Cantor Air

Tecnam P.2008 JC – MKII I-CNTA

The Tecnam P2008JC-MKII is a high wing, two place, single engine airplane equipped with tricycle landing gear, built by TECNAM – Capua, ITALY. The P2008JC MkII has both metal wings and a metal stabilator. Tecnam chose to construct the P2008 with metal wings and stabilator structures for strength, reliability, and the ability to flex in flight, thereby ensuring a more comfortable ride. To produce the desired increase in cabin width and greater aerodynamic efficiency, Tecnam chose carbon fibre.


The wing is based on the well-known NACA63A airfoil, and through partial tapering, it is brought close to the optimal lift distribution (elliptical). The single-slot flaps extend along much of the wing span. The Frise type aileron along with the taper design provides a high rate of roll.

I CNTA


The all movable type (stabilator) horizontal tail, traditional on Tecnam aircraft, allows excellent controllability and excellent “hands off” longitudinal stability.
The P2008 JC MKII is powered with a ROTAX 912S2 100 HP, 4 Cylinders liquid/air cooled, integrated reduction gear and alimented by MOGAS or AVGAS.


I-CNTA is a P2008 JC-MKII certified for VFR and VFR-NIGHT, delivered in April 2018 directly to CANTOR Air. The ATO uses this a/c for PPL, VFR-N training and Hours Building.

 

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Specifications


General characteristics

  • Crew: 1 pilot
  • Capacity: 1 passenger
  • Fuselage Height:   2.67 mt – 8.76 ft
  • Fuselage Length:    6.97 mt – 22.87 ft
  • Wingspan:    9 mt – 29.5 ft
  • Cabin Height (seat to cover):    0.91 mt – 3 ft
  • Cabin Width:    1.2 mt – 3.9 ft
  • Max Seating capacity:    2
  • Fuel tank capacity :   2 x 55 lt – 2 x 14.5 US Gal

Powerplant

  • Engine Manufacturer    ROTAX 912 ULS – 912is – 914
  • Engine Power    98 to 115 HP
  • Time Before Overhaul    2000 hrs
  • Propeller    2/3 Blades Fixed/Ground Adj. Pitch
  • Fuel Consumption    17 lt/h – 4.50 US Gal/h
  • Fuel Type    Mogas and Avgas

 
Design Weight & Loading

  • Baggage allowance    20 kg – 44 lb
  • Design Weight    650 kg – 1433 lb

Performance

  • Max Cruise Speed (KTAS)    222 km/h – 120 kts
  • Stall Speed (Flaps Down Power Off) KCAS    72 km/h – 39 kts
  • Practical ceiling    4267 mt – 14,000 ft
  • Take off run    165 mt – 541 ft
  • Take off distance    345 mt – 1131 ft
  • Landing Run    115 mt – 377 ft
  • Landing Distance    285 mt – 935 ft
  • Rate of climb    900 ft/min – 4,57 m/sec
  • Range    703 NM -1302 km

 

 

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