P2008 JC MKII
Innovation is in the air.
Now even more!
The Tecnam P2008JC is a high wing, two place, single engine airplane equipped with tricycle landing gear. But is not only that. The P2008JC MkII is up-to-date technology with composite fuselage, safe and easy flying with beauty, inside and outside.
The Tecnam P2008JC MkII is delivered in full compliance with the requirements of
About 1300 km range 222 km/h Two seats – Side by side More than enough for 2 persons and some luggage.
Max Cruise Speed
About 1300 km range
Two seats – Side by side
More than enough for 2 persons and some luggage.
The P2008JC MkII 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 MkII is designed to allow you and your passenger to experience the most outstanding style, comfort, and beauty of flight..
Enjoy the P2008JC MkII!
Export certification requirements may require additional equipment and charges.
DUAL DISPLAY GDU 460 SYSTEM WITH EIS
Two GDU 460 Display
Two GSU25 ADAHRS
GEA 24 Unit Only
GMU 22, Unit only
G3X Installation Kit
Two GSU 25 Inst & Conn. Kit
GEA 24 Conn. kit
GMU 22 Connector and install rack kit
GAP 26 unheated
Hydraulic Toe Brakes
Electrical Flaps, preselect
Dual Flight Controls
Castering Nose Wheel
Stabilator Trim (Electric actuated from stick)
OTHER INSTRUMENTS / INDICATORS / WARNINGS
Fuel Indicator RH and LH
– Low Oil pressure
– Low Fuel pressure
– Alt. Out
– Fuel Pump ON
_ Central Quadrant With Single Throttle Lever
Flight Trim Controls
_ Stabilator with Indicator
Fuel Control Selector ANDAIR
_ Split Starter
Starter Key ACS
12 VOLT 18A AMP. Battery FIAMM 64
12 VOLT Alternator 20 AMP.
12 VOLT socket
External Power Supply Receptical
Auxiliary Alternator 40A
Circuit Breaker Panel
Two Integral Fuel Tanks With 120 Litres Total Capacity
Engine Driven Fuel Pump
Fuel Quick Drain
Electrical Fuel Pump
Pilot And Copilot Seats
_ Adjustable Fore and Aft
Seat Belts & Shoulder Harness, All Seats
Wall To Wall Carpeting
Map and Storage Pockets
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
Nav. Lights LED with strobe AVEO full LED TSO
Taxi Light LED
CABIN COMFORT SYSTEM
Ventilator Adjustable, 2 Place
POWERPLANT AND PROPELLER
ENGINE – 1 ROTAX 912S2 100 HP, 4 Cylinders
liquid/air cooled, integrated reduction gear
Dual Ignition System
Tubular Steel Engine Mount
Propeller – Hoffman, 2 Blade Fix
Oil And Water Coolers
Carburetor Heat With Manual Control
Thermostat Valve Water And Oil
Manufacturers Full Two Year Limited Warranty
Pilots Operation Handbook
Aircraft Log Book
Engine Log Book
STANDARD GARMIN AVIONICS PACKAGE
GMA 345 Audio Panel
GNC 255A Com/Nav
GTX 335 Transponder ADS-B OUT
ELT 406 Mhz
– 35 GPS/WAAS
– Marker Beacon
Stick Push-To-Talk Switch, Pilot/Copilot
Mic & Phone Jacks, Pilot/Copilot
|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||382 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.