P2006T

Flexible,

economical light twin.

The Tecnam P2006T Twin has established itself as the aircraft of choice for not only the world’s most reputable Flight Training Organisations but private owners alike. A firm favorite with leading General Aviation fight-test journalists who praise its styling, handling and very low operating costs.

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Quick facts

0NM

Max Range

With this range you can use it cross country.

150 kts

Max Cruise Speed

278 km/h

0

Seating

Four seats.

0lt/h

Fuel Consumption

Only 9 Us Gal per hour both engines,
AVGAS and MOGAS Automotive Fuel

Exteriors

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.

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 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.

 

Standard Equipment

Flight instruments and indicators

Magnetic Compass
Airspeed Ind., Kts, Two
Altimeter Dual Mode (In/hP), Two
Vertical Speed
Directional Electric
Attitude Horizon Electric, Two
Turn and Slip Indicator
O.A.T.
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

Engine Instruments

Tachometer + Hour Recorder, Two
Manifold Press., Dual
Oil Press, Two
Oil Temp., Two
Coolant Temp., Two
Fuel Press., Two
Ammeter
Voltmeter
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

Flight controls

Hydraulic Toe Brakes
Parking Brake
Electric Flaps
Dual Flight Controls
Steerable Nose Wheel
Aileron Lock
Stabilator Trim (Manual)
Engine Controls
-Throttle, Two
-Propellers, Two
-Carburettor 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 RH
-Left Engine LH and RH Ignition Switches
-Right Engine LH and RH Ignition Switches

Electrical system

12 volt 35 AH GILL
12 volt alternator-40 amp, two
rocker switches internally lighted
-master switch
-landing light
-taxi light
-navigation lights
-strobe light
-pitot heat
-map light
external power supply receptical
circuit breaker panel
static discharge wicks

Fuel system

Two Integral Fuel Tanks with 200 Litres 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

Interior

Pilot and Co-Pilot Seats Simulated Leather
– Adjustable Fore and Aft
– Vertical Adjustment
Rear Passenger Seats, Two
Seat Belts & Shoulder Harness, all Seats
wall to wall Carpeting
Fire Extinguisher
Map & Storage Pockets
Radio Call Plate
Tow Bar
Soundproofing
Luggage Compartments
Overhead Cockpit Speaker
Four Position Intercom System
First Aid Kit

Interior Light

Avionics Instruments Internally Lighted
Avionics Radios Internally Lighted
Engine Instruments Internally Lighted
Flight Instruments Internally Lighted
Compass Internally Lighted
Map Light
Dimmers

Exterior

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

Exteriors lights

Nav. Lights LED with Strobe Full LED TSO
Vertical Tail Strobe
Landing/Taxi Light LED

Product Support/Documents

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

Cabin Comfort System

Windshield Defroster
Ventilator adjustable, 4 Place
Heating System

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 Blades, Constant Speed, Full Feathering
Propeller Spinner, Two
Propeller Control LH/RH
Air Filter, Two
Oil Filter, Two
Oil and Water Coolers, Two
Carburettor Heat with Manual Control

Standard GARMIN Avionics Package

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


Avionics Options

 

Standard

P2006T-Analogue Avionics

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


 

Avionics Option 1

P2006T-Garmin-G950

Garmin G950 IFR Empty Weight 845 KG

Includes the following equipment:
• G950 Integrated Flight Deck System
• GDU-1040 Primary Flight Display (PFD)
• GDU-1040 Multi-Function Display (MFD)
• GDC-74A Air Data Computer with OAT Probe
• GRS-77 AHRS
• GMU-44 Magnetometer
• GMA-1347 Digital Audio Panel with Marker Beacon/Intercom
• GTX345R Mode S Transponder ADS-B OUT
• Dual GIA-63W NAV/COM/GPS/WAAS with GS#1
• MD302 Back Up instrument
• DME – KING KN63 – Integrated control – displayed on PFD

Non-Additive. Replaces all Standard Avionics.


Avionics Option 2 – P2006T MkII

P2006T-Garmin-G950

GARMIN G1000 Nxi PACKAGE Empty Weight  845 KG

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

Non-Additive. Replaces all Standard Avionics.

Export certification requirements may require additional equipment and charges.


Paint Options


Optional Equipment

Standard Analogue Version

Code

Kg

Description

T101

5,5

KCS55A HSI Slaved Compass System (exchange for Standard DG with Heading Bug)

T102

6,0

GTN 650 Com/Nav/GPS with Antennas and inst. with GI106A Indicator

T103

6,1

GTN 750 Com/Nav/GPS with Antennas and inst. with GI106A Indicator (Exchange for Standard GTN560)

T104

5,0

KING KR87 ADF with KI 227 Indicator

Glass Version

Code

Kg

Description

T106

4,5

ADF KING KR87  (displayed on PFD)

T106/A

4,5

ADF BECKER RA4502  Remote Unit

T108

5,5

TAS 600 AVIDYNE Traf c Advisory System

T109

3,0

L-3 Storm Scope WX 500

All Versions

Code

Kg

Description

T110

9,0

Autopilot System S-TEC  55X DUAL AXIS with Automatic Electric Trim Turn Coordinator (exchange for Std TC) and DG with Heading Bug (exchange for Standard DG)

T111

3,0

Electric TRIM (S-TEC, already included in the option 110)

T112

0,5

Power Supply from built-in Generator (Max 20 Amps (each) @ 5800rpm

T113

1,5

Debris Protection

T114

1,0

Surround View Windows

T115/A

2,0

Leather Seats Two-Coloured (New Look)

T116

6,0

Special Paint two colours 

Code

Kg

Description

T116/A

5,5

Premium Luxury Interiors (Leather Seats Two- Coloured New Look and Wall side Panel Matt Gray)

T117

28

TKS System

T119

5,5

Alternators 70 Amps (Exchange for standard 40 Amps)

T122

0,5

Cabin Hole 267mm Diameter (ref. Mod. 2006_229)

T123

0,5

Cabin Hatches small (two) 359×272 + 150×150 mm (length x width) (ref. Mod. 2006_170)

T124

1,5

Tailcone Hatch 395×305 mm (lenght x width) (ref. Mod. 2006_261)

T125

 

Fuselage Cover

Specification

Aircraft Dimensions

Fuselage Height 2,58 mt – 8.46 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

Powerplant

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
Empty Weight, Standard 819 kg – 1806 lb VFR Standard
Useful Load 411 kg – 906 lb
Baggage allowance 80 kg – 176 lb

Performance

Max Cruise Speed (KTAS) 278 km/h – 150 kts
Stall Speed (Flaps Down Power Off) KCAS 102 km/h – 55 kts
Practical ceiling 4267 mt – 14,000 ft
Take off run 301 mt – 988 ft
Take off distance 394 mt – 1293 ft
Landing Run 231 mt – 758 ft
Landing Distance 349 mt – 1145 ft
Rate of climb 5.3 m/sec – 1036 ft/min
Range 669 NM – 1239 km
Flight Rule VFR Day, VFR Night, IFR

Specifications subject to change without notice. Always consult the Aircraft Flight Manual.

NASA X-57 Maxwell

NASA has selected the Tecnam P2006T twin as the airframe on which it will evaluate the potential of LEAPtech (Leading Edge Asynchronous Technology), with the aim of developing safer, more energy efficient, lower operating cost and greener general aviation aircraft.
More details here: http://www.tecnam.com/innovation/p2006t-x-57-maxwell-nasa/

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