P2002 Sierra MkII AUL

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.
Categories: Advanced Ultralight

Exterior

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.

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 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. .

Avionics

 

Analog Standard

 
FLIGHT INSTRUMENTS AND INDICATORS

 

Magnetic Compass
Airspeed Ind., Kts Altimeter
Vertical Speed Sideslip Indicator Pitot System Static System

 
ENGINE INSTRUMENTS

 

Tachometer
Hour Recorder
Oil Press
Oil Temp.
Cylinder Head Temp.
Fuel Press.
Voltmeter
Elevator Trim Position Indicator Flap Indicator
Lh+ Rh Fuel Qty

 
ELECTRICAL SYSTEM

 

13,2V 7 AMP Alliant Battery
14V Alternator-20 AMP. Starter Key ACS
Split Starter
Switches :
Avionic Master
Fuel Pump
Landing light
Nav light
Strobelight
Circuit Breaker
Panel 12V Socket
Flap Three Positions
Warning Light:
– Alt Out

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 55 lt – 2 x 14.5 US Gal

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

Baggage allowance 20 kg – 44 lb
Design Weight 620 kg – 1367 lb

Performance

 

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.