P2002 Sierra MKII AUL
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.
Max Range 1188km 226 km/h Two seats – Side by side Only 4.5 US Gal per hour,
Max Cruise Speed
AVGAS and MOGAS Automotive Fuel
Max Range 1188km
Two seats – Side by side
Only 4.5 US Gal per hour,
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.
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 roomy baggage compartment accommodates voluminous items with both external and internal access.
A strong automotive type seal is used on the baggage door and a courtesy lamp illuminates when opened.
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.
The following list of equipment is included in the standard aircraft Analog Avionics Package and does not reflect optional equipment.
Flight instruments and indicators
· Magnetic Compass
· Airspeed Ind., (In/Mb)
· Vertical Speed
· Bank Indicator
· Pitot System
· Static System
· Hydraulic Toe Brakes
· Parking Brake
· Electrical Flaps, Preselect
· Dual Flight Controls
· Steerable Nose Wheel
· Engine Controls:
– Central Quadrant With Single Throttle Lever
· Stabilator Trim, Electric (Controlled From Stick)
· Fuel Control Selector With Lh/Rh Off (Andair)
12 VOLT 18A AMP. Battery, Alliant
12 VOLT Alternators-20 AMP.
Starter Key ACS
– Avionic Master
– Fuel Pump
– Landing light
– Nav. Light
– Strobe light
Circuit Breaker Panel
Wing Tip Strobe And Position Light LED
12 Volt socket
– Alt Out
Dynon D10 Includes:
· Hour Recorder
· Oil Press
· Oil Temp.
· Head Temp.
· Fuel Press.
· Lh+Rh fuel qty
· Stabilator Trim Position Indicator
· Flap Indicator
• Two Integral Fuel Tanks With 110Lt\29Usgal Total Capacity
• Engine Driven Fuel Pump
• Auxiliary Fuel Pump, Electric
• Fuel Tank Quick Drain , Two
• 1 X Shut Off And Fuel Selector Valve (Andair)
Powerplant and Propeller
• Inox Firewall
• Engine – 1 Rotax 912Uls2 100 Hp
• Dual Ignition System
• Throttle Control (Central)
• Tubular Steel Engine Mount
• Propeller 2 Blade Fixed Pitch Sensenich
• Propeller Spinner
• Two Air Filters
• Oil Filter
• Oil And Water Coolers
• Fire Sleeve Fuel And Oil Tubes
• Termostatic Oil Valve
• Epoxy Corrosion Proofing, All Structure
• Canopy, Lock And Key
• Tie Down Rings
• Main Wheels, 5.00 X 5 – Nose 5,00 X 5
• Wing Light Green/Red, White And Strobe Aveo Full LED
• LED Landing/Taxi Light
Wing Tip Strobe And Position Light LED
• Pilot And Co-Pilot Seats
– Longitudinally Adjustable; Covered With Synthetic Leather
• Seat Belts 4 Points All Seats
• Wall To Wall Carpeting
• Map & Storage Pockets
• Radio Call Plate
• Luggage Compartments
• Emergency Hammer
• Windshield Defroster
• Adjustable Ventilator
• Heating System
Cabin comfort system
Product Support and Documents
• Manufacturer’s Full Two Year Limited Warranty
• Pilot’s Operation Handbook
• Maintenance Manual
• Parts Catalog
|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 55 lt – 2 x 14.5 US Gal|
|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
|Baggage allowance||20 kg – 44 lb|
|Design Weight||620 kg – 1367 lb|
|Max Cruise Speed (KTAS)||122 kts- 226 km/h KTAS|
|Stall Speed (Flaps Down Power Off) KCAS||40 kt – 74 km/h KCAS|
|Practical ceiling||14,000 ft – 4267 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 – 4,69 m/sec|
|Range||642 NM – 1189 km|
Specifications subject to change without notice. Always consult the Aircraft Flight Manual.