Low Wing, High Pleasure.
The Tecnam P2002 JF is a low wing, two place, single engine airplane equipped with tricycle landing gear. But is not only that. The P2002 JF is the plane for flying with a style, enjoying beauty inside and outside.
With this range you can use it to 226 km/h Two seats – Side by side Only 4.5 US Gal per hour,
Max Cruise Speed
Day & Night VFR Flight Rule
AVGAS and MOGAS Automotive Fuel
With this range you can use it to
Two seats – Side by side
Only 4.5 US Gal per hour,
The P2002JF is a two-seater side by side, low wing aircraft.
The P2002JF features superlative performance and flying qualities, now confirmed by hundreds of P2002 ultralights, Light Sport and VLA aircraft sold throughout the world and validated in 15 countries other than Europe.
The ease of piloting and maintenance make this aircraft an excellent solution for training in flight schools. It is also an ideal platform for surveillance and as well as, of course, for pure recreational and private use.
The option to use 100LL AVGAS or unleaded automotive fuel (with up to 10% ethanol content) makes this aircraft even more flexible and cost effective.
The P2002JF encompasses the latest developments of Tecnam aircraft. The use of advanced software for design, structural and fluidynamics analysis, and experience in building aeroplanes with all types of materials results in continuous aircraft improvement.
Due to the tapered laminar aerofoil and the slotted flaps the P2002JF is an outstanding aircraft, a perfect mix of aerodynamics, performance, and structural efficiency.
Many flight schools in Europe and all over the world rely on P2002JF (certified according to the CS-VLA and validated in several foreign countries) for students initial training. Many of them continue their training up to the ATPL with the Tecnam P2006T twin making Tecnam the ideal one-stop-shop for flight training aircraft all over the world.
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.
Heat and defrost are standard.
The fresh air vents are conveniently located in the doors.
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 conventional type instrument panel allows placement of a broad range of equipment.
Enjoy the JF!
Special Hand Controls
On March, 27th, 2014, the P2002JF aeroplane was approved by EASA to incorporate full integrated hand control kits for disabled pilots.
This makes the P2002JF the first worldwide factory-built VLA certified aircraft equipped with hand controls.
This version of the Tecnam P2002JF aircraft architecture is very simple and flexible. Flight instruction will be allowed by a third throttle control and second slip indicator on the RH side, while whomever is seated on the left side (student or disabled pilot flying solo) will:
control the stick (pitch and roll) and the brakes with the left hand;
control the rudder, throttle and flap with the right hand on the central control.
No flight control operations other than the radio and altimeter settings, will need to separate the hands from controls making this solution safe and ergonomic.
In addition to the flight control modifications, several improvements have been made to make the access to disabled pilots easier: strengthened leading edges (both LH and RH), four additional grab handles to help step inside and outside the cabin and, finally, an increased canopy opening.
Export certificate requirements may require additional equipment or a different equipment list.
Export certification requirements may require additional equipment and charges. Options also pictured.
Flight instruments and indicators
Airspeed Ind., Kts
Turn And Bank Indicator
Stabilator Trim Position Indicator
LH + RH Fuel Qty
Generator Warning Light
Vacuum Suction Gauge
Dual Flight Controls
Steerable Nose Wheel
Stabilator Trim (electric actuated from stick)
