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P2006 T

Two engines are better than one.

Tecnam P2006T is a twin-engine four-seat aircraft with fully retractable landing gear. The high-wing configuration offers stability, superior cabin visibility and easy access for passengers and luggage.

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Max Range

With this range you can use if cross country.

Max Speed

287 km/h


Four seats
9US gal/h

Fuel Consumption

Only 34 liters per hour both engines, AVGAS and MOGAS Automotive Fuel


Tecnam has used its extensive experience with aluminum airframes to create in the P2006T a robust yet very light airframe, resulting in an outstanding payload-to-total weight ratio. Wings are of traditional construction with integral fuel tanks located outboard of the engines, holding 100 liters each for a total of 200 liters. A laminar flow NACA 63A airfoil of moderate thickness has been selected for the semitapered wing platform offering low drag and good high altitude performance. The wide slotted aluminum flaps,electrically operated, allow stall speeds below 48kts. These flaps offer the potential for very steep approaches and short landings. Fraise ailerons allow aggressive roll rates with minimal adverse yaw. Aileron control is via internal cabin cables linked to push-rods in the wing leading edges. Particular attention was paid to the cabin's structural design in order to ensure the required crashworthiness prescribed in recent amendments to the FAA-FAR23 and EASA-CS23 codes. The Tecnam P2006T's ability to conform to such rigid safety requirements has been proven during dynamic tests carried out by a certified laboratory, demonstrating forward load factors up to 26g.

Interiors Details

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 optimize their comfort. Each seat is provided with three-point seat belts with inertia reel. 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 liters, which is easily accessible.


Standard Analogue Panel IFR

P2006T-Analogue Avionics

Option Garmin G950 IFR

Non additive, replaces standard equipment and avionic
Integrated Flight Deck System
– GMA-1347 Digital Audio Panel with Marker Beacon/Intercom
– GTX-33 Transponder-Mode S w-TIS
– GDU-1040 Primary Flight Display (PFD)
– GDU-1040 Multi-Function Display (MFD)
– GDC-74A Air Data Computer with OAT Probe
– GMU-44 Magnetometer
Backup Airspeed, Attitude, and Altimeter Internally Lighted
DME-KING KN63 integrated control displayed on PFD

Standard Equipment

Flight instruments and indicators

Magnetic Compass
Airspeed Ind., Kts
Altimeter Dual Mode (In/Mb)
Vertical Speed
Directional Electric
Attitude Horizon Electric
Turn And Bank Indicator
Pitot System, Heated
Static System
Alternate Static Source
Stall Warning Audible
Landing Gear Position Light, Three
Landing Gear-In-Transit/Not Locked Light
Stabilator Trim Position Indicator
Rudder Trim Position Indicator
Backup Attitude, Altimeter And Airspeed Indicator

Engine Instruments

Tachometer + Hour Recorder, Two
Manifold, Dual
Oil Press, Two
Oil Temp, Two
Head Temp, Two
Fuel Press., Two
Lh + Rh Fuel Qty
Annunciator Panel Lighted Push To Test:
Lh Low Fuel
Rh Low Fuel
Lh Low Oil Press
Rh Low Oil Press
Lh Low Voltage
Rh Low Voltage
Pilot Door Open

Other Instruments/Warnings

Generator Warning Light
Vacuum Suction Gauge
Warning Light:
– Alt. Out
– Fuel Pump On

Flight controls

Hydraulic Brakes
Parking Brake
Electrical Flaps
Dual Flight Controls
Steerable Nose Wheel
Aileron And Elevator Lock
Stabilator Trim (Manual)
Engine Controls:
– Throttle, Two
– Propellers, Two
– Carburetor Heat, Two
– Choke, Two
Flight Trim Controls
– Rudder With Indicator
– Stabilator With Indicator
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:
– Starter Lh And Rh
– Fuel Pump Lh And
– Left Engine Lh And Rh Ignition Switches
– Right Engine Lh And Rh Ignition Switches

Electrical system

112 Volt 23 Ah Gill 35A
12 Volt 10 Ah Spark 500
12 Volt Alternators-40 Amp, Two
Rocker Switches Internally Lighted
– Master Switch
– Landing Light
– Taxi Light
– Navigation Lights
– Strobe Light
– Pitot Heat
– Map Light
External Power Supply Receptacle
Circuit Breaker Panel
Static Discharge Wicks
Landing/Taxi Light Led

Fuel system

Two Integral Fuel Tanks With 52.83 US Gal Total Capacity
Engine Driven Fuel Pumps, Two
Auxiliary Fuel Pumps, Electric, Two
Fuel Tank Quick Drain , Two
2 X Shut Off Valves With Cross Feed


Pilot, Co-Pilot And Passenger Seats Simulated Leather
– Adjustable Fore And Aft
– Vertical Adjustment
Seat Belts & Shoulder Harness, All Seats
Wall To Wall Carpeting
Fire Extinguisher
Map & Storage Pockets
Radio Call Plate
Tow Bar
Luggage Compartments
Overhead Cockpit Speaker
Four Position Intercom System
First Aid Kit
Interior Lighting
– Pilot/Copilot Cabin Overhead Lights
– Passenger Overhead Light
– Interior Lights Dimming Control
– Avionics Radios Internally Lighted
– Compass Internally Lighted
– Map Light

