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.
Categories: Advanced Ultralight

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

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.

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

Specification

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
 
 
 

 

Specifications subject to change without notice. Always consult the Aircraft Flight Manual.