The sleek and beautiful lines of the single-engine Tecnam P2008 incorporate a level of comfort, quality and efficiency that have made it the ideal touring aircraft. With its carbon-fiber fuselage, metals wings and stabilator, the Tecnam P2008 has a vast number of advantages over traditional aircraft.
This combination of both composite material and metal has resulted in a more fuel efficient and much quieter aircraft. Pilots appreciate the quality and security built into this popular Tecnam design.
In service with many Flight Schools around the globe the P2008 is recognized as a state of- the-art flight trainer as well.
With a choice of 3 engines, the Rotax 912ULS, 914 Turbo and the 912iS, the P2008 enjoys low operating costs. The P2008, is Tecnam’s most cost effective and environmentally friendly aircraft.
The Tecnam P2008 is the first Tecnam aircraft fitted with the all new Rotax 912iS engine. Delivering significantly better fuel efficiency and lower operating costs than comparable light sport and ultra-light aircraft, the Tecnam P2008 is powered by the all new Rotax 912iS, reducing fuel costs, be it Mogas or Avgas, by up to a remarkable 20%.
The single-engine Tecnam P2008’s versatility and ease of use has established it as both the aircraft of choice for Flight Training Organizations worldwide as well as recreational flyers.
P2008
Exteriors
Interior Details
The P2008 is available with multiple automotive style interiors, paint, and avionics options along with 3 engine choices to suit your mission. These options allow the P2008 the aircraft of choice for flight training organizations as well as the private cross country aviator.
Standard Equipment
Flight instruments and indicators
MAGNETIC COMPASS
AIRSPEED IND.,
ALTIMETER DUAL MODE (IN/Mb)
VERTICAL SPEED
BANK INDICATOR
PITOT SYSTEM
STATIC SYSTEM
STABILATOR TRIM POSITION INDICATOR
Engine instruments
TACHOMETER
HOUR RECORDER
OIL PRESS
OIL TEMP.
HEAD TEMP.
FUEL PRESS.
VOLTMETER
LH + RH FUEL QTY
TRIM INDICATOR
FLAP INDICATOR
Flight controls
HYDRAULIC TOE BRAKES
PARKING BRAKE
ELECTRICAL FLAPS
DUAL FLIGHT CONTROLS
CASTERING NOSE WHEEL
STABILATOR TRIM (Electric actuated from Stick)
ENGINE CONTROLS
_ CENTRAL QUADRANT with SINGLE TROTTLE LEVEL
_ CHOKE
FLIGHT TRIM CONTROLS
_ STABILATOR with INDICATOR
FUEL CONTROL SELECTOR ANDAIR
PANEL SWITCHES:
_ AVIONIC MASTER
Electrical system
12 VOLT 18A AMP. BATTERY
12 VOLT ALTERNATORS-20 AMP.
SWITCHES
_Landing Light
_Strobe Light
_Nav Light
12 VOLT socket
CIRCUIT BREAKERS PANEL
Fuel system
TWO INTEGRAL FUEL TANKS WITH 110 LITRES TOTAL CAPACITY
ENGINE DRIVEN FUEL PUMP
FUEL QUICK DRAIN
Interiors
PILOT and COPILOT SEATS
_ Adjustable Fore and Aft
SEAT BELTS & Shoulder Harness, All Seats
WALL TO WALL CARPETING
MAP E STORAGE POCKETS
LUGGAGE COMPARTMENTS
Exterior
EPOXY CORROSION PROOFING, All structure
LH/RH FRONT DOOR Pilot/Copilot, Lock and Key
ALL LATERAL WINDOWS TINTED FUME’
MAIN WHEELS, 5,00 X 5
NOSE WHEEL, 5,00 X 5
Exteriors lights
WING LIGHT GREEN/RED, WHITE AND STROBE AVEO NON TSO
LANDING LIGHT
Cabin comfort system
WINDSHIELD DEFROSTER
VENTILATOR ADJUSTABLE, 2 place
HEATING SYSTEM
Powerplant and Propeller
ENGINES – 1 ROTAX 912ULS2 100 HP, 4 Cylinders
liquid/air cooled, integrated reduction gear
DUAL IGNITION SYSTEM
THROTTLE CONTROL
TUBULAR STEEL ENGINE MOUNT
PROPELLER – SENSENICH or GT Propeller, 2 Blade fix
PROPELLER SPINNER
AIR FILTER
OIL FILTER
OIL AND WATER COOLERS
Product Support and Documents
MANUFACTURERS FULL TWO YEAR LIMITED WARRANTY
PILOTS OPERATION HANDBOOK
MAINTENANCE MANUAL
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 | 1.2 mt – 3.9 ft |
| Max Seating capacity | 2 |
| Fuel tank capacity | 2 x 55 lt – 2 x 14.5 US Gal |
Powerplant
| Engine Manufacturer | ROTAX 912 ULS – 912is – 914 |
| Engine Power | 98 to 115 HP |
| Time Before Overhaul | 2000 hrs |
| Propeller | 2/3 Blades Fixed/Ground Adj. Pitch |
| Fuel Consumption | 17 lt/h – 4.50 US Gal/h |
| Fuel Type | Mogas and Avgas |
Design Weight & Loading
| Baggage allowance | 20 kg – 44 lb |
| Design Weight | 650 kg – 1433 lb |
Performance
| Max Cruise Speed (KTAS) | 222 km/h – 120 kts |
| Stall Speed (Flaps Down Power Off) KCAS | 72 km/h – 39 kts |
| Practical ceiling | 4267 mt – 14,000 ft |
| Take off run | 165 mt – 541 ft |
| Take off distance | 345 mt – 1131 ft |
| Landing Run | 115 mt – 377 ft |
| Landing Distance | 285 mt – 935 ft |
| Rate of climb | 900 ft/min – 4,57 m/sec |
| Range | 703 NM -1302 km |