The P2002 Sierra Mk2 encompasses the latest developments in Tecnam aircraft. The use of advanced software for design, structural and fluidynamics analysis, and experience in building airplanes using all types of materials, results in continuous aircraft improvement. Due to the tapered laminar airfoil and the slotted flaps the P2002 Sierra Mk2 is an outstanding aircraft with the perfect mix of aerodynamics, performance, and structural efficiency.
The wing is all light alloy built with a single spar and full metal torsion box. The wing’s leading edges are easily detachable for repairs and also incorporate the fuel tanks (110 Lt – 29 US Gal in total). They are separated from the cabin in order to maximize passive protection. The sliding canopy allows 360° of vision in the cockpit and has full rollover protection tested via inverted drop tests.
The horizontal stabilator tail design, provides remarkable longitudinal hands-off stability along with minimum drag and weight penalty. This provides balanced two finger flight control. The wide slotted flaps, are electrically activated and allow stall speed lower than 40 Kts, and allow the aircraft to perform steep approaches and easier landings. The all alloy ailerons are effective and ensure a quick roll rate without being overly sensitive. All control surfaces are made out of light alloy and all, except for flaps and tab, are mass-balanced.
P2002 Sierra MkII US-LSA
Venerable classic,
reimagined.
This popular Tecnam classic low wing has gotten a major update and still retained its balanced flight soul. Great for training and enjoying the day in the sky.
Exterior
Interior Details
The Cabin offers newly designed seats and seat rails which are easily operated and adjustable fore and aft via a single handle with a reinforced area between the rails to make cabin access even easier. A wide cockpit panel provides plenty of room for glass panel avionics.
The largest selection of avionics choice is available on the P2002 Sierra Mk2 in order to allow almost any type of operation. With an extremely wide choice of rack-mounted avionics, including the latest Garmin radios and GPS, IFR training procedures (not in IMC conditions) can be possible. .
Avionics
Specification
Aircraft Dimensions
| Fuselage Height | 2.4 mt – 8.0ft |
| Fuselage Length | 6.74 mt – 22.11ft |
| Wingspan | 8.56 mt – 28.08 ft |
| Cabin Height (seat to cover) | 0.95 mt – 3.1 ft |
| Cabin Width | 1.11 mt – 3.6 ft |
| Max Seating capacity | 2 |
| Fuel tank capacity | 2 x 14.5 US Gal – 2 x 55 lt |
Powerplant
| Engine Manufacturer | ROTAX 912ULS2 |
| Engine Power | 98 HP |
| Time Before Overhaul | 2000 hrs |
| Propeller | Two-Bladed Fixed Pitch |
| Fuel Consumption | 17 lt/h – 4.50 US Gal/h |
| Fuel Type | Mogas and Avgas |
Design Weight & Loading
| Maximum Take Off Weight | 1323 lb – 600 kg – |
| Empty Weight, Standard | 809 lb – 367 kg |
| Useful Load | 513.7 lb – 233 kg |
| Baggage allowance | 44 lb – 20 kg |
| Design Weight | 1367 lb – 620 kg |
Performance
| Max Cruise Speed (KTAS) | 120 kts – 222 km/h KTAS |
| Stall Speed (Flaps Down Power Off) KCAS | 40 kts – 74 km/h KCAS |
| Practical ceiling | 14,000 ft – 4.267 mt |
| Take off run | 489 ft – 149 mt |
| Take off distance | 984 ft – 300 mt |
| Landing Run | 620 ft – 189 mt |
| Landing Distance | 1100 ft – 335 mt |
| Rate of climb | 923 ft/min – 4,7 mt/sec |
| Range | 642 NM – 1188 km |