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.

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Quick facts

0NM

Max Range

Fuel Capacity
2 x 14.5 US Gal – 2 x 55 lt

120 kts

Max Cruise Speed

222 km/h

0

Seating

Two seats side by side

4.5
US Gal/h

Fuel Consumption

Only 17 lt per hour, AVGAS and MOGAS Automotive Fuel

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 – 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-ADAHRS-200
• SV-ADAHRS-201
• SV-EMS-221/A Engine Monitoring Module For Rotax 912
• SV-GPS-250
• SV-BAT-320
• Backup Altimeter And Airspeed Indicator

AVIONICS PACKAGE

• Dynon SV-INTERCOM-2S
• 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
• Antennas:
– 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
• 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

Standard Equipment

Flight instruments and indicators

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

Engine instruments

Dynon D10 Includes:
• Tachometer
• Hour Recorder
• Oil Press
• Oil Temp.
• Head Temp.
• Fuel Press.
• Voltmeter
• 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.
• Switches:
– 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

Interiors

• 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
• Soundproofing
• Luggage Compartments

Exterior

• 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

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) 0.91 mt -3 ft
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.

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