Sleek and Beautiful

The Tecnam P2008 is a high wing, two place, single engine airplane equipped with tricycle landing gear. But is not only that. The P2008 incorporates a level of comfort, quality and efficiency ideal for training and touring.

Contacteaza-ne acum la 021-!

Cere o oferta de pret!


Max Range

55 x2 lt - 14,5 x2 US Gal.

Max Speed

235 km/h


Two seats side by side.

Fuel Consumption

Only 4.5 US Gal per hour, AVGAS and MOGAS Automotive Fuel


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 recognised as a stateof- the-art flight trainer too. With a choice of 3 engines, the Rotax 912ULS, 914 Turbo and the 912iS, the P2008 enjoys low operating costs. The P2008, 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.

Interiors Details

The P2008 is available with multiple automotive style interiors, paint, and avionics options along with 3 engine choices to suit your mission. With these options, flight characteristics has made the P2008 the aircraft of choice for flight training organizations as well as the private cross country aviator.



Non additive, replaces standard equipment and avionics
Flight instruments and indicators
Attitude, Electric
Directional, Electric
Turn & Bank
Trim Position Indicator
Flap Indicator

Engine analog instruments:

Hour Recorder
Oil Press
Oil Temp.
Head Temp.
Fuel Press.
LH + RH Fuel Q.ty


Garmin GMA 240 Audio Panel
Garmin GTR 200 Com
Garmin GTX 327 Transponder
Garmin 796 Gps XM Version
Stick Pushp-To-Talk Switch Pilot/Copilot
Mic & Phone Jacks Pilot/Copilot
– Transponder
– Vhf
– Gps

Option 2 – Dynon SV1000

Non additive, replaces standard equipment and avionic
Dynon Sky View SV1000 Two Screens Avionics Pack For Rotax 912 ULS2 & Is
Skyview SV 1000 10" 2 Screen Display (Includes Main Wiring Harness)
SV-EMS-221/A Engine Monitoring Module For Rotax 912
Backup Altimeter And Airspeed Indicator


Dynon SV-COM-C25 Com (25 Khz)
Dynon SV-XPNDR-261 Transponder
Garmin 796 GPS Xm Version
Stick Push-to-talk Switch-pilot/Copilot
Mic & Phone Jacks-pilot/Copilot
– Transponder
– Vhf
– Gps

Option 3 - GARMIN G3X

Non additive, replaces standard equipment and avionics
Garmin G3X two screens Avionics Package for For Rotax 912 Uls2 & Is
GEA 24 Engine Instrument Module
GMU 22 Magnetometer
GTP 59 Temperature Probe
GA 35 GPS/WAAS Antenna
GA55 XM Antenna (Tso’d-GDU 375 Only)
Installation Kit
G3X Sensor Kit
Back Up Airspeed. And Altimeter


Ammeters Shunt or Hall Effect
Monitor Cht
Aircraft Bus Voltages
Oil Temperature
Oil Pressure
Manifold Pressure
Fuel Pressure
Trim Indicator


Garmin GMA 240 Audio – Panel
Garmin GTR 200 Com
GTX 23 Transponder Mode S Remote Mounted
Stick Push-top-talk Switch-pilot/Copilot
Mic & Phone Jacks-pilot/Copilot
– Transponder
– Vhf
– Gps

Standard Equipment

Flight instruments and indicators

Magnetic Compass
Airspeed Ind. Kts
Vertical Speed
Sideslip Indicator
Pitot System
Static System
Lh + Rh Fuel Qty

Engine instruments

Dynon D10 Includes:
Hour Recorder
Oil Press
Oil Temp.
Head Temp.
Fuel Press.
Stabilator Trim Position Indicator
Flap Indicator

Flight controls

Hydraulic Toe Brakes
Parking Brake
Electrical Flaps
Dual Flight Controls
Castoring Nose Wheel
Stabilator Trim (Electric Actuated From Stick)
Engine Controls:
– Central Quadrant with Single Throttle Lever
– Choke
Flight Trim Controls:
– Stabilator Trim With Indicator
Fuel Control Selector ANDAIR

Panel switches

Split Starter
Avionics Master
Fuel Pump
Starter Key Acs

Electrical system

13.2 Volt 7 Amp. ALLIANT Battery
14 Volt Alternators-20 Amp.
– Master Switch
– Landing Light
– Nav Light
– Strobe Light
Circuit Breaker Panel
Landing/Taxi Led Light
Wing Light Green/Red, White And Strobe Aveo Full Led
12 Volt Socket
External Power Supply

Fuel system

Two Integral Fuel Tanks With 110Lt\29 US gal Total Capacity
Engine Driven Fuel Pump
Auxiliary Fuel Pump, Electric
Fuel Tank Quick Drain , Two
1 x Shut Off Valve


Pilot And Copilot Seats:
– Eco Leather
– Adjustable Fore And Aft
Seat Belts 3 Points, All Seats
Wall To Wall Carpeting
Map & Storage Pockets
Radio Call Plate
Luggage Compartments


Epoxy Corrosion Proofing, All Structure
Lh/Rh Front Door Pilot/Copilot, Lock And Key
All Windows Tinted
Main Wheels, 5,00 X 5
Nose Wheel, 5,00 X 5
Parachute Pre-Installation (No Harness)

Exteriors lights

Wing Tip Light Strobe and Position Led Light
Landing/Taxi Light Led

Cabin comfort system

Windshield Defroster
Ventilator Adjustable
Heating System

Powerplant and Propeller

Fire Wall Inox
Engines 1 Rotax 912Uls2 100 Hp, 4 Cylinders
Liquid/Air Cooled, Integrated Reduction Gear
Dual Ignition System
Throttle Control Central
Tubular Steel Engine Mount
Propeller Sensenich, 2 Blade Fixed Pitch
Propeller Spinner
2 Air Filter
Oil Filter
Oil And Water Coolers
Fire Sleeve On Fuel And Oil Tubes
Termostatic Oil Valve

Standard Avionics Package

ELT 406 Mhz With Antenna & Remote Mounted Switch

Product Support and Documents

Manufacturers Full Two Year Limited Warranty
Pilots Operation Handbook
Maintenance Manual
Parts Catalog


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


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
Fuel Type Mogas and Avgas

Design Weight & Loading

Maximum Take Off Weight Design Weight: 600 kg – 1320 lb
Std. Empty Weight 367 kg – 809 lb
Useful Load 233 kg – 511 lb
Baggage allowance 20 kg – 44 lb


Vmax 222 km/h – 120 kts
Cruise Speed 75% 219 km/h – 118 kts
Stall Speed (Flaps Down Power Off) 70 km/h – 38 kts
Pratical ceiling 4572 mt – 15,000 ft
Take off run 214 mt – 700 ft
Take off distance 360 mt – 700 ft
Landing Run 153 mt – 500 ft
Landing Distance 280 mt – 915 ft
Rate of climb 4.6 m/sec – 900 ft/min
Range 633 NM
Flight Rule

Afla mai multe despre acest tip de avion, descarcand brosura de prezentare!