• 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