P2010 P Twenty-Ten
The future is now
4 seats, 3 passenger doors. 1 baggage door. Lycoming 180/215 hp engine.Carbon fibre fuselage. Metal wings, landing gear and stabilator. Balanced controls. Unsurpassed stability. The P2010 is where performance and comfort meet in one sexy IFR package.
Max Range
With this range you can use it cross country. (IO-360)
Max Cruise Speed
270km/h (IO-390)
Seating
Four seats.
Doors
1 large baggage door.
Useful Load
405 kg
Exterior
The Tecnam P Twenty-Ten brings together an advanced technology all carbon fibre fuselage with a metal wing to deliver a superlative single engined, 4 seat aeroplane, designed by Italy’s most innovative Aerospace design ‘guru’ Professor Luigi Pascale.
Carbon fibre ensures smooth surfaces and allows for an elegance and styling you would expect from Tecnam’s Italian design team. Metal is used for the wing and stabilator to provide further strength and stability. The wing is based on the well-proven NACA63A aerofoil. Through partial tapering, the design brings it close to the optimal lift distribution (elliptical). The all movable type (stabilator) horizontal tail, a trade mark of all Tecnam aeroplanes, allows for excellent controllability and ‘hands off’ longitudinal stability.
Interior Details
Tecnam has always put the comfort for both pilots and passengers first.
This four-seater aeroplane brings together an advanced technology all carbon fibre fuselage with a metal wing and stabilator, an expansive cabin featuring ergonomic front and rear seats with exceptional legroom and a separate third entry door.
The wide composite cabin allows for a large instrument panel with latest avionic options: the next generation twin-screen Garmin G1000 Nxi IFR, new Flat-Panel Suite with integrated GFC700 autopilot.
Powerplant & Propeller
The P Twenty-Ten MkII is available with the 180 HP Lycoming IO-360 and has a high fuel capacity (240lt, 63.4 imp. gal). Of course, carbon fibre equals a lighter and therefore more fuel efficient and most economical aeroplane.
You have also the option for Lycoming’s IO-390-C3B6 engine. The Lycoming IO390-C3B6 enables the P Twenty-Ten to climb at 1,100 ft/m and cruise on 75% power at 146 kts. The IO-390-C3B6 provides 215 hp @ 2,700 rpm, coupled with a variable-pitch propeller
The selection of the Lycoming IO390-C3B6 to power this next-generarion four-seater, was primarily as a result of its capability to burn alternative fuels other than 100LL. The approval of this major design change by FAA set an important milestone on Tecnam’s “green transition” as the first worldwide General Aviation aircraft manufacturer able to obtain such a wide, flexible and non-single-brand related choice, as well as the first manufacturer capable of obtaining approval for use of automotive fuel on IO-360 Lycoming engine.
IO-360-M1A 180 hp
Power: 180 HP@2700 RPM
Fuel: Unleaded Aviation Fuels: UL91 or higher per ASTM D7547 or Automotive Fuels: 93 AKI or equivalent per ASTM D4814. Please refer to Lycoming Engines SI 1070 for a complete listing of approved fuels.
IO-390-C3B6 215 hp
Power: 215 HP@2700 RPM
Fuel: UL100 or 100LL
P Twenty Ten 180HP
EMPTY WEIGHT 755 KG
Also Includes the following equipment:
Lycoming IO360 180 HP Engine
2 Bladed Fixed Propeller
P Twenty Ten 215HP
EMPTY WEIGHT 770 KG
Non-Additive. Also Includes the following equipment:
Lycoming IO390 215 HP Engine
3 Bladed VP Propeller
Avionics
Export certificate requirements may require additional equipment or a different equipment list.
STANDARD Glass Garmin G1000 NXI IFR – BOTH POWERTRAINS
• G1000 Nxi Integrated Flight Deck System, includes:
• GDU 1050 1O-inches PFD
• GDU 1050 1O-inches MFD
• Dual GEA 71 Engine & Airframe unit
• Dual GIA 63WAAS Com/nav/GPS/GS/Loc
• GMA1347 Digital audio system
• GMU44 Magnetometer
• GDC72 Air data computer
• GRS79 AHrS
• GTP59 OAT
• GTX345R Mode S Transponder (ADS-B In and OUT)
Non additive, replaces standard avionics. Export certification requirements may require additional equipment and charges. Options also pictured.
