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.
P2008 US-LSA
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.
Exteriors
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.
Avionics
Option 1 – GARMIN SIX PACK
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:
• Tachometer
• Hour Recorder
• Oil Press
• Oil Temp.
• Head Temp.
• Fuel Press.
• Voltmeter
• Ammeter
• LH + RH Fuel Q.ty
AVIONICS PACKAGE
• 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
• Antennas:
– Transponder
– Vhf
– Gps
Option 2 – GARMIN G3X
Non additive, replaces standard equipment and avionics
Garmin G3X two screens Avionics Package for For Rotax 912 Uls2 & Is
• GDU460
• GDU465
• ADAHRS GSU 25
• ADAHRS GSU 25 2nd ADAHRS
• 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)
• LRU Kit
• Installation Kit
• G3X Sensor Kit
• Back Up Airspeed. And Altimeter
GSU CONFIGURATION
• Ammeters Shunt or Hall Effect
• Monitor Cht
• Aircraft Bus Voltages
• Oil Temperature
• OAT
• Oil Pressure
• Manifold Pressure
• Fuel Pressure
• Rpm
• Trim Indicator
AVIONICS PACKAGE
• 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
• Antennas:
– Transponder
– Vhf
– Gps
Aircraft Dimensions
| Fuselage Height | 8.1 ft – 2.46 mt |
| Fuselage Length | 22.7 ft – 6.93 mt |
| Wingspan | 29.5 ft – 9 mt |
| Cabin Height (seat to cover) | 3 ft – 0.91 mt |
| Cabin Width | 3.9 ft -1.2 mt |
| Max Seating capacity | 2 |
| Fuel tank capacity | 2 x 13.7 US Gal -2 x 52 lt |
Powerplant
| Engine Manufacturer | ROTAX 912 ULS – 912is – 914 |
| Engine Power | 98 to 115 HP |
| Time Before Overhaul | 2000 hrs |
| Propeller | 2/3 Blades Fixed |
| Fuel Consumption | 4.50 US Gal/h – 17 lt/h |
| Fuel Type | Mogas and Avgas |
Design Weight & Loading
| Maximum Take Off Weight | Design Weight: 600 kg – 1320 lb |
| Empty Weight, Standard | 827 lb -375 kg |
| Useful Load | 496 lb -225 kg |
| Baggage allowance | 44 lb -20 kg |
Performance
| Max Cruise Speed (KTAS) | 120 kts – 222 km/h KTAS |
| Stall Speed (Flaps Down Power Off) KCAS | 39 kts – 72 km/h KCAS |
| Practical ceiling | 15,000 ft – 4,572mt |
| Take off run | 700 ft -214 mt |
| Take off distance | 1230 ft -375 mt |
| Landing Run | 525 ft -160 mt |
| Landing Distance | 1115 ft -240 mt |
| Rate of climb | 900 ft/min – 4.6 m/sec |
| Range | 633 NM |