PPL(A), CPL(A), ATP(A) LICENCEZERO TO ATPLZERO TO ATPLCOMPLEX PILOT TRAININGIR(A) SEP, IR(A) MEP(A), FI(A)IR(A) SEP, IR(A) MEP(A), FI(A)TECNAM P2010PPL(A), CPL(A), ATP(A) LICENCECOMPLEX PILOT TRAININGCOMPLEX PILOT TRAINING

P2002 JF CS/VLA

P2002 JF CS/VLA

 

DESCRIPTION

The P2002-JF is a two-seater side by side, low wing aircraft. The JF P2002 features superlative performance and flying qualities, now confirmed by hundreds of P2002 ultralights sold throughout the world. The ease of piloting and maintenance make this aircraft an excellent solution for training in flight schools but also an ideal platform for surveillance and patrolling territory as well as, of course, for pure recreational use. The option to use AVGAS 100LL or unleaded MOGAS ASTM D4814-EN/228 SUPER make this airplane even more flexible and economical.

The P2002-JF represents the latest development of the Tecnam aircraft as result of the aircraft continuous improvement, the use of advanced software for design, the structural and fluidynamics analysis. Thanks to the tapered laminar flow airfoil and the sloned flaps the P2002 an outstanding aircraft, with the perfect mix of aerodynamic and structural efficiency.

There are many flying schools in Europe and in the rest of the world that rely on P2002JF (certified according to the CS-VLA) for students training, even up to ATPL level.

 

Construction:

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.

 

Landing gear:

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.

 

 

Interior and outdoor:

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.

 

STANDARD EQUIPMENT

FLIGHT INSTRUMENTS and INDICATORS
MAGNETIC COMPASS
AIRSPEED IND., Kts
ALTIMETER (IN)
VERTICAL SPEED
ATTITUDE GYRO
DIRECTIONAL GYRO
TURN AND BANK INDICATOR
FLAPS INDICATOR
PITOT SYSTEM
STATIC SYSTEM
STABILATOR TRIM POSITION INDICATOR
ENGINE INSTRUMENTS
RPM INDICATOR
HOUR RECORDER
OIL PRESS
OIL TEMP.
HEAD TEMP.
FUEL PRESS.
VOLTMETER
AMMETER
LH + RH FUEL QTY
OTHER INSTRUMENTS / WARNING
CHRONOMETER
O.A.T. INDICATOR
GENERATOR WARNING LIGHT
VACUUM SUCTION GAUGE
FLIGHT CONTROLS
HYDRAULIC BRAKES
PARKING BRAKE
ELECTRICAL FLAPS
DUAL FLIGHT CONTROLS
STEERABLE NOSE WHEEL
STABILATOR TRIM (Electric actuated from Stick)
ENGINE CONTROLS
- THROTTLE, TWO
- CARBURETOR HEAT
- CHOKE
FLIGHT TRIM CONTROLS
- STABILATOR with INDICATOR
FUEL CONTROL SELECTOR WITH ON/OFF
PANEL SWITCHES:
- STARTER
- FUEL PUMP
- ENGINE LH and RH IGNITION SWITCHES
ELECTRICAL SYSTEM
12 VOLT 18A AMP. BATTERY
12 VOLT ALTERNATORS-20 AMP.
SWITCHES
NAV. LIGHTS
- LANDING LIGHT
- STROBE LIGHT
EXTERNAL POWER SUPPLY RECEPTABLE
CIRCUIT BREAKER PANEL
FUEL SYSTEM
TWO INTEGRAL FUEL TANKS WITH 100 LITRES
TOTAL CAPACITY
ENGINE DRIVEN FUEL PUMP
AUXILIARY FUEL PUMPS, ELECTRIC
FUEL QUICK DRAIN
INTERIOR
PILOT AND COPILOT SEATS
ADJUSTABLE FORE AND AFT
SEAT BELTS & SHOULDER HARNESS, ALL SEATS
WALL TO WALL CARPETING
LUGGAGE COMPARTMENTS
FIRE EXTINGUISHER
RADIO CALL PLATE
SOUNDPROOFING
FIRST AID KIT
EXTERIOR
EPOXY CORROSION PROOFING, ALL STRUCTURE
SLIDING CANOPY WITH LOCK AND KEY
REAR WINDOW
TIE DOWN RINGS
MAIN WHEELS, 5,00 X 5 CLEVELAND
NOSE WHEEL, 5,00 X 5
EXTERIOR LIGHTS
NAV. LIGHTS WITH STROBE
VERTICAL TAIL STROBE
TAXI LIGHT
CABIN CONFORT SYSTEM
WINDSHIELD DEFROSTER
VENTILATOR ADJUSTABLE, 2 PLACE
HEATING 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
PROPELLER SPINNER
AIR FILTER
OIL FILTER
OIL AND WATER COOLERS
CARBURETOR HEAT WITH MANUAL CONTROL
THERMOSTAT VALVE
PRODUCT SUPPORT/DOCUMENTS
MANUFACTURERS FULL TWO YEAR LIMITED WARRANTY
PILOTS OPERATION HANDBOOK
MAINTENANCE MANUAL
PARTS CATALOG
AIRCRAFT LOG BOOK
ENGINE LOG BOOK

 

BROCHURE

BROCHURE - P2002 JF CS/VLA

 

PHOTO GALLERY

 

DETAILS