Paint Options
go to the Color Configurator
Interior Options
Standard Interior comes with blue seats and ivory cabin. Electric lift of the seats is Standard.
Premium option makes your aircraft more precious: Alcantara leather and a dark ceiling improve your flying experience with unique ingredients. Your aircraft interior is now more exclusive with electrically adjustable comfort front seats while guaranteeing absolute compliance with the industry’s strictest standards.
We in Tecnam always strive for excellence and we want your aircraft to be more precious than ever. The italian flair is not only external, but now also at your finger tips, because we have spent a great deal of time to improve every detail of the interior. A completely new designed interior with a choice of leather seat colours, new dark material for the ceiling and the sidewalls, dimmable LED lights, USB chargers put your aircraft at the top level of comfort. It is your aeroplane, your lifestyle and you deserve the best.
A) Leather anthracite gray
B) Medium gray
A) Leather anthracite light gray
B) Anthracite gray
Photos as example. Options subject to change without notice. Always consult the Aircraft Configuration list.
-
- Seats and Garmin Nxi avionic suite
-
- Dimmable overhead lights
-
- Fine leather seats, a new design of the interior with dark colours
-
- Electric seat lift
-
- Levers
-
- USB charger
-
- Overhead light and sunglasses holder
-
- Details of door handle
-
- USB and 12 v chargers
-
- Details of door handle
-
- P2010 Premium Edition
Standard Equipment
Garmin G1000 Nxi
G1000 Nxi Integrated Flight Deck System, includes:
GDU 1050 1O-inches PFD
GDU 1050 1O-inches MFD
Dual GEA 71 Engine & Airframe unit
Dual GIA 63WAAS Com/nav/GPS/GS/Loc
GMA1347 Digital audio system
GMU44 Magnetometer
GDC72 Air data computer
GRS79 AHRS
GTP59 OAT
GTX345R Mode S Transponder (ADS-B In and OUT)
Flight instruments and indicators
Magnetic Compass
MD 302 Standby Attitude Module
Pitot System Heated
Static System
Alternate Static Source
Stall Warning Audible
Stabilator Trim Position Indicator
Rudder Trim Position Indicator
Flight controls
Hydraulic Toe Brakes
Parking Brake
Electrical Flaps
Dual Flight Controls
Castering Nose Wheel
Aileron Lock and Elevator Lock
Flight Trim Controls
– Rudder with Indicator
– Stabilator with Indicator
Engine Controls:
– Throttle
– Mixture
– Alternate Air
– Fuel Control Selector with LH/RH/OFF
Electrical system
Alternator, 28 Volt, 60 Amp
Battery, 24 Volt 8.0 AH
Rocker Switches:
– Master Switch
– Fuel Pump
– Landing Light
– Taxi Light
– Navigation Lights
– Strobe Light
External Power Supply Receptacle
Circuit Breaker Panel
Static Discharge Wicks
Landing/Taxi Light LED
Interior
Pilot and Co-Pilot Seats Leather
– Adjustable Fore and Aft
– Vertical Adjustment
Two Rear Passenger Seats Leather
Seat Belts & Shoulder Harness, All Seats
Wall To Wall Carpeting
Hand Held Fire Extinguisher
Map & Storage Pockets
Radio Call Plate
Tow Bar
Soundproofing
Luggage Compartments
Overhead Cockpit Speaker
Four Position Intercom System
First Aid Kit
Powerplant and Propeller
Lycoming IO-360-M1A Engine 180 HP @ 2700 RPM
Fuel Injection System
Tubular Steel Engine Mount
Dynafocal Rear Mount
Engine Driven Vacuum Pump
Alternate Engine Air
Oil Cooler
Shock Mounted Cowling
Throttle Control
