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P2008 JC

Innovation is in the air

The Tecnam P2008 is a hig wing, two place, single engine airplane equipped with tricycle landing gear. But is not only that. The P2008 is up-to-date technology with composite fuselage, safe and easy flying with beauty, inside and outside.

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Max Range

With this range you can use if cross country.

Cruise Speed

219 km/h Sea Level


Two seats side by side.

Useful Load

the load able to be carried by an aircraft.


The P2008JC has metal Wings and a metal stabilator. Tecnam chose metal wings and stabilator structures for strength, reliability, and ability to flex in flight providing a more comfortable ride. To produce the desired increase in cabin width and greater aerodynamic efficiency, Tecnam chose carbon fiber. The decision to utilize both materials was for the optimization of aerodynamic qualities, flight characteristics, and reliability. This addition allows Tecnam to make decisions to be based on design and structural integrity rather than purely the cost of production. The wing is based on the well-known NACA63A airfoil, and through partial tapering, it is brought close to the optimal lift distribution (elliptical). The Single-slot flaps extend along much of the wing span. The Frise type aileron along with the taper design provides a high rate of roll. The all movable type (stabilator) horizontal tail, traditional on Tecnam aircraft, allows excellent controllability and excellent "hands off" longitudinal stability.

Interiors Details

The Cabin offers newly designed seats and seat rails which are easily operated and adjustable fore and aft via a single handle with a reinforced area between the rails to make cabin access even easier. A roomy baggage compartment accommodates voluminous items with both external and internal access. A strong automotive type seal is used on the baggage door and a courtesy lamp illuminates when opened. A wide cockpit panel provides plenty of room for glass panel avionicsA comfortable armrest and USB charger round out the luxurious interior. Everything about the Tecnam P2008 is designed to allow you and your passenger to experience the most outstanding style, comfort, and beauty of flight.. Enjoy the P2008!


Non additive, replaces standard equipment and avionic

Standard GARMIN Avionics Package

Non additive, replaces standard equipment and avionics
GMA 340 Audio Panel
GNC 255A Com/Nav
CTX 328 Tdx
ELT 406 Mhz
Marker Bacon
Stick PushToTalk SwitchPilot/Copilot
Mic& Phone JacksPilot/Copilot

Option 2 - P2008JC VFR Night

Non additive, replaces standard equipment and avionic
Heated Pitot
Gill 25A Battery
Instruments Light
Emergency Light
Map Light
Compass Lighted
Alternate Static Source
Day & Night Switch
Analogue Indicators:
Attitude Electric O Rpm
Oil Temp
Warning Light:
Pitot Heat
High Oil Press

Standard Equipment

Standard Equipment for P2008 JC Aircraft

Flight instruments and indicators

G3X Dual Screen
2 X Gdu370
Lru Kit
Sensor Kit
Installation Kit
G3X Sensor Kit
Antenna Gps

Engine instruments

Amps (Ammeter Shunt Or Hall Effect)
Monitor Cht
Aircraft Bus Voltages
Oil Temperature
Oil Pressure
Fuel Pressure
Trim Indicator

Other instruments / Indicators / Warnings

Airspeed And Altimeter Back Up Tso
Fuel Indicator Rh And Lh
Bank Indicator
Trim Indicator
Warning Light:
– Low Oil Pressure
– Low Fuel Pressure Alt. Out
– Fuel Pump On

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

12 Volt 18A Amp. Battery Fiamm 64
12 Volt Alternators20 Amp.
– Avionic Master
– Fuel Press
– Nav. Lights
– Landing Light
– Strobe Light
12 Volt Socket
External Power Supply Receptable
Auxiliary Alternator 40A
Circuit Breaker Panel

Fuel system

Two Integral Fuel Tanks With 120 Litres Total Capacity
Engine Driven Fuel Pump
Fuel Quick Drain
Electrical Fuel Pump

Powerplant and Propeller

Engines 1 Rotax 912S2 100 Hp, 4 Cylinders
Liquid/Air Cooled, Integrated Reduction Gear
Dual Ignition System
Throttle Control
Tubular Steel Engine Mount
Propeller Gt Propeller, 2 Blade Fix
Propeller Spinner
Air Filter
Oil Filter
Oil And Water Coolers
Carburetor Heat With Manual Control
Thermostat Valve Water And Oil
Auxiliary Alternator

Product Support/Documents

Manufacturers Full Two Year Limited Warranty
Pilots Operation Handbook
Maintenance Manual
Parts Catalog
Aircraft Log Book
Engine Log Book


Pilot And Copilot Seats _ Adjustable Fore And Aft
Seat Belts & Shoulder Harness, All Seats
Wall To Wall Carpeting
Map E Storage Pockets
Luggage Compartments
Fire Extinguisher
Radio Call Plate
First Aid Kit


Epoxy Corrosion Proofing, All Structure
Lh/Rh Front Door Pilot/Copilot, Lock And Key
All Lateral Windows Tinted
Main Wheels, 5,00 X 5
Nose Wheel, 5,00 X 5
Stall Warning

Exteriors lights

Nav. Lights Led With Strobe Aveo Full Led Tso
Taxi Light Led

Cabin comfort system

Windshield Defroster
Ventilator Adjustable, 2 Place
Heating System

Standard GARMIN Avionics Package

GMA 340 Audio Panel
GNC 255A Com/Nav
CTX 328 Tdx
ELT 406 Mhz
Marker Bacon
Stick PushToTalk SwitchPilot/Copilot
Mic& Phone JacksPilot/Copilot


Specification for P2008 JC Aircraft

Aircraft Dimensions

Fuselage Height 2.67 mt – 8.76 ft
Fuselage Length 6.97 mt – 22.87 ft
Wingspan 9 mt – 29.5 ft
Cabin Height (seat to cover) 0.91 mt – 3 ft
Cabin Width 1.14 mt – 3.74 ft
Max Seating capacity 2
Fuel tank capacity 2 x 55 lt – 2 x 14.5 US Gal


Engine Manufacturer ROTAX 912 S2
Engine Power 98 HP
Time Before Overhaul 2000 hrs
Propeller Two-Bladed Fixed Pitch
Fuel Consumption 17 lt/h – 4.50 US Gal/h
Fuel Type Mogas and Avgas

Design Weight & Loading

Maximum Take Off Weight 630 kg – 1388 lb
Std. Empty Weight 390 kg – 859 lb
Useful Load 240 kg – 529 lb
Baggage allowance 20 kg – 44 lb


Vmax 225 km/h – 122 kts
Cruise Speed 75% 215 km/h – 116 kts
Stall Speed (Flaps Down Power Off) 74 km/h – 40 kts
Pratical ceiling 4572 mt – 15000 ft
Take off run 220 mt – 722 ft
Take off distance 264 mt – 866 ft
Landing Run 150 mt – 492 ft
Landing Distance 290 mt – 951 ft
Rate of climb 4.6 m/sec – 900 ft/min
Range 640 NM
Flight Rule VFR Day/VFR Night

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