P2010TDI JET-A1-Diesel

Improving Perfection. Now with Diesel.

Burning just 5.2 US Gal per hour (less than 20 litres), with roomy, Italian-style shaped cabin interiors, and taking advantage of the high-wing configuration with 3 access doors plus another dedicated one for the baggage compartment, is no longer a dream. And it is no longer a dream to cover 1,000nm with the full tank capacity of 63 US Gal (240 litres).


Contiental CD-170 JET-Diesel

136 kts

Max Cruise Speed​ KTAS 252 km/h

1050 NM

Range - 1940 km

5.2 USG/h

Fuel Consumption 19.5 lt/hr


The state-of-the-art Tecnam P TwentyTen is the most advanced high-wing modern single-engine aircraft in the marketplace, today with Continental CD-170 Diesel engine.
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 state of art avionic options: twin-screen G1000 Nxi IFR, new Flat-Panel Suite with integrated GFC700 autopilot. 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.


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. 

The D-Revolution

The P2010 TDI is the aircraft with the longest range and lowest consumption in Tecnam fleet.

Tecnam’s choice of Diesel fuel offers the following benefits:

Typical Mission Examples

Mission 1 400 nm FL90 Mission [MTOW] 75% PWR
Fuel 24.3 USG – 92 lt
Occupants + Luggage 639 lb – 290 kg


Mission 2 600 nm FL90 Mission [MTOW] 75% PWR
Fuel 34.4 USG – 130 lt
Occupants + Luggage 573 lb – 260 kg


Mission 1
75 % PWR
Fuel Consumption 6.6USG/h – 25lt/h
Speed @6000ft 127 ktas
Speed @9000ft 132 ktas

Mission 2 
60 % PWR
Fuel Consumption 5.2USG/h – 19.5lt/h
Speed @6000ft 110 ktas
Speed @9000ft 115 ktas


Powered by Continental

The P TwentyTen TDI is powered by the Continental CD-170, which is a liquid-cooled 4-cylinder in-line four-stroke Diesel engine with DOHC (double overhead camshaft). The valves are actuated by a cam follower. The operation of the direct Diesel injection engine is based on the common-rail technique and is turbo charged. The engine is controlled by a FADEC system. The propeller is driven via an integrated gearbox (i=1.69) with a clutch or dual mass flywheel. The engine is equipped with an electric starter and one alternator and optional auxiliary drive. Engine monitoring is fully integrated inside the avionic suite screens and allows a management of power, with significant fully automatic mixture control (absence of related lever and always guarantees the best fuel/air ratio for every single cylinder).


Standard Equipment

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

Fuel system

Two Integral Fuel Tanks With 240 Litres (63 US Gal) Total Capacity
Two engine driven fuel pumps
Support Fuel Pump Electric
Fuel Tank Quick Drain
Fuel Selector Valve, LH/RH/OFF

Powerplant and Propeller

Continental CD-170 Engine 170 HP
Tubular Steel Engine Mount
Alternate Engine Air
Fadec thrust-lever
Engine Exhaust Muffler
Constant speed MT 3 Blade Propeller
Propeller Spinner
Electric Starter

Flight controls

Hydraulic Toe Brakes
Parking Brake
Electrical Flaps
Dual Flight Controls
Castering Nose Wheel
Ailerons Lock and Elevator Lock
Flight Trim Controls:
Rudder with Indicator
Stabilator with Indicator
Engine Controls:
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


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
Luggage Compartments
Overhead Cockpit Speaker
Four Position Intercom System
First Aid Kit


Epoxy Corrosion Proofing, 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

Exterior lights

Nav. Lights LED With Strobe
Landing/Taxi Light LED

Cabin comfort system

Windshield Defroster
Ventilator Adjustable, 4 Place
Heating System
Cabin Monoxide Detection System

Product Support and Documents

Manufacturer’s Full Two Year Limited Warranty
Pilot’s Operation Handbook
Maintenance Manual
Parts Catalogue
Aircraft Log Book
Engine Log Book

Standard Avionics 

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 mhz
DME KING KN63 – Displayed on PFD

• Marker Beacon Antenna
• Transponder Antenna
• VHF Antenna
• Nav Antenna
• Emergency Locator Transmitter Antenna


IFR Glass Cockpit

Standard Garmin Avionics Package

G1000 Nxi Integrated Flight Deck System, includes:
GDU 1050 10-inches PFD
GDU 1050 10-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
GTX345R Mode S Transponder (ADS-B IN and OUT)


• Marker Beacon
• Transponder

Optional Equipment

Code Kg Description

P201 10 Autopilot GFC700 Garmin – Fully integrated two-axis 

P202 4,5 ADF RA3502  Becker remote unit

P203 10 TAS GTS 800 Garmin  with Dual GA58

P204 4,5 Interior Premium Edition: leather electrically adjustable seats (front), Matte Grey interior finishing, chrome metallic badge

P205 2,9 Special Paint two colours

P208 Flight Stream 510 Garmin

P209 Fuselage Cover

P210 1,5 Metallic paint, (requires option P205)

P211 Disassembling and packing in one 40 ft container

P212 3 Aviation Oxygen System, Portable for 4 people

Paint Schemes

Go to Tecnam colors to configure your schemes: http://colors.tecnam.com/config2018/p2010.html

General Views

Technical Specifications

P2010TDI JET-A1-Diesel

Specifications subject to change without notice. Always consult the Aircraft Flight Manual.


Fuselage Height 8.66 ft 2.64 m
Fuselage Length 25.98 ft 7.92 m
Wingspan 33.79 ft 10.3 m
Area 149 ft2 13.9 sqm
Max Seating capacity 4
Fuel tank capacity 55 US Gal 210 lt

Design Weight & Loading

Maximum Take Off Weight 2,557 lb 1,160 kg
Empty Weight, Standard** 1,753 lb 795 kg
Useful Load 805 lb 365 kg
Baggage allowance 88 lb 40 kg

 *Empty weight could vary by ±2%
**Without unusable fuel


Engine Manufacturer CONTINENTAL AERO CD-170
Engine Power 168 HP
Propeller Constant Speed 3 Blade  MT Propeller
Fuel Consumption 5.2USG/h – 19.5lt/h
Fuel Type JET A-1 (ASTM D 1655), JET A (ASTM D 1655), Diesel (EN 590)


P2010TDI MkII 3 Blades Variable Pitch Propeller

Max Cruise Speed KTAS 136 kts – 252 km/h
Cruise speed 75% @6000 ft 127 ktas – 235 km/h
Cruise speed 75% @9000 ft 132 ktas – 244 km/h
Stall Speed (Flaps Down Power Off) KCAS 52 kts 96 km/h
Practical Ceiling 18,000 ft –  5486 m
Take off run 1246 ft – 380 m
Take off distance 1903 ft – 580 m
Rate of climb 787 ft/min – 4 m/sec
Landing Run 853 ft – 260 m
Landing Distance 1772 ft – 540 m
Range** 1050 NM 1940 km

*Sea Level
**(75% + res. 30 min) max fuel
All estimated performance data are based on aeroplane weights at MTOW; standard atmospheric conditions; level, hard surface, dry runways, no wind.



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