P2008
Elegant,
Comfortable and Efficient Touring
The Tecnam P2008 is a two place aircraft that combines a carbon fiber fuselage and metal wings. The result of this blending of building materials is an aircraft with an unparalleled balance of flight control feel, comfortable cross country ride and room to stretch out while still being able to take what you need with you. Going somewhere? Tecnam P2008.
Quick facts
Max Range
Fuel Capacity
2 x 55 lt – 2 x 14.5 US Gal
Max Cruise Speed
222 km/h
Seating
Two seats side by side
Fuel Consumption
Only 4.5 US Gal 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 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.
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. Km
• Altimeter Dual (In/Mb)
• Vertical Speed
• Bank Indicator
• Pitot System
• Static System
• Stabilator Trim Position Indicator
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
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 Lateral Windows Tinted
• Main Wheels, 5,00 X 5
• Nose Wheel, 5,00 X 5
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
Product Support and Documents
• Manufacturers Full Two Year Limited Warranty
• Pilots Operation Handbook
• Maintenance Manual
• Parts Catalog
Avionics
Analog Standard
• Magnetic Compass
• Airspeed Ind. Km
• Altimeter Dual (In/Mb)
• Vertical Speed
• Bank Indicator
• Pitot System
• Static System
• Stabilator Trim Position Indicator
Dynon D10 Includes:
• Tachometer
• Hour Recorder
• Oil Press
• Oil Temp.
• Head Temp.
• Fuel Press.
• Voltmeter
• Stabilator Trim Position Indicator
• Flap Indicator
• 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
Six Pack
replaces standard equipment and avionics
Attitude, Electric
Directional, Electric
Turn & Bank
Tachometer
Hour Recorder
Oil Press
Oil Temp.
Head Temp.
Fuel Press.
Voltmeter
Ammeter
Lh + Rh Fuel Qty
GARMIN GMA 245 Audio Panel NEW
GARMIN GTR 200 COM
GARMIN GTX 335 Transponder with GPS
GARMIN 796 GPS XM VERSION
Stick Push-To-Talk Switch-Pilot/Copilot
Mic & Phone Jacks-Pilot/Copilot
Antennas:
– Transponder
– VHF
– GPS
GARMIN G3X
replaces standard equipment and avionics
GDU460
GDU460
ADAHRS GSU 25
GEA 24 Engine Instrument Module
GMU 22 Magnetometer
GTP 59 Temperature Probe
LRU Kit
Installation Kit
G3X Sensor Kit
GA 56 Antenna
Amps (Ammeter Shunt Or Hall Effect)
Monitor CT
Aircraft Bus Voltages
Oil Temperature
OAT
Oil Pressure
Manifold Pressure
Fuel Pressure
RPM
Trim Indicator
Lh + Rh Fuel Qty
GARMIN GMA 245 Audio Panel NEW
GARMIN GTR 200 COM
GTX 35R Transponder mode S remote mounted
Stick Push-To-Talk Switch-Pilot/Copilot
Mic & Phone Jacks-Pilot/Copilot
Antennas:
– Transponder
– VHF
Category Upgrades
P08-1001 Advanced ULM
Includes:
– Radio Garmin Gtr 200 Com Installed
– Garmin Gtx 335 Transponder With Gps
– ELT Kannad 406 Mhz With Antenna & Remote Mounted Switch
– Parachute Galaxy 600 Kg
– Fire Sleeve On Fuel And Oil Tube
P08-1002 LSA
Includes:
– Extended Warranty For Rotax Engine (1 Year Extention)
– Landing Light Led
– External Power Receptable
– Baggage Compartment Net
– ELT Kannad 406 Mhz With Antenna & Remote Mounted Switch
P08-1003 US LSA – ADS-B OUT (Only for P08-OPT. 2 G3X)
Includes:
• GDU465 (Exchange for Std. GDU460)
• GPS 20A – ADSB OUT
• GA 37 Antenna (ADSB & XM)
P08-1004 US LSA – ADS-B IN/OUT (Only for P08-OPT. 2 G3X)
Includes:
• GDU465 (Exchange for Std. GDU460)
• GTX 45R GPS (Exch. For Std. GTX 35R)
• GPS 20A – ADSB OUT
• GA 37 Antenna (ADSB & XM)
Engine Upgrades
P08-EUP01 ROTAX 912IS
Non-Additive. Replaces all Standard Equipment.- Also Includes the following equipment:
• ENGINE ROTAX 912 IS
It requires Engine Instrument Module for the Std version 1001
P08-EUP01 ROTAX914 TURBO
Non-Additive. Replaces all Standard Equipment.
Also Includes the following equipment:
• Engine ROTAX 914 Turbo
• MAP
• SENSENICH ground adjustable 2 blades propeller (exchange for Std FIX Prop.)
P08-EUP03 ROTAX914 TURBO VP
Non-Additive. Replaces all Standard Equipment.
Also Includes the following equipment:
• Engine ROTAX 914 Turbo
• MAP
• NEUFORM V.P. PROPELLER ELECTRIC with regulator 2 Blades
Paint Schemes
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 |