The design the P2002 Sierra, Tecnam has made user of the most advanced systems of 3D design, fluid dynamics and structural analysis,
resulting in one of the best two-seater low wing aircraft in its category.
Tampered laminar flow wing, slotted flaps, up turned wing tips and a streamlined fuselage give the P2002 superlative performance,
a complete harmony of controls and style.
The resulting product is a symphony of aerodynamic and structure effectiveness with graceful, fluid flight.
Designed with the pilot in mind, this aircraft will delight even the most discerning pilot while still keeping the inexperienced pilot safe and comfortable.   

ADVANTAGES:

* Superior performance and flight characteristics
* 225 km/h (122 kts) cruise speed - stable and responsive
* High level of comfort that makes it ideal for long flights
* Excellent visibility
* Sliding canopy can be opened in flight
* Exciting, yet easy to fly

DIMENSIONS:

Wing Fuselage
Wing Span 9 m 29,5 Ft Lenght 6,6m 21,7 FT
Wing Area 11,5 mē 124 SQFT Height 2,3m 7,5 FT

SPECIFICATIONS:

Engine

 Sierra De Luxe   Sierra Turbo
Manufacturer   Rotax  
Model 912ULS2   914UL
Power 100 HP   115 HP
Number of cylinders   4  
Propeller      
Manufacturer   GT Propeller  
Model   GT  
Number of blades   2  
Type   Fix  
Designed Weight and loading   LB KG  
Designed MTOW   1320 600  
Limit loads   +4 -2 G  
Ultimate loads   +6 -3 G  
Dimension   LB KG  
Baggage allowance   44 20  
Performance mtow 472.5kg-1040 LB Sierra De Luxe   Sierra Turbo
Speed KTS        KM/H   KTS         KM/H
VMAX 132       245   139       258
Cruise speed 75%, 6500 feet 122       225   130       242
Vne   157 KTS - 290 KM/H  
At 10.000 FT/34 IN     KTS        KM/H
5.500 RPM     139       252
5.000 RPM     132       244
4.800 RPM     128       237
Stall Speed   KTS       KM/H  
Flaps down, power off   35       65  
Rate of climb at Sea level   1200FT/M   1300FT/M  
Service Ceiling 13110FT  4300M   15000FT       4572M
Take off performance FT       M   FT       M
Ground Roll 394       120   394       120
Tot. over 50 fr obstacle 721       220   722       220
Landing performance      
Ground Roll 394       120   39       120
Tot. over 50 fr obstacle 885       270   885       270
Fuel tank capacity   13,2 x 2 GAL / 50 x 2 Lt  
Consumption 4,5 GAL/Hr       17Lt./Hr   6,2 GAL/Hr       23 Lt./Hr

 

Construction Interior
* The tecnam line employs a monocoque tail cone with sheet aluminium over steel tubing for the forward section.
* The aluminium tapered wing has a conventional structure with a forward load bearing spar and a conventional rear spar. The wing halves are attached to the fuselage by a very strong carry-through made of the 2024-T3 grade aluminium fixed to the cabin truss.
* The fuel tank hold 13.2 gal/50L each, located in the wing leading edges separated from the fuselage for safety.
* The sliding canopy allows 360° of vision from the cockpit. The canopy can be opened during flight up to 70 knots.
* The all moving stabilator is fitted with a trim tab controlled by buttons on the control column.
* The ailerons are effective in allowing for a quick roll rate without being overly sensitive.
* All control surfaces are made out of aluminium.
* The canopy has full rollover protection.
  

* Seats are adjustable and increase in height as they are moved forward.
* The luggage area allows 44 pounds/20 Kg of weight and is located behind the seats with easy access in flight.
* The dual controls come standard with PTT on both sticks.
* The trim tab and the flaps are electrically activated with position indicators on the instrument panel.
* The fresh air vents are conveniently located on each side of the panel.
* The aircraft comes with dual rudder pedals with a steerable nose wheel.
* The interior is spacious, ergonomic and comfortable.
* Cabin is a roomy 44 inch / 112 cm wide.
* The wide instrument panel is designed to accomodate a full variety of instrumentation.
* Four point harness system is standard.

Landing Gear Engine and Propeller
* The main landing gear legs are made of spring steel, directly connected to the main structure. The landing gear is robust enough for rough strips and requires no maintenance.
* The trailing link nose gear uses a rubber shock absorber system that was designed for the rigours of the training environment with easy and economical maintenance.
* The main landing gear wheels and brakes are conventional aircraft size
(5.00 x 5)
* The brake lever control and the parking brake are located forward between the seats.		 * The top and bottom engine cowls are quickly and easily removable making any maintenance easier to accomplish. The top cowl has 2 large hinged openings for easy acces to the engine compartement, without the need for tools to allow effective pre-flight inspections.
* The engine's mount is steel-tubing with shock mounts. It also supports the nosewheel assembly.
* The powerplant is a Rotax 912 ULS2 series (100 HP) four-cylinder, four-stroke engine.
* The engineis a partially liquid and partially air cooled engine with an integral 1:2:4286 reduction gearbox.
* A fixed pitch wood and composite propeller comes as standard.
* The quick drain gascolator is installed in the engine compartement with eeasy outside access.
* The fuel system uses a mechanical engine driven pump along with an electrical backup pump.
* The engine installation allows the option for an additional 40 AH alternator.
* The battery is easily accesible through a hinged door in the rear fuselage.




    

Flight instruments and indicators Electrical Flaps Auxilary fuel pumps, electric fuel drain Powerplant and propeller
Magnetic compass Dual Flight controls Interior 1 Rotax 912 ULS2 100 HP, 4 cylinder
Airspeed ind., Kts Steerable Nose Wheel Pilot and copilot seats: Liquid/Air cooled, integrated reduction
Altimeter (ln) Stabilator trim (electric from stick) Adjustable for and aft (only P2002 Sierra Deluxe)
Vertical speed Engine controls: Seat belts & shoulder harness, all seats 1 Rotax 912 ULS2 115 HP, 4 cylinder
Bank indicator - Throttle, two Wall to wall carpeting Liquid/Air cooled, integrated reduction
Flaps indicator - Choke Luggage compartement (only P2002 Sierra Turbo)
Pitot system Flight Trim controls: Exterior Dual ignition system
Static system - Stabilator with indicator Sliding canopy with lock and key Throttle control Lh / Rh
Stabilator Trim position indicator Fuel control selector with on/off Rear window Tubular steel engine mount
Engine Instruments Panel switches: Tie down rings GT Propeller, 2 blade Fix
Tachometer - Starter Main wheels 5.00 x 5 (only P2002 Sierra Deluxe)
Hour recorder - Fuel pump Nose wheel 4.00 x 6 Gt Propeller, 2 blade Variable pitch
Oil press - Engine Lh + Rh ignition switches Exterior Lights (only P2002 Sierra Turbo)
Oil temp Electrical system Vertical tail strobe Propeller Spinner
Head temp 12 volt 18 Amp. battery Taxi light Air Filter
Fuel press 12 volt alternator 20 Amp. Cabin confort system Oil Filter
Voltmeter Switches: landing light - strobe light Ventilator adjustable, 2 place Oil and water coolers
Lh + Rh Fuel Qty Circuit fuses panel   Product Support/Docs
Flight Controls Fuel System   Manufactures full 2 year limited warranty
Hydraulic brakes Two integral tanks with 100 L capacity   Pilots operation handbook
Parking brake Engine driven fuel pump   Maintenance manual