Mixture Control
Dual Ignition System, Shielded Magneto Engine Exhaust Muffer
Fixed Pitch 2 Blade MT Propeller
Propeller Spinner
Electric Starter
Fuel system
Two Integral Fuel Tanks With 240 Litres (64 UsGal) Total Capacity
Engine Driven Fuel Pump
Auxiliary Fuel Pump, Electric
Fuel Tank Quick Drain
Fuel Selector Valve, Left//Right/Off
Exterior
Epoxy Corrosion Proo ng, All Structure
LH/RH Front Door Pilot/Co-Pilot, Lock and Key
Rh Rear Door Passenger
Rh Baggage Door With Lock
Rear Window
All Lateral Windows Tinted
Fixed Landing Gear
White Polyurethane Exterior Paint
Tie Down Rings
Main Wheels, 6.00 X 6
Nose Wheel, 5.00 X 5
Exteriors lights
Nav. Lights LED with Strobe Aveo Full LED TSO
Landing/Taxi Light LED
Cabin comfort system
Windshield Defroster
Ventilator adjustable, 4 Place
Heating System
Soundproofing
Cabin Monoxide Detection System
Product Support/Documents
Manufacturer’s Full Two Year Limited Warranty
Pilot’s Operation Handbook
Maintenance Manual
Parts Catalog
Aircraft Log Book
Engine Log Book
Standard Avionics Package
also includes:
Altitude Encoder
Avionics Master Switch
Mic & Phone Jacks Pilot/Copilot/Passengers
Hand Held Microphone
Avionics Circuit Breaker Panel
Pilot And Co-Pilot PTT
ELT 406
DME KING KN63 – Displayed on PFD
Antennas:
• Marker Beacon Antenna
• Transponder Antenna
• VHF Antenna
• NAV Antenna
• Emergency Locator Transmitter Antenna
Optional Equipment
|
Code |
Kg |
Description |
|
P01 |
10 |
Autopilot GFC700 Garmin – Fully integrated two-axis |
|
P02 |
4,5 |
ADF RA3502 Becker remote unit |
|
P03 |
10 |
TAS GTS 800 Garmin with Dual GA58 |
|
P04 |
2,5 |
Interior Premium Edition: leather electrically adjustable seats (front), Matte Grey interior finishing, chrome metallic badge |
|
P05 |
2,5 |
Special Paint two colours |
|
P06 |
9 |
MT 2 Blade VP Propeller (Exchange for Standard Fixed Pitch Propeller – only IO-360) |
|
P10 |
10 |
MT 3Blade VP Propeller MTV-12-B/183-59b (Exchange for Standard Fixed Pitch Propeller – only IO-360) |
|
P09 |
Fuselage Cover |
Aircraft Dimensions
| Fuselage Height | 2,64 mt – 8.66 ft |
| Fuselage Length | 7,97 mt – 26.15 ft |
| Wingspan | 10,3 mt – 33.79 ft |
| Cabin Height (seat to cover) | 0,91 mt – 3 ft |
| Cabin Width | 1,14 mt – 3.74 ft |
| Max Seating capacity | 4 |
| Fuel tank capacity | 2 x 120 lt – 2 x 31.70 US Gal |
Powerplant
| Engine Manufacturer | Lycoming IO 360 M1A 180hp / IO-390-C3B6 215 hp |
| Engine Power | 180 hp/ 215 hp |
| Time Before Overhaul | 2000 hrs |
| Propeller | Two Bladed Fixed Pitch/Variable Pitch Three Bladed Variable Pitch |
| Fuel Consumption | 39 lt/h – 10.3 US Gal/h |
| Fuel Type | Mogas and Avgas |
Design Weight & Loading
| Maximum Take Off Weight | 1160 kg – 2557 lb |
| Empty Weight, Standard | 740 kg – 1631 lb |
| Useful Load | 420 kg – 925 lb |
| Baggage allowance | 40 kg – 88 lb |
Performance
IO-360 180 HP with Variable Pitch Propeller
| Max Cruise Speed (KTAS) | 137 kts – 254 km/h |
| Stall Speed (Flaps Down Power Off) KCAS | 52 kts – 96 km/h |
| Practical ceiling | 12000 ft -3658 mt |
| Take off run | 1102 ft – 336 mt |
| Take off distance | 1952 ft – 595 mt |
| Landing Run | 778 ft – 237 mt |
| Landing Distance | 1709 ft – 521 mt |
| Rate of climb | 841 ft/min – 4.3 m/sec |
| Range | 600 NM – 1111 km |
| Flight Rule | VFR Day/VFR Night/IFR |
[/columns7]