• Founded in 1884 as a ship interiors and furnishing manufacturer
• Aviation activities started in 1915
• More than 50 aircraft types designed and manufactured since then
• Piaggio was also a pioneer in design and experimentation of rotorcraft, well before Sikorsky’s first flights
100 years of history
• Aircraft design and manufacturing
• Aircraft maintenance
• Aero-structures
• Aero-engines parts manufacturing & MRO
Leading company
in the aviation sector
100% of capital as of September 2015
Shareholding structure
Piaggio Aerospace inaugurated on November 2014 its new HQ at Villanova d’Albenga.
Strategically located for direct access to the airport of Villanova, the 127,000 sqm site hosts a state-of-the-art industrial plant covering 49,000 sqm where Piaggio Aerospace designs, develops and manufactures aircraft, Unmanned Aerial Systems and aero-engines.
Centre of Excellence
Core Business
Business and special mission aircraft design, manufacturing , development and support
Aero-engines parts manufacturing final assembly and MRO
Unmanned Aerial System and Multirole Parol Aircraft design, manufacturing, development and support
Aero-Engines
• Parts manufacturing, test and certification of sub-assembly.
• Assembly, test and certification of complete aero-engines:
- Pratt & Whitney Canada: PW206 & PW207
- Honeywell: 55-L-714 A
• MRO of following turbojet and turboshaft engines:
- Honeywell:
T53, T55 and LTP
- Rolls-Royce:
Viper, GEM and M250
Parts manufacturing – Assembly – MRO under license from other manufacturers
VIP/Utility transport
P.180 Avanti
Aircraft Family
P.1HH HammerHead Unmanned Aerial System
Aero Ambulance
Flight Inspection
Special Mission
MPA
Business Aviation P.180 Avanti
• Fast and fuel-saving
• Up to 8 passengers
• Best-in-class volume per seat
• Short take-off/landing capability
• All-weather capability
• Jet-like performances
• Cost-effective operations
• Environmentally friendly
A world fleet with more than 900.000 FH
Powerplant
Performance enhancement:
Time to climb: -3%
Fuel to climb: -3,5%
Fuel consumption: -3%
Max range: + 3%
New landing gear
New system with digital steering and anti-skid
Improvement on contaminated runway
Reduction of pilot workload
Automatic steering engagement/disengagement
Increased range Range improvement through an additional fuel tank
No take-off & landing performance change
Range increase: 300 NM
Range with 4 pax: up to 1,770 NM
(ISA conditions, NBAA IFR fuel reserve)
New propelling system
New Hartzell scimitar-shaped blades
New exhaust duct
External noise reduction: - 68% (5 dB)
Internal noise reduction: -20% (1 dB)
New winglet system
Improvements
Cockpit – Rockwell Collins ProLine 21
No. 3 10” x 8” LC displays TCAS , TAWS-B
Flight Management System FMS-3000 IFIS Flight Information System
Global Positioning System GPS-4000S RVSM approved
Attitude Heading Reference System CAT II approach capability
Wx Radar w/ Turbulence Detection P-RNAV capability
Max Speed: Max Service Ceiling: 402 KTAS (745 km/h) 41000 ft (12.500 m)
Cruise Speed at Maximum Cruise Power (MCP):
At 35000 ft: 390 KTAS (722 km/h) At 39000 ft: 366 KTAS (678 km/h)
Fuel consumption at MCP (FL350, 390 KTAS): 97 USG/h (360 lt/h) IFR Max Range at Max Range Power (39000 ft):
1770 nm (3278 km) with additional fuel tank
Take-off Distance (50 ft obstacle, S.L. ,ISA): 3196 ft (974 m)
Landing Distance (50 ft obstacle, S.L., ISA, no reverse):
3282 ft (1000 m) Certified for steep-approach, P-RNAV and Cat II Operations
Performances
1,85 m
(6.1 ft)
1,75 m
(5.9 ft)
BEST IN CLASS CABIN SIZE
1,70 m
(67 in)
BEST IN CLASS CABIN SIZE
Full Stand-up cabin
Cabin altitude up to FL240 = Sea Level (S.L.)
