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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.
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.
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!
Garmin G500 Txi Flight Display
GDU1060 PFD 10.6 inch color LCD touchscreen display
GSU 75 ADAHRS #1
GA 35 GPS/WAAS, antenna
Other Instruments / System / Warnings
Stall Warning Audible
GDU700P MFD/EIS Txi with Integrated ADAHRS #2
GBB 54 Battery
GEA110 Engine Interface Adapter
Oil Pressure and Temperature
Lh/Rh Fuel Quantity
CHT – Cylinder Head Temperature
EGT – Exaust Gas Temperature
Hydraulic Toe Brakes
Electrical Flaps, Preselect
Dual Flight Controls
Steerable Nose Wheel
Flight Trim Controls
-Stabilator With Indicator
Central Quadrant With Single Throttle Level
Fuel Control Selector With Lh/Rh/Off
Alternator, 12 Volt, 20 Amp
Auxiliary Alternator, 12 Volt, 40 Amp
Battery, 12 Volt,25 Amp, Gill
External Power Supply Receptacle
Circuit Breaker Panel
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
First Aid Kit
Epoxy Corrosion Proofing, All Structure
Lh/Rh Front Door Pilot/Co-Pilot, Lock And Key
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
Navigation Lights Led With Strobe Aveo Full LED TSO
Landing Light LED
Ventilator Adjustable, 2 Place
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
Shock Mounted Oil And Water Coolers
Central Quadrant With Single Throttle
Thermostat Valves Oil And Water
Engine Exhaust Muffler
Fixed Pitch 2 Blade Hoffman Propeller
Manufacturer’s Full Two Year Limited Warranty
Pilot’s Operation Handbook
Aircraft Log Book
Engine Log Book
GMA 350 Audio Panel
GTN 650 Com/Nav/Gps
GTX 335R Transponder Ads-B Out
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
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
DME KING KN63 Displayed on PDF
Pitot System Heated
Landing/Taxi Light Led
Alternate Static Source
Day & Night Switch
Static Discharge Wicks
AUDIO, RADIO & NAVIGATION EQUIPMENTS
|120/B||1,04||GARMIN GTR225A 10W COM 8.33 Khz with Antenna and Inst. (Exch.For Std GTR200)|
|137||1,27||KR 87 ADF with KI227 Indicator|
|216||Power Flarm TRX1500- AT-1|
|157||Clear-Com Headset, two|
|157/A||BOSE A20 Headset, two|
|JF-PCK||P2002 JF MkII PACKING|
Specifications subject to change without notice. Always consult the Aircraft Flight Manual.
|Fuselage Height||2.4 mt||7.9 ft|
|Fuselage Length||6.63 mt||21.7 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 55 lt||2 x 14.5 US Gal|
|Design Weight||650 kg||1433 lb|
|Empty Weight VFR Standard||410 kg||
|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|
|Max Cruise Speed (KTAS)||226 km/h||122 kts|
|Stall Speed (Flaps Down Power Off) KCAS||76 km/h||41 kts|
|Practical ceiling||4267 mt||14,000 ft|
|Take off run||240 mt||787 ft|
|Take off distance||396 mt||1,299 ft|
|Landing Run||165 mt||541 ft|
|Landing Distance||326 mt||1,069 ft|
|Rate of climb||4,3 m/sec||546 ft/min|
|Range||1.148 km||620 NM|
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