New 2018 Tecnam P2010 position available –
The Tecnam P2010 is a single engine, 4-seat, IFR-rated, high wing aircraft with a smooth, carbon fiber fuselage and metal wings for superior strength and stability. It has 2 engine options:
Standard Configuration – equipped with a 180HP Lycoming IO360
MkII model – equipped with a 215HP Lycoming IO390.
The wing is based on the well-proven NACA63A aerofoil. Through partial tapering, the design brings it close to the optimal lift distribution (elliptical). The stabilator, a trademark of all Tecnam airplanes, allows for excellent controllability and ‘hands off’ longitudinal stability.Delta Aviation is Tecnam’s exclusive dealer for Texas, California, Washington, Nevada, Oregon, Idaho, Utah, Arizona, Colorado, New Mexico, Wyoming, North Dakota, South Dakota, Alaska, Montana, and Hawaii.
Call Mark Woods at Delta Aviation (810) 417-9950.DELTA AVIATION
Email: mark@deltaaviation dot com
Airframe Options –
• Luxury Interior Upgrade
• Special PaintFAQs:
Standard Configuration – $382,912 (Lycoming IO-360 – 180 HP)
MkII version – $411,432 (Lycoming IO-390 – 215 HP with a 3 Blade Constant Speed Prop)Dimensions
• Overall Height: 8.66 ft.
• Overall Length: 26.15 ft.
• Wing Span (Overall): 33.79 ft.
Weight and Loading:
•Max Take-off Weight: 2,557 lbs.
•Empty Weight: 1,631 lbs. (Standard Configuration)
•Useful Load: 926 lbs. (Standard Configuration)
•Fuel Tank Capacity: 63 Gal.
• Max Cruise Speed KTAS: 134kts/146kts*
• Stall Speed KCAS: 52kts (Flaps down, Power off)
• Practical ceiling: 12,000ft/15,000ft*
• Take Off Run: 1,102 ft.
• Take Off Distance: 1,952 ft.
The P2010 offers 2 powerplant choices:
Standard Configuration – includes the Lycoming IO-360, 180HP engine with a high fuel capacity of 65.4 gallons. Fuel: Unleaded Aviation Fuels: UL91 or higher per ASTM D7547 or Automotive Fuels: 93 AKI or equivalent per ASTM D4814. Please refer to Lycoming Engines SI 1070 for a complete listing of approved fuels.
MkII version – includes Lycoming’s new 215 HP IO-390, which enables the plane to climb at 1,050ft/m. It provides 215HP at 2,700 rpm, coupled with a variable pitch prop. This engine can burn 100LL or UL100 fuel.
The selection of the Lycoming IO-390 to power this plane was primarily its capability to burn alternative fuels other than 100LL. The approval of this major design change by FAA set an important milestone on Tecnam’s “green transition” as the first worldwide General Aviation aircraft manufacturer able to obtain such a wide, flexible and non-single-brand related choice, as well as the first manufacturer capable of obtaining approval for use of automotive fuel on IO-360 Lycoming engine.
IO-360 Powerplant: 2 Blade MT Fixed Pitch with optional upgrade for 2 or 3 Blade MT Constant Speed Prop.
IO-390 Powerplant: Only available with G1000 Nxi and 3 Blade Constant Speed Propeller
G1000 Nxi Integrated Flight Deck System, includes:
GDU 1050 1O-inches PFD
GDU 1050 1O-inches MFD
Dual GEA 71 Engine & Airframe unit
Dual GIA 63WAAS Com/nav/GPS/GS/Loc
GMA1347 Digital audio system
GDC72 Air data computer
GTX345R Mode S Transponder (ADS-B In and OUT)ENGINE IO390 ONLY AVAILABLE WITH G1000 Nxi and VP PropellerAvionics Upgrades:
Garmin GFC 700 Autopilot
Garmin GTS 800 Traffic Advisory System
High wing aircraft with a smooth, carbon fiber fuselage and metal wings for superior strength and stability.
White Polyurethane Exterior Paint
Epoxy Corrosion Proofing, All Structure
LH/RH Front Door Pilot/Co-Pilot, Lock and Key
RH Rear Door Passenger
RH Baggage Door With Lock
Tinted Lateral Windows
Fixed Landing Gear with Castering Nose Wheel
Comfort for both pilots and passengers is provided by an expansive cabin featuring ergonomic front and rear leather seats, exceptional legroom, and easy accessibility with 3 passenger doors and a baggage door.
• Cabin Height: 3 ft. (Seat to Cover)
• Cabin Width: 3.74 ft.
• Baggage Max. Permissible Load: 88 lbs.
Airframe: 24 Months or 1000 Hours
Engine: 24 Months or 1000 Hours
Garmin Avionics: 2 year or 800 HoursSpecifications 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.
|Fuel Efficiency (mpg US): ||11.77|
|Per Seat Efficiency: ||11.77|
|Seating Options: ||1+4|
|Wing Loading lb/sq ft: ||17.1|
|Power Loading lb/hp: ||14.2|
|External Length (FT): ||25.9 ft|
|External Height (FT): ||8.8 ft|
|External Span (FT): ||33.8 ft|
|Internal Length (Overall/Net Height): ||71 in|
|Internal Width (Max/Floor): ||44 in|
|Internal Height: ||36 in|
|Baggage Area 1 Cubic Feet / Lbs: ||18 cu ft / 176 lbs|
|Engine: ||Lycoming IO-360-M1A|
|Power Output / Flat Rating: ||180|
|Engine(s) TBO (hrs): ||2000|
|Max Ramp Weight (LBS): ||2557|
|Max Takeoff Weight (LBS): ||2557|
|Max Landing Weight (LBS): ||2557|
|Zero Fuel Weight (LBS): ||1647|
|Useful Load (LBS): ||992|
|Max Fuel (LBS): ||380|
|Max Fuel (Gallons): ||63.4|
|Avail Payload Max Fuel (LBS): ||612|
|TO Distance (SL @ ISA) FT: ||804|
|Landing Distance (FT): ||1027|
|Certificated Ceiling: ||12000|
|Propeller: ||2-Blade 74 In|
|Aircraft Broker: ||DeltaAviation|
|Listing Package: ||General|