P2010 PTwenty-Ten
P2010 PTwenty-Ten
Sexy and Speedy.Ready to go?
Tecnam P2010 Twent Ten is a single-engine four-seat aircraft with composite fuselage. The high-wing configuration offers stability, superior cabin visibility. The rear third door grants easy access for passengers and luggage.
Contacteaza-ne acum la 021-22.22.55.4!
Cere o oferta de pret!
Max Range
With this range you can use if cross country.
Cruise Speed
230 km/h Sea Level
Seating
Four seats side by side.
Useful Load
the load able to be carried by an aircraft.
Exteriors
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. Powered by the well proven and reliable Lycoming IO-360-M1A (`Lycoming Light`) engine, providing 180HP and 2700RPM. The Tecnam P Twenty-Ten has a high fuel capacity (240 litres). The fuel tanks are installed in the wing box, behind the main spar, to preserve their integrity for the maximum safety. Of course carbon fibre equals a lighter and therefore more fuel efficient aeroplane.
Interiors Details
Tecnam has always put the comfort for both pilots and passengers first. The Tecnam P Twenty-Ten with its spacious interior and its generous luggage compartment of 300 litres has been designed to be both a very enjoyable aeroplane to fly cross country as well as a robust trainer. The cabin width also allows for a large instrument panel, with its modular design specifically tailored to allow customers to fit either an analogue or digital instrumentation package.
Avionics
Export certificate requirements may require additional equipment or a different equipment list.
Standard
Glass Garmin G500 Day VFR
Option 1
Glass Garmin G500 IFR
Non additive, replaces standard avionics. Also includes the following equipment:
GNC 255A COM/NAV
DME King Kn63 integrated control – dysplayed on PFD
Pitot System Heated
Alternate Static Source
Rocker Switches:
– Pitot Heat
– Map Light
– Day / Night
– Emergency Light
Interior Lighting:
– Panel Light
– Emergency Light
– Pilot/Copilot Cabin Overhead Lights
– Passengers Overhead Light
– Map Light
– Interiors Light Dimming Controls
– Avionics Radios Internally Lighted
– Compass Internally Lighted
– Rocker Switches Internally Lighted
Option 2
Glass Garmin G1000 IFR
Non additive, replaces standard avionics. Also includes the following equipment:
Garmin G1000 Integrated Flight Deck System
Standard Equipment
Garmin G500 Flight Display
GDU 620 Dual 6.5 inches diagonal color LCD
GRS-77 AHRS
GDC-74A Air Data Computer with OAT Probe
GMU-44 Magnetometer
GTP59
GA 35 GPS/WAAS antenna
Flight instruments and indicators
Magnetic Compass
Airspeed Ind., Kts
Altimeter Dual Mode (In/Mb)
Vertical Speed
Directional Electric
Attitude Horizon Electric
Turn And Bank Indicator
Oat
Pitot System Heated
Static System
Alternate Static Source
Stall Warning Audible
Stabilator Trim Position Indicator
Elt Remote Switch/Annunciator
Engine instruments
Jpi Ems 4 Cyl. For L/R 2 Tanks Setup Complete Primary Package With Senders
Annunciation Panel- Caution And Warning Alerts
Flight controls
Hydraulic Brakes
Parking Brake
Electrical Flaps
Dual Flight Controls
Castering Nose Wheel
Aileron And Elevator Lock
Stabilator Trim (Manual)
Engine Controls
Throttle
Mixture
Alternate Air
Flight Trim Controls
Stabilator With Indicator
Flight controls
Hydraulic Toe Brakes
Parking Brake
Electrical Flaps, Preselect
Dual Flight Controls
Castering Nose Wheel
