The Tecnam line employs a monocoque construction style using sheet aluminium over steel tubing.
The wing is all aluminium and constructed in a conventional way with a single spar and metal torsion box.
The leading edges of the wings and are easily detachable for repairs.
The fuel tanks are each 50 Lt (13.2 gal) and are located in the leading edge separated from the fuselage for safety.
The sliding canopy allows 360° of vision in the cockpit.
The all-moving tailplane provides remarkable longitudinal hands-off stability along with minimum drag and weight penalty providing balanced, 2 finger, flight control.
The wide slotted flaps, electrically activated, allow stall speed lower than 40 Kts.
The P2002 JF has 38 degrees of flaps making steep approach landings easier.
The all aluminium 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 in flight and increase in height as they are moved forward.
The luggage area allowing for 44 pounds/20 kg of weight is located behind the seats with ample room for several travel bags.
All Tecnam aircraft have dual control sticks with a curve at the base for ease of ingress and egress.
The dual controls come standard with PTT and electric stabilator trim on the stick with a trim indicator on the panel.
The interior is spacious, ergonomic and comfortable.
Dual throttles allow the pilot to fly either left or right handed.
The fresh air vents are conveniently located on the panel.
All Tecnam aircraft provide excellent forward visibility over the cowling.
The planes come with dual conventional rudder pedals with a steerable nose wheel.
The wide instrument panel is designed to accommodate a full variety of instrumentation, from a standard 6 pack to fully integrated EFIS installations.
The all new instrument panel is modular for ease of avionics installations.
Cabin is a roomy 44 in/112 cm wide.
Four point harness system as an option.
The main landing gear is spring steel that is robust enough for unimproved strips and requires no service.
The trailing link nose gear uses a rubber shock absorber system that was designed for the rigours of the training environment.
The main landing gear wheels and brakes are conventional aircraft size (5.00x5).
The brake lever control is located forward between the seats.
A parking brake is between the seats and is actuated by use of a single twist.
The top and bottom engine cowls are quickly and easily removed making any maintenance procedure faster to accomplish.
The top cowl has 2 large hinged openings for easy access to the engine compartment for effective pre-flight inspections.
The engine is set low and the cowling slopes down from the windshield, so forward visi¬bility is excellent.
The engine is mount is Cro-Moly steel-tubing with shock mounts.
The steel firewall is soundproofed.
The power plant is a Rotax 912 S2 series four-cylinder, four-stroke engine.
The engine is a liquid and air cooled engine with an integrated 1:2.4286 reduction gear.
A fixed pitch wood and composite Hoffmann propeller comes standard.
The quick drain gascolator is installed under the cabin floor with easy access. A back-up electrical pump engages if mechanical fuel pump is out.
Circuit breakers are standard.
The battery is located in the rear of the fuselage with easy access through a hinged door. There is also an external power socket.
|FLIGHT INSTRUMENTS AND INDICATORS|
AIRSPEED IND., KTS
TURN AND BANK INDICATOR
STABILATOR TRIM POSITION INDICATOR
| ||ENGINE INSTRUMENTS|
LH + RH FUEL QTY
| ||OTHER INSTRUMENTS / WARNING|
GENERATOR WARNING LIGHT
VACUUM SUCTION GAUGE
DUAL FLIGHT CONTROLS
STEERABLE NOSE WHEEL
STABILATOR TRIM (ELECTRIC ACTUATED FROM STICK)
- THROTTLE, TWO
- CARBURETOR HEAT
FLIGHT TRIM CONTROLS
- STABILATOR WITH INDICATOR
FUEL CONTROL SELECTOR WITH ON/OFF
- FUEL PUMP
- ENGINE LH AND RH IGNITION SWITCHES
| ||ELECTRICAL SYSTEM|
12 VOLT 18A AMP. BATTERY
12 VOLT ALTERNATORS-20 AMP.
- LANDING LIGHT
- STROBE LIGHT
EXTERNAL POWER SUPPLY RECEPTABLE
CIRCUIT BREAKER PANEL
| ||FUEL SYSTEM|
TWO INTEGRAL FUEL TANKS WITH 100 LITRES
ENGINE DRIVEN FUEL PUMP
AUXILIARY FUEL PUMPS, ELECTRIC
FUEL QUICK DRAIN
PILOT AND COPILOT SEATS
ADJUSTABLE FORE AND AFT
SEAT BELTS & SHOULDER HARNESS, ALL SEATS
WALL TO WALL CARPETING
RADIO CALL PLATE
FIRST AID KIT
EPOXY CORROSION PROOFING, ALL STRUCTURE
SLIDING CANOPY WITH LOCK AND KEY
TIE DOWN RINGS
MAIN WHEELS, 5,00 X 5 CLEVELAND
NOSE WHEEL, 5,00 X 5
| ||EXTERIOR LIGHTS|
NAV. LIGHTS WITH STROBE ORION 600 FULL LED
TAXI LIGHT LED
|CABIN CONFORT SYSTEM|
VENTILATOR ADJUSTABLE, 2 PLACE
| ||POWERPLANT AND PROPELLER|
ENGINES - 1 ROTAX 912S2 100 HP, 4 CYLINDERS
LIQUID/AIR COOLED, INTEGRATED REDUCTION GEAR
DUAL IGNITION SYSTEM
THROTTLE CONTROL LH/RH
TUBULAR STEEL ENGINE MOUNT
PROPELLER - HOFFMANN, 2 BLADE FIX
CARBURETOR HEAT WITH MANUAL CONTROL
| ||PRODUCT SUPPORT/DOCUMENTS|
MANUFACTURERS FULL TWO YEAR LIMITED WARRANTY
PILOTS OPERATION HANDBOOK
AIRCRAFT LOG BOOK
ENGINE LOG BOOK
|STANDARD GARMIN AVIONICS PACKAGE|
GMA 340 AUDIO PANEL
GNC 225A COM/NAV
GTX 328 TDX
ELT 406 MHZ
STICK PUSH-TO-TALK SWITCH-PILOT/COPILOT
MIC& PHONE JACKS-PILOT/COPILOT