P2008 JC

Innovation is in the air.

The Tecnam P2008 is a high 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.
The Tecnam P2008JC is delivered in full compliance with the requirements of


Quick facts


Max Range

With this range you can use it cross country.


Max Cruise Speed

222 km/h



Two seats side by side.


Useful Load

More than enough for 2 persons and some luggage.


The P2008JC has both metal wings and a metal stabilator. Tecnam chose to construct the P2008 with metal wings and stabilator structures for strength, reliability, and the ability to flex in flight, thereby ensuring a more comfortable ride. To produce the desired increase in cabin width and greater aerodynamic efficiency, Tecnam chose carbon fibre.
The decision to use both materials was for the optimisation of aerodynamic qualities, flight characteristic, and reliability. This addition enables Tecnam to make construction decisions based on optimum 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 with internal acccess accommodates voluminous items.
A wide cockpit panel provides plenty of room for glass panel avionics.
A comfortable armrest and USB charger round out the luxurious interior.
Everything about the Tecnam P2008JC is designed to allow you and your passenger to experience the most outstanding style, comfort, and beauty of flight..
Enjoy the P2008JC




  • GMA 340 Audio Panel
  • GNC 255A Com/Nav
  • GTX 335 Transponder ADS-B OUT
  • ELT 406 Mhz
  • Antennas:

– Transponder



– Marker Beacon

  • Speakers
  • Microphone
  • Stick Push-To-Talk Switch, Pilot/Copilot
  • Mic & Phone Jacks, Pilot/Copilot


Includes the following equipment:

  • Heated Pitot
  • GILL 25A Battery
  • Instrument Light
  • Emergency Light
  • Map Light
  • Dimmer
  • Landing/Taxi Light Led
  • Nav. Light Led
  • Compass Lighted
  • Alternate Static Source
  • Day & Night Switch
  • Analogue Indicators:
  • Attitude Electric
  • RPM
  • Oil Temp
  • Volt
  • Warning Light:
  • Pitot Heat
  • Oil High Press

Export certification requirements may require additional equipment and charges.

Standard Equipment

Flight instruments and indicators

G3X Dual Screen
2 X GDU370
Sensor Kit
Installation Kit
G3X Sensor kit
Antenna GPS


Engine Instruments, GSU Configuration

• Amps (Ammeter Shunt or Hall Effect)
• Monitor CT
• 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 Throttle Lever
_ Throttle
_ Choke
Flight Trim Controls
_ Stabilator with Indicator
Fuel Control Selector Andair
Panel Switches:
_ Split Master/Alternator switch
_ Avionic
Starter Key ACS

Electrical system

12 VOLT 18A AMP. Battery FIAMM 64
12 VOLT Alternator 20 AMP.



_Avionic Master
_Fuel Press
_Nav. Lights
_Landing Light
_Strobe Light
12 VOLT socket
External Power Supply Receptical
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

ENGINE – 1 ROTAX 912S2 100 HP, 4 Cylinders
liquid/air cooled, integrated reduction gear
Dual Ignition System
Throttle Control
Tubular Steel Engine Mount
Propeller – Hoffman, 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 and 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
GTX 335 Transponder ADS-B OUT
ELT 406 Mhz
– Transponder
– Marker Beacon
Stick Push-To-Talk Switch, Pilot/Copilot
Mic & Phone Jacks, Pilot/Copilot

Paint Schemes

Optional Equipment

Code  Description 
114/A Turn & Slip Indicator 2 1/4”
120/A GTR225 COM 25 Mhz with Antenna and Installation
120/B GTR225A COM 8.33 Khz with Antenna and Installation
119 MD200 VOR Indicator Only for GNC255A
121 GTN 650 Com/Nav/Gps with Antennas, Triplex and inst. With GI106A Indicator
121/A GTN 650 Com/Nav/Gps with Antennas, Triplex. & inst. With GI106A Ind.(Exchange for Std. GNC255A)
122 GTN 750 Com/Nav/Gps with Antennas, Triplex and inst. With GI106A Indicator
122/A GTN 750 Com/Nav/Gps with Antennas, Triplex & inst. With GI106A Ind.(Exchange for Std. GNC255A)
128 AERA 500 with Antenna, Panel Support and Installation
132 GARMIN 795 with Antenna, Panel Support and Installation
137 KR 87 ADF with KI227 Indicator
139 DME KN63-14 with KDI 572 Indicator
157 Head Sets, two
157/A BOSE A20 Head Sets, two
182 Fuselage Cover
185 Battery Gill G25 (Exchange for standard battery)
208 Premium Edition (includes Opt. 201)
209 Control Lock
210 Towing Bar
201 Special Paint Two Colours


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 Hoffmann 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 650 kg – 1433 lb
Empty Weight, Standard 400 kg – 882 lb
Useful Load 250 kg – 551 lb
Baggage allowance 20 kg – 44 lb


MTOW 650 kg

Max Cruise Speed (KTAS) 222 km/h – 120 kts
Stall Speed (Flaps Down Power Off) KCAS 81 km/h – 44 kts
Practical ceiling 4.267 mt – 14,000 ft
Take off run 207 mt – 679 ft
Take off distance 428mt – 1404 ft
Landing Run 173 mt – 568 ft
Landing Distance 302 mt – 1253 ft
Rate of climb 3,84 m/sec – 755 ft/min
Range 703 NM – 1302 km
Flight Rule VFR Day/VFR Night

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