£411,826
Aircraft Location:Olathe, Kansas, USA
Seller Information
View Seller InformationGeneral
Year
2016
Manufacturer
Model
Serial Number
167/US
Registration #
N167TU
Condition
Used
FlightRules
IFR
Based at
KOJC
Description
Garmin G950 Avionics with STEC 55X. Aircraft is equipped with WAAS and ADS B out.
Airframe
Total Time
1,599
Airframe
Dimensions
• Overall Height: 8.46 ft.
• Overall Length: 28.5 ft.
• Wing Span (Overall): 37.4 ft.
Performance (Based on Standard 912 S3 Powerplant)
• Max Cruise Speed KTAS: 140 Kts (75% Power)
• Stall Speed (Flaps Down Power Off) KCAS: 55 Kts
• Practical ceiling: 14,000 ft.
• Take Off Distance: 1,292 ft.
• Landing Distance: 1,145 ft.
• Rate of Climb: 1,036 ft./min
• Range: 670 NM
Engine 1
Engine 1 Make/Model
ROTAX
Engine 1 Time
1,644 SNEW
Engine 1 TBO
2000
Engine Specs
1644 SNEW
The Tecnam P2006T is equipped with two 100 HP Rotax 912 S3 powerplants. The Rotax 912 S3 is a certified engine in accordance with FAR 33. This engine offers a time between overhauls of 2,000 hours and the best power to weight ratio in its class – no surprise that this engine is the best-selling 4-stroke aircraft engine.
The Tecnam P2006T enjoys excellent fuel efficiency and wonderfully low operating costs. The aircraft can utilize Mogas (Max allowed ethanol content is 10%) or 100LL Avgas. The Tecnam P2006T’s versatility and ease of use has established it as both the aircraft of choice for Flight Training Organizations worldwide and made it popular as a touring aircraft for private flyers.
Dual Rotax 912 S3 Engines – 100 HP, 4 Cylinders
• Liquid/Air Cooled, Integrated Reduction Gear
• Dual Electronic Ignition System
• Tubular Steel Engine Mount
• Propellers - 2 MT, 2 Blades, Constant Speed, Full Feathering
• Carburetor Heat with Manual Control
• TBO 2000 Hours
Engine 2
Engine 2 Make/Model
ROTAX
Engine 2 Time
0 SNEW
Engine 2 TBO
2000
Props
Prop 1 Manufacturer
MT
Prop 1 Time
1644 SNEW
Prop 2 Manufacturer
MT
Prop 2 Time
1657 SNEW
Prop Specs
Both Props and Governors 887 hours Since Overhaul August 2023
Two MT 2 Blade, Constant Speed Full Feathering Props
Avionics
Autopilot Manufacturer
S-TEC
Autopilot Model
SYSTEM 55X
ADS-B Equipped
Yes
WAAS
Yes
Avionics/Radios
Garmin G950, STEC 55 Autopilot, WAAS
Uavionix ADS B Out
Exterior
Exterior Notes
Blue/ White
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 applied its extensive experience with aluminum airframes to create this 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 26 gallons each for a total of 52 gallons.
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 codes.
Interior
Interior Notes
Blue Leather
The generous interior dimensions of the Tecnam P2006T allow maximum space for pilots and passengers alike. With its two doors and upholstered seats complete with headrests and vertical adjustment, the cabin provides great flexibility for pilots of varying physical size to optimize 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 in-flight visibility and safe ground operations. The cabin offers a spacious luggage compartment with baggage allowance of 176 lbs.
Cabin Dimensions
• Height: 3.0 ft.
• Width: 4.0 ft.
Baggage Compartment
• Volume: 12.4 cu. ft.
• Max. Permissible Load: 176 lb.
Inspection Status
Inspection Status
Annual will be Completed 5/2026
Bird Strike Right Engine Nacelle, No Prop damage. Parts replaced with new.
Specifications are believed to be accurate and complete, however it is the responsibility of the purchaser to verify and accept the aircraft upon physical inspection of the aircraft and its records.

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