Cabin altitude at FL410 = 2,012 m (6,600 ft )
Differential: 9.0 psi (0.62 bar)
CABIN LAYOUT “AMBIENTE” (6+1 SEATS)
CABIN LAYOUT “AMBIENTE” (6+1 SEATS)
CABIN LAYOUT “AMBIENTE” (6+1 SEATS)
CABIN LAYOUT “AMBIENTE” (6+1 SEATS)
CABIN LAYOUT “ARMONIA” (7+1 SEATS)
CABIN LAYOUT “ARMONIA” (7+1 SEATS)
•7+1 Seats Cabin Arrangement
CABIN LAYOUT “SHUTTLE” (7+1 SEATS)
Aero Ambulance
Aero Ambulance
Loading system
Aero Ambulance
One (or two) 6’ Lifeport P.L.U.S. equipped with:
Stretcher fixing system to the floor
Oxygen cilindres with pressure regulator
Vacuum pumps (medical suction unit)
Air Compressor with pressure accumulator
Power supply for the medical equipment (12-28 VDC and 230 VAC)
Aero Ambulance Control panel
Aero Ambulance
Provisions for self-contained medical equipment such as:
• Monitor: Propaq series type or equivalent,
• Respirator: Breas LVT 1000 Pulmonetic type or equivalent
• Infusion pumps: Braun Perfusor compact type or equivalent
• Defibrillator
Aero Ambulance
Incubator
ENAV – Italian Flight Inspection Provider
Flight Inspection
Flight Inspection
Configuration for ENAV and the Italian Air Force
Data Analyser Rack
5+1 available seats:
One (1) operator seat
Four (4) passengers seats
One (1) lavatory seat
Flight Inspection
certified for take-off and landing
Operator Console
Special Mission Provision to install CA-295 Camera
Add two windows on aircraft sides
P.180 RTAF – RECON CA-295 CameraInstallation
Provision to install Visionmap A3 Camera
Add an interface window on aircraft bottom fuselage skin.
P.180 RTAF – Visionmap A3 CameraInstallation
Fairing on lower side
Provision to install Visionmap A3 Camera
Provide appropriate attachment plate to install the A3 camera in the central lower floor.
P.180 RTAF – Visionmap A3 CameraInstallation
Fairings on lateral sides
Photogrammetry
Customer Service
World Fleet in operation
Authorized Service Centers
The P180 Avanti inspection program mainly consists of individual maintenance checks, performed at various flight hour intervals:
200FH Tasks (except when B, C, D occur)
B Check – Every 600 FH (except when C, D occur)
C Check – Every 1800 FH (except when D occurs, corresponding to Engine HIS)
D Check – Every 3600 FH (corresponding to Engines and Propellers Overhaul)
Inspections Program
200FH Tasks
P180 Avanti current warranty coverage:
– 5 years for Piaggio’s proprietary parts
– 5 years for structures
– 5 years for engines by Pratt & Whitney
– 5 years for avionic suite by Rockwell Collins
– 2 years for other components
Warranties
Maintainers Training Maintenance Training
o Class B1 (airframe) - 3 weeks plus PracticalElements
o Class B2 (avionics) - 2 weeks plus PracticalElements
o Practical elements - on demand
o Class C (familiarization) - 1 week
•11
• At Piaggio Training Center in Genoa, Italy (EASA/CAAC/DAT Part 147 approved)
• At the Flight Safety International Wichita Maintenance Learning Center in Florida, USA
Pilots Training
Aircraft comparison
200 250 300 350 400
PC 12
TBM 850
King Air 250
King Air 350i
M2
CJ2+
CJ3
Phenom 300
280 KTAS
402 KTAS
KTAS
Jet and
Avanti EVO
Other
Turboprops
Speed comparison
P.180 Avanti
442 KTAS
0 20 40 60 80 100 120 140
PC12NG
TBM 850
King Air 250
King Air 350i
M2
CJ2+
CJ3
Phenom 300
98 min
88 min
min
Jet and Avanti EVO
Other
Turboprops
Flight time for a route of 1100 km (600 NM)
P.180 Avanti
135 min
0 500 1000 1500 2000
PC12NG
TBM 850
King Air 250
King Air 350i
M2
CJ2+
CJ3
Phenom 300
947 lb
1144 lb
1750 lb
lb
Jet and Avanti EVO
Other
Turboprops
Fuel consumption for a route of 1100 km (600 NM)
P.180 Avanti
0,00
0,50
1,00
1,50
2,00
2,50
3,00
3,50
4,00
4,50
5,00
Avanti EVO M2 Phenom 300
CJ2+ CJ3+ King Air 350i
King Air B250
USD/NM
Source: Conklin and De Decker
Direct Operating Costs per Nautical Mile
P.180 Avanti
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