENERAL CHARACTERISTICS Capacity: 7/8 passengers Length: 47 ft 3 in (14.41 m) Wingspan: 46 ft 0 in (14.03 m) Height: 13 ft 0 in (3.98 m) Max Cruise Speed: 737 km/h (398 kts) Range: 2,800 km (1,500 nm) Max. Certified Taxi Gross Weight: 12,100 pounds (5,488 kg) Max. Certified Take-Off Weight: 12,050 pounds (5,466 kg) Max. Certified Landing Weight: 11,450 pounds (5,194 kg) Maximum Zero Fuel Weight: 9,800 pounds (4,445 kg) Powerplant: 2 P&WC PT6A-66B, 850 lbf each AIRFRAME Year of manufacture: 2007 Year of delivery: 2007 Total time airframe: 2,026 h Total landings: 1,391 Certified for: 7/8 passengers Range: 1,500 nm Cargo Space: 1,25 m³ (44.15 ft³) Inspections: C check CW 02/2016, A check CW 10/2016 No damage history ENGINES Manufacturer: Mfg Part No.: LH Engine Total Time: LH Engine Time Since HIS: RH Engine Total Time: RH Engine Time Since HIS: LH Engine Total Cycles: RH Engine Total Cycles: Thrust Rating: Pratt & Whitney Canada PT6A-66B 2,020 h 206 h 2,020 h 206 h 1,387 landings 1,387 landings 850 lbf PROPELLERS Manufacturer: Mfg Part No.: LH / RH Propeller Total Time: Hartzell HC-E5N-3 2,020 h ISSUE Page 3

4 EXTERIOR Snow White with Red, Blue and Gold Stripes INTERIOR Beautiful and luxuriously appointed seven passenger layout with seating completed in beige leather Standard cabin shells Standard Passenger Service Units (1 each side) customized to suit seat configuration Standard cabinets with partitions between cockpit and passenger cabin Standard aft partitions between passenger cabin and toilet area Four individual seats in Club configuration One two-place divan One one-place divan Two folding tables One refreshment center Standard Cabinet Assembly Vanity Closet Standard Cabinet Assembly Toilet Console Standard Cabinet Assembly Vanity Facia Toilet (Belted) Miscellanea ISSUE Page 4

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6 AVIONICS Collins Pro-Line 21 - UPGRADE IFIS 5000 Radio Management System Collins RTU-4200, CDU-3000 Dual VHF COM - Collins VHF-4000 Transceiver with Antenna with 8.33 khz spacing VHF NAV 1 + ADF - Collins NAV-4000 VOR/ILS/MKR/ADF Receiver with Antennae VHF NAV 2 - Collins NAV-4500 VOR/ILS/MKR Receiver with Antennae Single DME - Collins DME-4000 (3 channel) with Antenna Dual Mode S Flight ID Diversity Transponder - Collins TDR-94D Radio Altimeter - Collins ALT-4000 (Operation to 2500 ft) with Antennae Turbulence Detection Weather Radar - Collins RTA-852 Colour Radar with 12" Antenna TCAS I L-3 Communications SkyWatch HP model SKY899 TAWS Class B with Worldwide Database L-3 Landmark TAWS 8000 Dual Audio Panel - Baker B1045, Dual Cockpit Speaker Dual hand-held Microphone, Dual Boom/Microphone/Headset EFIS with EIS Three Collins displays AFD-3010, two DCP-3030, CCP-3000 Flight Guidance System - Collins Dual FGC-3003 (A/P,YD and dual Flight Director included),three SVO-3000 Servos, single FGP-3000 Flight Guidance Panel Single FMS - Collins FMC-3000 (NAV to NAV and VNAV), CDU-3000 DBU-4100 GPS Sensor Unit - Collins GPS-4000A Dual ADS - Collins ADC-3000 Dual AHRS - Collins AHC-3000 and FDU-3000 Maintenance Diagnostic System - Collins MDC-3110 Four Data Concentrator Unit - Collins DCU-3001 Stand-by Cluster Instrument L-3 Communications GH-3100 Emergency Locator Transmitter ELT 406 Dual Clock (Flight Hour Meter included) Dual Master Annunciator Dual Turn&Slip Indicator (shown on the displays) Reversionary/Miscellaneous Panel ISSUE Page 6

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8 CONTACT ENGEL&VÖLKERS AVIATION Eric PAUWELS DISCLAIMER This offering is subject, but not limited to, errors, omissions, price fluctuation, and prior sale or withdrawal without notice. All details disclosed are without guarantee and solely based on the information received by Engel & Völkers Aviation. Engel & Völkers Aviation cannot be held liable for any lack of completeness, inaccuracy, or ambiguities and/or errors contained in the information disclosed. It is the buyer s responsibility to disclose the details of any concern(s) to the seller, by the request of an independent survey, pre-purchase inspection and/or enquiry. The buyer must ensure that the purchase contract properly reflects his concern(s) and that it sets out any representations and/or details on upon which he may rely. We are at your disposal for any further information about the aircraft. Upon receipt of notice, the aircraft is available for viewing at timing to be agreed upon, accompanied by an Engel & Völkers Aviation representative. ISSUE Page 8