_ Throttle, Two
_ Carburettor Heat
Flight Trim Controls
_ Stabilator With Indicator
Fuel Control Selector with On/Off
_ Fuel Pump
_ Engine LH And RH Ignition Switches
12 VOLT 18AMP. Battery
12 VOLT Alternator 20 AMP.
External Power Supply Receptable
Circuit Breaker Panel
Two Integral Fuel Tanks with 100 litres total capacity
Engine Driven Fuel Pump
Auxiliary Fuel Pumps, electric
Fuel Quick Drain
1 X Shut Off And Fuel Selector Valve ANDAIR
Pilot And Copilot Seats
_ adjustable fore and aft
Seat Belts & Shoulder Harness, all seats
Wall To Wall Carpeting
Radio Call Plate
First Aid Kit
Manufacturer Full Two Year Limited Warranty
Pilots Operation Handbook
Aircraft Log Book
Engine Log Book
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
Nav. Lights LED with strobe AVEO Full LED TSO
Taxi Light LED
Cabin comfort system
Ventilator Adjustable, 2 Place
Powerplant and Propeller
Engine – 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 Fixed Pitch
Oil And Water Coolers
Carburettor Heat with Manual Control
Thermostat Valves Oil and Water
Standard GARMIN Avionics Package
GMA 345 Audio Panel
GNC 255A COM/NAV
GTX 335 Transponder ADS-B OUT
ELT 406 Mhz KANNAD
– Marker Beacon
Stick Push-To-Talk Switch-Pilot/Copilot
Mic & Phone Jacks-Pilot/Copilot
Variable Pitch Option 1
P2002 JF VP CS/VLA
Includes the following equipment:
Rotax 912 S3 100 hp Engine with Governor
Central Quadrant with single throttle and pitch lever
Hoffmann Variable Pitch Propeller
Manifold Pressure Indicator
Attitude and Directional Electric
Non-Additive. Replaces all Standard Avionics.
|1006||Rudder, throttle and brakes hand controls|
RADIO & NAVIGATION EQUIPMENT
|117/A||GMA 35 Audio Panel with Antenna and inst. (only for GTN750 exchange for std. GMA345)|
|119||MD200 VOR Indicator Only for GNC255A|
|120/B||GTR225A COM 8.33 Khz with Antenna and Installation|
|121||GTN 650 Com/Nav/Gps with Antennas, Triplex & Installation with GI106B Indicator|
|121/A||GTN 650 Com/Nav/Gps with Antennas, Triplex & Installation with GI106B Indicator (Exch. for Std. GNC255A)|
|122||GTN 750 Com/Nav/Gps with Antennas, Triplex & Installation with GI106B Indicator.|
|122/A||GTN 750 Com/Nav/Gps with Antennas, Triplex & Installation with GI106B Indicator (Exch for Std. GNC255A)|
|128||AERA 500 with Antenna, Panel Support and Installation|
|132||795 with Antenna, Panel Support and Installation|
|137||KR 87 ADF with KI227 Indicator|
|139||DME KN63-14 with KDI 572 Indicator|
|216||POWERFLARM TRX-1500 Collision Avoidance System|
|157||Head Sets, Two|
|157/A||BOSE A 20 Head Sets, Two|
|176||Toe Brakes (see note # 1)|
|178||Central Quadrant with single throttle lever|
|185||Battery GILL G25 (Exchange for standard battery)|
|201/A (JF)||Special Paint Two Colours|
ENGINE and PROPELLER EQUIPMENT
#1 TOE BRAKES INCLUDES:
- New Pedals
- 4 Brakes Pumps
- Parking Brake Selector
|Fuselage Height||2.43 mt – 8 ft|
|Fuselage Length||6.65 mt – 21.8 ft|
|Wingspan||8.6 mt – 28.2 ft|
|Cabin Height (seat to cover)||0.91 mt – 3 ft|
|Cabin Width||1.11 mt – 3.6 ft|
|Max Seating capacity||2|
|Fuel tank capacity||2 x 50 lt – 2 x 13.2 US Gal|
|Engine Manufacturer||ROTAX 912 S2/S3|
|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
|Maximum Take Off Weight||620 kg – 1367 lb|
|Empty Weight, Standard||380 kg – 838 lb|
|Useful Load||240 kg – 529 lb|
|Baggage allowance||20 kg – 44 lb|
with fixed pitch propeller
|Max Cruise Speed (KTAS)||122 kts – 226 km/h|
|Stall Speed (Flaps Down Power Off) KCAS||41 kts – 76 km/h|
|Practical ceiling||14000 ft – 4267 mt|
|Take off run||777ft – 237 m|
|Take off distance||1286ft – 392m|
|Landing Run||538 ft – 164m|
|Landing Distance||1056ft – 322m|
|Rate of climb||874 ft/min – 4,44 m/sec|
|Range||568NM – 1052km|
|Flight Rule||VFR Day/VFR Night|