Twin Engine
2 Rotax 912S3 100 Hp, AVGAS and MOGAS Automotive Fuel
150 kts
Max Cruise SpeedKTAS 278 km/h
669NM
Range - 1240 km
9USG/h
Only 34lt/h Us Gal per hour both engines,
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2 Rotax 912S3 100 Hp, AVGAS and MOGAS Automotive Fuel
Max Cruise SpeedKTAS 278 km/h
Range - 1240 km
Only 34lt/h Us Gal per hour both engines,
Tecnam P2006T is a twin-engine four-seat aircraft with fully retractable landing gear. The superior high-wing configuration offers stability, superior cabin visibility and easy access for passengers and luggage. Tecnam has used its extensive experience with aluminum airframes to create in the Tecnam P2006 a robust yet very light airframe, resulting in an outstanding payload-to-total weight ratio.
The wings are of traditional construction, that is essentially a mono spar configuration. Integral fuel tanks are located outboard of the engines, holding 100 litres each for a total of 200 litres.
Particular attention has been paid to the cabin’s structural design in order to ensure the required crashworthiness as prescribed in recent amendments to the FAA-FAR23 and EASA-CS23 codes.
The generous interior dimensions of the Tecnam P2006T allow maximum space for pilots and passengers alike. With its two doors, its upholstered seats complete with headrests and vertical adjustment, the cabin provides great flexibility for pilots of varying physical size to optimise their comfort. Specific care has been given to cabin interiors and acoustic comfort. The ventilation system features one vent outlet for each occupant. The heating system uniformly warms the cabin and a defrost manifold prevents the windshield from fogging up even while taxiing. Large windows, together with the high wings, provide excellent visibility for a very pleasant flight, as well as for safe ground operations. The cabin has a spacious luggage compartment of 350 litres, which is easily accessible.
Premium option makes your aircraft more precious: Alcantara leather and a dark ceiling improve your flying experience with unique ingredients. Your aircraft interiors is now more exclusive and comfortable while guaranteeing absolute compliance with the industry’s strictest standards.
ANALOGUE VERSION IFR RETRACTABLE GEAR Empty Weight 828 kg
GTN 650 COMM/NAV/GPS Multifunction Display with GI-106A VOR/LOC/GS/GPS INDICATOR
GNC 255A COM/NAV with MD200 VOR Indicator
GTX 345 TRANSPONDER ADS-B OUT
GMA 340 AUDIO PANEL
Others:
DME – KING KN63 with KD572 Indicator
MICROPHONE TELEX 100T
PILOT and CO-PILOT PTT
ELT 406
• Marker Beacon
• Transponder
• VHF
• NAV
• GPS
• ELT
Includes the following equipment:
G1000 Nxi Integrated Flight Deck System, includes:
• GDU 1050 1O-inch PFD
• GDU 1050 1O-inch MFD
• Dual GEA 71 Engine & Airframe unit
• Dual GIA 63WAAS Com/Nav/GPS/GS/LOC
• GMA1347 Digital audio system
• GMU44 Magnetometer
• GDC72 Air data computer
• GRS79 AHRS
• GTP59 OAT
• GTX345R Mode S Transponder ADS-B IN and OUT
• MD302 Back Up instrument
• DME – KING KN63 – Integrated control – displayed on PFD
• Pitot System Heated
Non-Additive. Replaces all Standard Avionics.
Specifications subject to change without notice. Always consult the Aircraft Flight Manual.
Fuselage Height 8.46 ft- 2,58 mt
Fuselage Length 28.5 ft – 8.7 mt
Wingspan 37.4 ft – 11.4 mt
Cabin Height (Seat to cover) 3 ft – 0.91 mt
Cabin Width 4 ft – 1.22 mt
Max Seating capacity 4
Fuel tank capacity 2×26.4 US Gal – 2×100 lt
Maximum Take Off Weight 2712 lb – 1230 kg
Empty Weight, Standard** 1806 lb – 819 kg – VFR Standard
Useful Load 906 lb – 411 kg
Baggage allowance 176 lb – 80 kg
Engine Manufacturer ROTAX 912 S3
Engine Power 100 + 100 HP
Propeller Two-Bladed Constant Speed Full Feathering MT Propeller
Fuel Consumption 4.50 + 4.50 US Gal/h – 17 + 17 lt/h –
Fuel Type Mogas and Avgas
Max Cruise Speed KTAS 150 kts – 278 km/h
Stall Speed (Flaps Down Power Off) KCAS 55 kts 102 km/h
Practical Ceiling 14000 ft 4267 m
Take off run 988 ft 301 m
Take off distance 1293 ft 394 m
Rate of climb 1036 ft/min – 5.3 m/sec
Landing Run 758 ft 231 m
Landing Distance 1145 ft 349 m
Range** 669 NM 1239 km
*Sea Level
**(75% + res. 30 min) max fuel
All estimated performance data are based on aeroplane weights at MTOW; standard atmospheric conditions; level, hard surface, dry runways, no wind.
We work tirelessly to deliver rigorous results ethically and honestly. We have a thorough understanding of the latest developments in the sector and what this means for clients domestically and internationally.
