Tecnam Airframe and Engine Hourly Cost Maintenance Program”

The Tecnam Airframe and Engine Program is an hourly cost program where the operator pays an hourly rate based on utilization which covers parts and labor for unscheduled and scheduled maintenance. The program not only provides protection from unforeseen and unscheduled maintenance expenses but also allows predictability of having a fixed budget for the operation of the aircraft or fleet.

Now US and Canadian’s buyers could select the Tecnam Airframe and Engine Program as an option at time of purchase.

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.


Full IFR

122 kts

Max Cruise Speed​ 226 km/h

2 seats

Max Comfort

17 lt/hr

Fuel Consumption


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.


Improved sliding canopy configuration ensures an easy cabin access and high internal volumes. The revised cockpit and bigger canopy ensure an improvement in terms of visibility using larger windows.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 MkII!

Standard Equipment

Flight instruments and indicators

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 instruments

GDU700P MFD/EIS Txi with Integrated ADAHRS #2
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

Fuel system

Two Integral Fuel Tanks With 100 Litres 26.4 US Gal Total Capacity
Engine Driven Fuel Pumps
Auxiliary Fuel Pump, Electric
Fuel Tank Quick Drain
Fuel Selector Valve, Left/Right/Off

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

Powerplant and Propeller

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


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/Taxi Light LED

Cabin comfort system

Windshield Defroster
Ventilator Adjustable, 2 Place
Heating System

Product Support and Documents

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

Standard Avionics 

GMA 350 Audio Panel
GTX 335R Transponder ADS-B OUT
Altitude Encoder
Avionics Master Switch
Mic & Phone Jacks Pilot/Copilot/Passengers
Hand Held Microphone
Avionics Circuit Breaker Panel
• Marker Beacon
• Transponder
• Emergency Locator Transmitter

VFR Night Package

Pitot System, Heated
Instrument Light
Emergency Light
Map Light
Compass Lighted
Alternate Static Source
Day & Night Switch

Avionic Options

Standard Avionics DAY-NIGHT VFR

Standard Garmin Avionics Package

GARMIN GDU 1060 PFD/MFD 10 inches
GARMIN GDU 700P MFD/EIS (7-inch)
GMA 350 Audio Panel
GARMIN GTN650 Com/Nav/Gps
ARMIN GMU 44B Magnetometer
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 Kannad
Lighted Compass
Alternate static Source


• Marker Beacon
• Transponder

Option 1 IFR

replaces standard equipment and avionics

Includes the following equipment:

G5 Stand-by flight instrument
GNC255A 2nd Com/Nav with Antennas and inst.
GAD43E, adapter unit for DME
DME King KN63 – Displayed on PDF
Triplexer Antenna
Static Discharge Wicks

Optional Equipment

Code Description

Becker RA 3502 ADF, includes AC3504 & CU5502

JF02 Power Flarm TRX1500-AT-1
JF03 Tinted Windows
JF04 Fuselage Cover
JF05 Coolant Operating Cabin Heating System (Exch. Std. Heating System)
JF06 Controls Locker
JF07 Towing Bar
JF08 Special Paint Two Colors
JF09 Head Sets Clearcom, Two
JF10 Head Sets BOSE A 20, Two

Paint Schemes

Go to Tecnam colors to configure your schemes: http://colors.tecnam.com/config2018/p2002.html

General Views

Technical Specifications

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


Fuselage Height 2.43 mt  7.9 ft
Fuselage Length 6.80 mt 22.3 ft
Wingspan 8.6 mt  28.2 ft

11,5 sqm

123.8 ft2

Max Seating capacity 2  
Fuel tank capacity 2 x 50 lt  2 x 13.2 US Gal

Design Weight & Loading

P2002JF MkII Fixed Pitch Propeller

Design Weight 660 kg 1455 lb
Empty Weight VFR Standard 410 kg

904 lb

Useful Load 250 kg
551 lb
Baggage allowance 20 kg 44 lb


Engine Manufacturer ROTAX 912S
Engine Power 100 HP    
Time Before Overhaul 2000 hrs    
Propeller 2 Blade Fixed Pitch  Foffman Propeller 
Fuel Consumption 17 lt/h  4.50 US Gal/h  
Fuel Type Mogas and Avgas


P2002JF MkII Fixed Pitch Propeller

Max Cruise Speed (KTAS) 226 km/h 122 kts
Stall Speed (Flaps Down Power Off) KCAS 78,7 km/h 42.5 kts
Practical ceiling 4267 mt 14,000 ft
Take off run 265 mt 869 ft
Take off distance 439 mt 1,440 ft
Landing Run 166 mt  545 ft
Landing Distance 327 mt 1,0672 ft
Rate of climb 4,1 m/sec 812 ft/min
Range  1.148 km 620 NM


Download the brochure and discover the details from test elemento P2008

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