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
With this range you can use it cross country.
Max Cruise Speed
Two seats side by side.
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.
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
STANDARD GARMIN G3X AVIONICS PACKAGE
- GMA 340 Audio Panel
- GNC 255A Com/Nav
- GTX 335 Transponder ADS-B OUT
- ELT 406 Mhz
– Marker Beacon
- Stick Push-To-Talk Switch, Pilot/Copilot
- Mic & Phone Jacks, Pilot/Copilot
Option 1 – GARMIN G3X VFR NIGHT PACKAGE
- Heated Pitot
- GILL 25A Battery
- Instrument Light
- Emergency Light
- Map Light
- Landing/Taxi Light Led
- Nav. Light Led
- Compass Lighted
- Alternate Static Source
- Day & Night Switch
- Analogue Indicators:
- Attitude Electric
- Oil Temp
- Warning Light:
- Pitot Heat
- Oil High Press
Export certification requirements may require additional equipment and charges.
Flight instruments and indicators
Engine Instruments, GSU Configuration
Other instruments / Indicators / Warnings
Powerplant and Propeller
Cabin comfort system
Standard GARMIN Avionics Package
|114/A||Turn & Slip Indicator 2 1/4”|
|RADIO & NAVIGATION EQUIPMENTS|
|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|
|185||Battery Gill G25 (Exchange for standard battery)|
|208||Premium Edition (includes Opt. 201)|
|201||Special Paint Two Colours|
|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|