P2008
P2008
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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Max Range
55 x2 lt - 14,5 x2 US Gal.
Max Speed
235 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 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 | 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 | |
| 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 |
Performance
| 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 |