Stabilator Trim (Electric Actuated From Stick)
Engine Controls:
– Central Quadrant With Single Trottle Level _ Throttle
– Choke
Flight Trim Controls_
– Stabilator With Indicator
Fuel Control Selector Andair
Panel Switches:
– Split Starter
– Avionic
Starter Key Acs
Electrical system
Alternator, 28 Volt, 60 Amp
Battery, 24 Volt, 8.0 Ah (1 Hr Rate), Manifold Type
Rocker Switches Internally Lighted
– Master Switch
– Landing Light
– Taxi Light
– Navigation Lights
– Strobe Light
– Pitot Heat
– Map Light
External Power Supply Receptable
Circuit Breaker Panel
Static Discharge Wicks
Landing / Taxi Light
Fuel system
Two Integral Fuel Tanks With 210 Litres Total Capacity
Engine Driven Fuel Pumps
Auxiliary Fuel Pumps, Electric
Fuel Tank Quick Drain
Fuel Selector Valve, Left/Both/Right
Interiors
Pilot And Co-Pilot Seats Simulated Leather
– Adjustable Fore And Aft
– Vertical Adjustment
Two Rear Passenger Seats
– Adjustable Fore And Aft
– Vertical Adjustment
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
Interiors Lights
Pilot/Copilot Cabin Overhead Lights
Passenger Overhead Light
Interior Lights Dimming Control
Avionics Instruments Internally Lighted
Avionics Radios Internally Lighted
Engine Instruments Internally Lighted
Flight Instruments Internally Lighted
Compass Internally Lighted
Map Light
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 Muffler
Fixed Pitch 2
Propeller Spinner
Electric Starter
Exterior
Epoxy Corrosion Proofing, All Structure
Lh/Rh Front Door Pilot/Co-Pilot, Lock And Key
Rh Rear Door Passenger
Rh Bagagge Door With Lock And Key
All 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
Navigation Lh/Rh Wing Tip And Vertical Tail
Vertical Tail Strobe
Landing / Taxi Light
Cabin comfort system
Windshield Defroster
Ventilator Adjustable, 4 Place
Heating System
Soundproofing
Cabin Monoxide Detection System
Product Support/Documents
Manufacturers Full Two Year Limited Warranty
Pilot’s Operation Handbook
Maintenance Manual
Parts Catalog
Aircraft Log Book
Engine Log Book
Standard Avionics Package
Gma 340 Audio Panel
Gnc 255A Comm/Nav
Md200 Vor Indicator
Gtx 328 Transponder
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 Artex
Antennas:
– Marker Beacon Antenna
– Transponder Antenna
– Vhf Antenna
– Nav Antenna
– Emergency Locator Transmitter Antenna
Specification
Aircraft Dimensions
| Fuselage Height | 2.8 mt, 8.86 ft |
| Fuselage Length | 7.9 mt – 25.91 ft |
| Wingspan | 10.3 mt – 33.79 ft |
| Cabin Height (seat to cover) | 0.91 mt – 1 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 |
| Engine Power | 180 hp |
| Time Before Overhaul | 2000 hrs |
| Propeller | Two-Bladed Fixed Pitch |
| Fuel Consumption | 34.6 lt/h – 9.14 US Gal/h |
| Fuel Type | Mogas and Avgas |
Design Weight & Loading
| Maximum Take Off Weight | 1160 kg – 2557 lb |
| Std. Empty Weight | 710 kg – 1565 lb |
| Useful Load | 450 kg – 992 lb |
| Baggage allowance | 40 kg – 88 lb |
Performance
| Vmax | 260 km/h – 140 kts |
| Cruise Speed 75% | 246 km/h – 133 kts |
| Stall Speed (Flaps Down Power Off) | 85 km/h – 46 kts |
| Pratical ceiling | 4572 mt – 15000 ft |
| Take off run | 245 mt – 803 ft |
| Take off distance | 384 mt – 1259 ft |
| Landing Run | 200 mt – 656 ft |
| Landing Distance | 313 mt -1026 ft |
| Rate of climb | 5.1 m/sec – 1000 ft/min |
| Range | 715 NM |
| Flight Rule | VFR Day/VFR Night/IFR |