2026 TECNAM P2006T
| Angebotspreis | Preis auf Anfrage |
|---|---|
| Standort | Morrisville |
| Erstmals gesehen | 2026-03-24 |
| Aktualisiert | 2026-08-21 |
Technische Daten
Zelle
| Baujahr | 2026 |
|---|---|
| Kennzeichen | NTBD |
Motor & Propeller
| Motorlaufzeit (TSOH) | 0 SNEW |
|---|---|
| Propellerlaufzeit (TSOH) | 0 SNEW |
Gewichte & Kraftstoff
| Nutzlast | 816 lb |
|---|
Beschreibung
The Tecnam P2006T is a lightweight, twin-engine aircraft designed to deliver exceptional performance and versatility. Powered by two Rotax 912S3 engines, each producing 100 horsepower, it achieves a maximum cruise speed of 145 knots (269 km/h) and offers a remarkable range of up to 1,100 nautical miles (2,037 km). This efficiency makes it a cost-effective solution for both private owners and flight training organizations.
The aircraft features a modern design with a high-wing configuration, providing excellent visibility and stability. Its retractable landing gear and variable-pitch propellers enhance aerodynamic efficiency, while the spacious cabin comfortably accommodates four occupants. Equipped with advanced avionics, including options for glass cockpit configurations, the P2006T ensures a sophisticated and intuitive flying experience. Certified by both EASA and the FAA, it meets rigorous safety and performance standards, solidifying its position as a leader in the light twin-engine aircraft market.
Avionik & Ausstattung
GARMIN G1000 NXi Flight Deck:
GDU 1050 10-inches PFD
GDU 1054 10-inches MFD
Dual GEA 71B Engine & Airframe unit
Dual GIA 64WAAS Com/nav/GPS/GS/Loc
GMA1360 Digital audio system
GMU44 Magnetometer
GDC72 Air data computer
GRS79 AHRS
GTP59 OAT
GTX345R Mode S Transponder (ADS-B In and OUT)
S-TEC 55 dual Axis Autopilot with Electric Trim
STANDARD GARMIN AVIONICS ALSO INCLUDES:
Altitude Encoder
Avionics Master Switch
Mic & Phone Jacks Pilot/Copilot/Passengers
Hand Held Microphone
Avionics Circuit Breaker Panel
Pilot And Co-Pilot PTT
ELT 406
Zelle
FLIGHT INSTRUMENTS AND INDICATORS:
Magnetic Compass
MD 302 Standby Attitude Module
Pitot System Heated
Static System
Alternate Static Source
Stall Warning Audible
Stabilator Trim Position Indicator
Rudder Trim Position Indicator
FLIGHT CONTROLS:
Hydraulic Toe Brakes
Parking Brake
Electric Flaps
Dual Flight Controls
Steerable Nose Wheel
Aileron Lock
Stabilator Trim (Manual)
Engine Controls
Flight Trim Controls
Landing Gear, Retractable Electro-Hydraulic
Landing Gear Selector Switch
Landing Gear Warning Horn
Landing Gear Emergency Extension
Fuel Control Selector With On/Off/Crossfeed
Overhead Panel Switches:
ELECTRICAL SYSTEM:
12 volt 35 AH GILL
12 volt alternator-40 amp, two
rocker switches internally lighted
FUEL SYSTEM:
Two Integral Fuel Tanks with 53 Gal Capacity
Engine Driven Fuel Pumps
Auxiliary Fuel Pumps
Fuel Tank Quick Drain
2 x Shut Off Valves with Cross Feed
ANTENNAS:
Marker Beacon Antenna
Transponder Antenna
VHF Antenna
NAV Ante