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| Design weight and loading |
| Maximum take-off weight |
2712 lb |
1230 kg |
| Standard empty weight |
1874 lb |
850 kg |
| Standard useful load |
838 lb |
380 kg |
| Ultimate load factor |
+5,7g / -2,9g |
| Baggage allowance |
176 lb |
80 kg |
| Engine |
| Manufacturer |
ROTAX |
| Model |
912S3 |
| Number of cylinder |
4 |
| Take-off performance |
73,5 kW |
98 hp |
| Max. continuous performance |
69 kW |
92 hp |
| Gearbox reduction ratio |
2,43:1 |
| Propeller |
| Manufacturer |
MT PROPELLER |
| Type |
Const speed, full feathering |
| Number of blades |
2 |
| Model |
MTV-21-A-C-F/CF178-05 |
| Performance |
| Max. speed at sea level |
140 kts |
| Cruise speed (75%, 7000ft) |
131 kts |
| Cruise speed (65%, 9000ft) |
122 kts |
| Stall speed flap down |
47 kts |
| Climb rate, s.l. |
1190 ft/min |
| Climb rate, s.l. (single engine) |
300 ft /min |
| Range to 65%, 30’ reserve |
500 n.m. |
| Service ceiling (twin engine) |
14000 ft |
| Single-engine ceiling |
6000 ft |
| Take-off distance |
1476 ft |
450 m |
| Take-off run |
771 ft |
235 m |
| Landing distance |
1050 ft |
320 m |
| Landing run |
623 ft |
190 m |
| Wing span |
37,40 ft |
11,4 m |
| Wing area |
159,31 sq ft |
14,8 sqm |
| Fuselage length |
28,50 ft |
8,7 m |
| Fuselage height |
9,35 ft |
2,85 m |
| Cabin width |
48,03 in |
1,22 m |
| Cabin length (with bagg.) |
11 ft |
3,35 m |
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Flexible fuel system
MOGAS (automotive 95 oct) / AVGAS.
Twin engine
Tecnam P2006T is a twin-engine four-seat aircraft equipped with two four-cylinder four-stroke Rotax 912S3 liquid cooled engines of 100hp (73kW) each with an exceptional TBO of 2000 hours.
High wing
The superior high-wing configuration offers stability, cabin comfort and excellent visibility.
Payload capacity
P2006T is a robust yet very light airframe, resulting in an outstanding payload-to-total-weight ratio.
Fully retracting landing gear
The fully retracting landing gear allows the installation of multiple sensors on the belly avoiding reflections, obstacles and interferences thus maximizing the sensors performance.
Long endurance
Two fuel tanks are located outboard of the engines holding 200 liters in total providing 6 hours fly time.
Very low stall speed
The P2006T configuration allows stall speeds lower than 48 kts with very short take-off/landing distances (500 m) making it ideal to operate in short runways.
Advanced cockpit
The P2006T can be equipped with the most advanced IFR Glass Cockpit Display (Garmin 950) and other navigation aids like Autopilot, Synthetic Vision Display, Storm scope, DME, etc.
Safety
The cabin’s structural design ensures the required crashworthiness prescribed in recent amendments to the FAA-FAR23 and EASA-CS23 codes.
Reliability
The twin-engine configuration of the Tecnam P2006T is extremely dependable, enabling the aircraft to travel long over water distances or over rough terrain.
Maintainability
Simple and convenient access to the engine compartment allows for fast daily inspections.
Reduced operating costs
Low fuel consumption and minimum maintenance requirements convey in extremely affordable operating costs. |
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