Flexible, economical light twin.

Economical Unleaded burning Rotax engines, real one engine inoperative performance and quickly configurable interior with ease of access for passengers make the P2006T ideal for personal transportation. Incredible stability in all multi engine training scenarios, sturdy trailing link retractable landing gear, and unmatched acquisition and operating costs make the P2006T ideal for Multi Engine training. Personal transportation or training the P2006T is the flexible economical light twin.

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Exteriors

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 26 US Gallons each for a total of 52 US Gallons.
A laminar flow NACA 63A airfoil of moderate thickness has been selected for the semi tapered 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. Frise 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, 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 12.36 Cubic Feet, which is easily accessible.

Standard Equipment

Flight instruments and indicators

Magnetic Compass
Airspeed Ind., Kts, Two
Altimeter Dual Mode (In/Mb), Two
Vertical Speed
Directional Electric
Attitude Horizon Electric, Two
Turn and Bank 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, Dual
Oil Press, Two
Oil Temp., Two
Head 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 and Elevator 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 35A
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 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
Two Rear Passenger Seats
Seat Belts & Shoulder Harness, All Seats
Wall To Wall Carpeting
Fire Extinguisher
Map & Storage Pockets
Radio Call Plate
Tow Bar
Soundproo ng
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 Proo ng, 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 Blade, 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 ARTEX

Avionics Options

 

Standard

P2006T-Analogue Avionics

ANALOG VERSION IFR RETRACTABLE GEAR

 

 

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 (ADSB IN and OUT)
• Dual GIA-63W NAV/COM/GPS/WAAS with GS#1
• MD302 Back Up instrument
• DME – KING KN63 – Integrated control – displayed on PFDNon-Additive. Replaces all Standard Avionics.
Export certification requirements may require additional equipment and charges.

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 (ADSB IN and OUT)
• MD302 Back Up instrument
• DME – KING KN63 – Integrated control – displayed on PFDNon-Additive. Replaces all Standard Avionics.
Export certification requirements may require additional equipment and charges.

Optional Equipment

Analog 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

KING KR87 ADF (displayed on PFD)

T106/A

4,5

BECKER RA4502 ADF 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

S-TEC Autopilot System 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 optino 110)

T112

0,5

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

T113

1,5

Debris Protection

T114

1,0

Suround View Windows

T115/A

2,0

Leather Seats Two-Coloured (New Look)

T116

6,0

Special Paint two colors T116/A

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 (lenght 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. 
 

More about Tecnam P2006T:
http://www.indracompany.com/en/noticia/indra-presents-unmanned-version-p2006t-mri-maritime-reconnaissance-intelligence-aircraft