P2006 Twin

The second prototype of the TECNAM P2006T - with analogue instruments - made its maiden flight on 9 June 2008. All test flights conducted to date have clearly confirmed the positive characteristics and performances found on the first prototype of this twin-engine light aircraft.
Static tests and further flight tests are nearing completion and, based on the latest test program written with ENAC, we expect to receive the Type Certification for this analogue version at the beginning of October 2008. Certification for the Garmin 950 version of the TECNAM Twin will follow shortly thereafter. In the meantime, the production program has commenced and we anticipate the first TECNAM P2006T Twin aircraft to be delivered to clients by the end of October this year.

DIMENSIONS	ft	m	ENGINE
Wing Span	34.8 ft	10.6 m	Manufacturer	ROTAX
Wing Area	155.0 sq ft	14.4. sq m	Model	912 S
Fuselage Length	28.4 ft	8.66 m	Number of Cylinders	4
Fuselage Height	9.4 ft	2.85 m	Take-off Performance	73.5 kw 98 hp
Cabin Width	47.2 ft	1.20 m	Max Continuous Performance	69 kw 92 hp
Cabin Length	8.2 ft	2.5 m	Gearbox Reduction Ratio	2.43:1

PERFORMANCES		WEIGHT	lb	kg
Max speed at sea level	153kts/83 km/h	Maximum Take-Off Weight	2425lb	1100kg
Cruise speed (75%, 7000ft)	147 kts/272 km/h	Maximum Ramp Weight	2425lb	1100kg
Cruise speed (65%, 9000ft)	141 kts/261 km/h	Standard Equipped Weight	1411lb	640kg
Stall speed flap up	53.5 kts/99 km/h	Standard Useful Load	1014lb	460kg
Stall speed flap down	48 kts/89 km/h	Baggage Allowance	132lb	60kg
Climb rate, s.l.	1360ft/min/6.9 m/s
Climb rate, s.l. (single engine)	380 ft/min/1.9 m/s
Range to 75%, 30' reserve	610 nm/1130 km
Range to 65%, 30' reserve	710 nm/1315 km
Service ceiling (twin engine)	16,007 ft/4880 m
Service ceiling (single engine)	6690/2040 m
Takeoff roll	738 ft/225 m
Takeoff (50' obstacle)	1378 ft/420 m
Landing roll	591 ft/180 m
Landing (50' obstacle)	1115 ft/340 m