Product Support/Documents

Manufacturer's Full Two – Year Limited Warranty
Pilot's Operation Handbook
Maintenance Manual
Parts Catalog
Aircraft Log Book
Engine Log Book


Epoxy Corrosion Proofing, All Structure
Lh Front Door Pilot/Co-Pilot, Lock And Key
Rh Rear Door Passenger, Lock And Key
Rear Windows
All Windows Tinted
Retractable Landing Gear
Tie Down Rings
Main Wheels, 6.00 X 6 – Nose 5,00 X 5

Cabin Comfort System

Windshield Defroster
Ventilator Adjustable, 4 Place
Heating System

Exteriors lights

Nav. Lights Led With Strobe Ave – Full Led Tso
Taxi Light Led

Powerplant and Propeller

Engines – 2 Rotax 912S3 100 Hp, 4 Cylinders
Liquid/Air Cooled, Integrated Reduction Gear
Dual Ignition System
Throttle Control Lh/Rh
Tubular Steel Engine Mount
Propellers – 2 Mt, 2 Blade, Constant Speed
Propeller Spinner, Two
Propeller Control Lh/Rh
Air Filter, Two
Oil Filter, Two
Oil And Water Coolers, Two
Carburetor Heat With Manual Control

Product support/documents

Manufacturer’s Full Two Year Limited Warranty
Pilot’s Operation Handbook
Maintenance Manual
Parts Catalog
Aircraft Log Book
Engine Log Book

Standard Avionics Package

GNC 255A COM/NAV with MD200 VOR Indicator
DME-KING KN63 with KD572 indicator
Control Wheel
Push-To-Talk Switch-Pilot/Copilot Mic & Phone
Hand Held Microphone
– Marker Beacon
– Transponder
– VHF/GPS (2)
– Emergency Locator Transmitter External

Optional Equipment

Analog Version

101 KCS55A HSI Slaved Compass System (exc. for DG with Heading Bug)
102 GNC 255ACOM/NAV with MD200 VOR Indicator
103 GTN 650 Com/Nav/Gps with Antennas and inst. With GI106A Ind.
104 GTN 750 Com/Nav/Gps with Ant, and inst. With GI106A lnd.(Exc.for GTN560)
105 ADF – KING KR87 with Kl 227 Indicator
106 DME – KING KN63 with KD572 Indicator
107 ST-360 ALTITUDE SELECTOR ALERTER (Only available with Option 112)

Glass Version

108/A RA3502 ADF Becker remote unit
109 DME-KING KN63 remote unit
111 L-3 STORM SCOPE WX 500

All Versions

112 S-TEC AUTOPILOT SYSTEM 55X DUAL AXIS with Automatic Electric Trim Turn, Coordinator (exchange for Std TC) and DG with Heading Bug (exchange Std DG)
113 ELECTRIC TRIM (S-TEC, already included in the option 112)
114 SPINNER POLISHED ALLUMINUM LOOK (Exchange for std. Spinner)
115 Power Supply from built-in Generator (Max 20 Amps (each) @ 5800rpm
116 Debris Protection
117 Suround View Windows
118 Blue Leather Seats (New Look)
120 New paint scheme painted
121 TKS
122 TKS retrofit


Aircraft Dimensions

Fuselage Height 2.85 mt – 9.35 ft
Fuselage Length 8.7 mt – 28.5 ft
Wingspan 11.4 mt – 37.4 ft
Cabin Height (seat to cover) 0.91 mt – 3 ft
Cabin Width 1.22 mt – 4 ft
Max Seating capacity 4
Fuel tank capacity 2×100 lt – 2×26.4 US Gal


Engine Manufacturer ROTAX 912 S3
Engine Power 100 + 100 HP
Time Before Overhaul 2000 hrs
Propeller Two-Bladed Constant Speed Full Feathering
Fuel Consumption 17 + 17 lt/h – 4.50 + 4.50 US Gal/h
Fuel Type Mogas and Avgas

Design Weight & Loading

Maximum Take Off Weight 1230 kg – 2712 lb
Std. Empty Weight 800 kg – 1764 lb
Useful Load 430 kg – 948 lb
Baggage allowance 80 kg – 176 lb


Vmax 287 km/h – 155 kts
Cruise Speed 75% 260 km/h – 140 kts
Stall Speed (Flaps Down Power Off) 89 km/h – 48 kts
Pratical ceiling 4572 mt – 15,000 ft
Take off run 235 mt – 771 ft
Take off distance 450 mt – 1476 ft
Landing Run 190 mt – 623 ft
Landing Distance 320 mt – 1050 ft
Rate of climb 6.1 m/sec – 1200 ft/min
Range 742 NM
Flight Rule VFR Day/VFR Night/IFR

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