Smart IFR Training

The Tecnam P2002 JF MkII IFR is a low wing, two place, single engine airplane equipped with tricycle landing gear and now with IFR certification.

The P2002 JF MkII IFR is the plane for the most modern and affordable IFR training.

Quick facts


NEW 2019

The most affordable IFR trainer on the market.

Max Cruise Speed

Put starting value here (e.g. 0)kts

226 km/h



Two seats side by side,
Day & Night VFR Flight Rule

Full Consumption

Put starting value here (e.g. 0)l/h

Only 4.5 US Gal  per hour,
AVGAS and MOGAS Automotive Fuel


The P2002JF MkII is a two-seater side by side, low wing aircraft. The P2002JF MkII 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 MkII 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. Now they can continue their training up to the ATPL with the P2002JF MkII or with Tecnam P2006T twin for multi engine rating, making Tecnam the ideal one-stop-shop for flight training aircraft all over the world.

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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!

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Export certificate requirements may require additional equipment or a different equipment list.

Standard Avionics Day VFR

Standard Garmin Avionics Package

GMA 350 Audio Panel
GTN 650 Com/Nav/Gps
GTX 335R Transponder Ads-B Out
Altitude Encoder
Avionics Master Switch
Mic & Phone Jacks Pilot/Copilot/Passengers Hand Held Microphone
Avionics Circuit Breaker Panel
Pilot And Co-Pilot Ptt
ELT 406 Artex

Marker Beacon

Option 1 Night VFR

Includes the following equipment:

Pitot System Heated
Instrument Light
Emergency Light
Map Light

Landing/Taxi Light LED
Compass Lighted
Alternate Static Source
Day & Night Switch

Non additive, replaces standard avionics.

Option 2 IFR

Non-Additive. Replaces all Standard Equipment.- Also Includes the following equipment:

GNC255A 2nd Com/Nav with Antennas and inst.
GDU 700/1060 ADC, Unit Only
GMU44B, 2nd AHRS Unit Only
GTP59, 2nd OAT
GBB 54 , Backup battery
GAD43E, adapter unit for DME
Triplexer Antenna
DME KING KN63 Displayed on PDF
Pitot System Heated
Instrument Light

Emergency Light
Map Light
Landing/Taxi Light Led
Compass Lighted
Alternate Static Source
Day & Night Switch
Static Discharge Wicks

Export certification requirements may require additional equipment and charges. Options also pictured.

Standard Equipment

Garmin G500 Txi Flight Display
GDU1060 PFD 10.6 inch color LCD touchscreen display
GMU-44B Magnetometer
GA 35 GPS/WAAS, antenna

Other Instruments / System / Warnings
Magnetic Compass
Static System
Stall Warning Audible

Engine Indication System Display
GDU700P MFD/EIS Txi with Integrated ADAHRS #2
GBB 54 Battery
GEA110 Engine Interface Adapter
Hour Recorder
Manifold Pressure
Oil Pressure and Temperature
Fuel Press
Fuel Flow
Lh/Rh Fuel Quantity
CHT – Cylinder Head Temperature
EGT – Exaust Gas Temperature

Flight Controls
Hydraulic Toe Brakes
Parking Brake
Electrical Flaps, Preselect
Dual Flight Controls
Steerable Nose Wheel
Flight Trim Controls
-Stabilator With Indicator
Engine Controls
Central Quadrant With Single Throttle Level
Carburettor Heat
Fuel Control Selector With Lh/Rh/Off

Electrical System
Alternator, 12 Volt, 20 Amp
Auxiliary Alternator, 12 Volt, 40 Amp
Battery, 12 Volt,25 Amp, Gill
Rocker Switches
-Master Switch
Fuel Pump
-Landing Light
-Navigation Lights
-Strobe Light
External Power Supply Receptacle
Circuit Breaker Panel

Fuel System
Two Integral Fuel Tanks With 100 Litres 26.41 US Gal Total Capacity
Engine Driven Fuel Pumps
Auxiliary Fuel Pump, Electric
Fuel Tank Quick Drain
Fuel Selector Valve, Left/Right/Off

Pilot And Co-Pilot Seats
– Adjustable Fore And Aft
Seat Belts, All Seats
Wall To Wall Carpeting
Hand Held Fire Extinguisher
Radio Call Plate
Luggage Compartments
Cockpit Speaker
Emergency Hammer
First Aid Kit

Epoxy Corrosion Proofing, All Structure
Lh/Rh Front Door Pilot/Co-Pilot, Lock And Key
Rear Window
All Lateral Windows Tinted
Fixed Landing Gear
White Polyurethane Exterior Paint
Tie Down Rings
Main Wheels, 5.00 X 6
Nose Wheel, 5.00 X 5

Exterior Lights
Navigation Lights Led With Strobe Aveo Full Led Tso
Landing Light Led

Cabin Comfort System
Windshield Defroster
Ventilator Adjustable, 2 Place
Heating System

Powerplant & Accessories
Engine – 1 Rotax 912S2 100 Hp, 4 Cylinders Liquid/Air Cooled, Integrated Reduction Gear
Dual Ignition System
Tubular Steel Engine Mount
Carburettor Heat With Manual Control
Electric Starter
Shock Mounted Oil And Water Coolers
Central Quadrant With Single Throttle
Choke Control
Thermostat Valves Oil And Water
Engine Exhaust Muffler
Fixed Pitch 2 Blade Hoffman Propeller
Propeller Spinner

Product Support/Documents
Manufacturer’s Full Two Year Limited Warranty
Pilot’s Operation Handbook
Maintenance Manual
Parts Catalogue
Aircraft Log Book
Engine Log Book

Paint Schemes

More colors? Click here 

Optional Equipment

120/B GARMIN GTR225A COM 8.33 Khz with Antenna and Installation 
137 ADF KR 87 with KI227 Indicator
216 Power Flarm AT-1
157 Head Sets Clearcom, Two
157/A Head Sets BOSE A 20, Two
174 Tinted Windows
182 Fuselage Cover
209 Control Lock
210 Towing Bar


Aircraft Dimensions

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

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Specifications subject to change without notice. Always consult the Aircraft Flight Manual.