Tecnam P2006T

Piston twin engine • High Wing • Retractable gear

Range Map

Origin:

nm at current load

• two fingers to move map

Payload vs. Range

Configure weights

Default: 190 lbs

Default: 30 lbs

Occupants
lb + lbs / pax

gal

Fuel on board

lbs

Extra weight

nm

Range

Available Range / nm
Mission capable. Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required. You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight. Reduce payload by lbs to safely operate this aircraft.
Extra weight is the additional payload available with your selected passengers.

Mission Profile

Endorsements & ratings:
  • Multi-Engine
  • Complex
145
KTAS
Cruise Speed
670
nm
Max Range
14,000
ft
Service Ceiling
4
Occupants
619
lbs
Wet Payload
In production Aircraft available new or used

Estimated Ownership Costs

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About the Tecnam P2006T

Type certificated 2009

Overview

The Tecnam P2006T is a four-seat light twin and the lightest certified piston twin in production. Two 100-horsepower Rotax 912 S3 engines turn constant-speed feathering propellers and burn about 9 to 10 gph total – roughly half what a legacy avgas twin drinks – on either mogas or 100LL. It pairs a high-wing aluminum airframe with retractable tricycle gear and a Garmin flight deck, and was type-certificated in 2009 (EASA.A.185; FAA A62CE, later A00067IB).

Choose the P2006T when you want genuine twin-engine redundancy and a multi-engine training platform at the lowest possible fuel and acquisition cost. At about 2,600 lb gross it is roughly 1,200 lb lighter than a Piper Seminole and burns less than half its fuel, which makes it a popular flight-school twin – though, as a light twin on modest power, it demands attentive single-engine handling. Its natural cross-shops are the diesel Diamond DA42 Twin Star and the avgas trainer twins, the Piper Seminole and Beechcraft Duchess.

Key Features for GA Buyers

  • Lightest certified piston twin. At about 2,600 lb gross it undercuts the Seminole by roughly 1,200 lb and the DA42 by more, holding down both acquisition and operating cost.
  • Twin-Rotax fuel economy. Two 100-hp Rotax 912 S3 engines burn about 9 to 10 gph total on mogas or avgas, roughly half a legacy Lycoming twin’s fuel bill.
  • Constant-speed feathering props. Two full-feathering MT propellers give real single-engine performance and the redundancy that justifies a second engine.
  • Retractable gear and glass. Retractable tricycle gear and a Garmin flight deck make it an IFR-capable multi-engine trainer and personal twin.

Trade-offs

  • Economy is fuel, not total cost. The fuel burn is half a legacy twin’s, but maintaining two Rotax engines, retractable gear, and two constant-speed props keeps the all-in hourly cost near a diesel DA42’s – the savings are at the pump, not across the board.
  • Modest single-engine margin. On two 100-hp engines the single-engine service ceiling is about 7,000 ft, and engine-out handling is less forgiving than a heavier, higher-powered twin – a virtue for training, a limit for loaded or high-terrain flying.
  • Multi-engine and complex requirements. As a retractable twin it requires multi-engine and complex endorsements, and insurance is priced for a multi-engine trainer.
  • Light-twin payload-range. Four adults with full fuel is a tight load, and real-world range is about 670 nm – well short of the optimistic marketing figures.

See Also

Technical Specifications

Dimensions & Weights

Wingspan 37.42 ft
Height
9.71 ft
Length
28.54 ft
Parking area (ft2)
1590.5 ft2
Max Takeoff Weight
Source: FAA Type Certificate Data Sheet 2,600 lbs
Useful Load
Source: third-party reference 925 lbs
Fuel Capacity
51 gal

Performance

Cruise Speed
Source: manufacturer figure 145 KTAS
Never-Exceed (VNE)
Source: FAA Type Certificate Data Sheet 167 KIAS
Max Structural Cruise (VNO)
Source: FAA Type Certificate Data Sheet 135 KIAS
Approach Speed
72 KIAS
Range
Source: third-party reference 670 NM
Service Ceiling
Source: third-party reference 14,000 ft
Rate of Climb
1036 fpm
Takeoff over 50 ft obstacle
1,293 ft
Landing ground roll
1,145 ft

Engines

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Sources

Where the figures on this page come from. Tecnam P2006T specifications are traced to published references; estimated values are flagged inline next to the figure.

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