P2002JF MkII IFR
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
IFR
The most affordable IFR trainer on the market.
Max Cruise Speed
226 km/h
Seating
Two seats side by side,
Day & Night VFR Flight Rule
Fuel Consumption
Only 4.5 US Gal per hour,
AVGAS and MOGAS Automotive Fuel
Exteriors
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.
Interiors Details
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!
Avionics
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
Option 1 NIGHT VFR
VFR NIGHT VERSION
Includes the following equipment:
- Pitot System Heated
- Instrument Light
- Emergency Light
- Map Light
- Dimmers
- Landing/Taxi Light LED
- Compass Lighted
- Alternate Static Source
- Day & Night Switch
Non additive, replaces standard avionics.
Option 2 IFR
IFR CONFIGURATION PACKAGE
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
- Dimmers
- 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
GSU 75 ADAHRS #1
GMU-44B Magnetometer
GTP59 OAT
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
Tachometer
Hour Recorder
Manifold Pressure
Oil Pressure and Temperature
Fuel Press
Fuel Flow
Lh/Rh Fuel Quantity
CHT – Cylinder Head Temperature
EGT – Exaust Gas Temperature
Ammeters
Voltmeters
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
Choke
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
Interior
Pilot And Co-Pilot Seats
– Adjustable Fore And Aft
Seat Belts, All Seats
Wall To Wall Carpeting
Hand Held Fire Extinguisher
Radio Call Plate
Soundproofing
Luggage Compartments
Cockpit Speaker
Emergency Hammer
First Aid Kit
Exterior
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
Soundproofing
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
go to the color configurator: http://colors.tecnam.com/config2018/p2002.html
Optional Equipment
|
INSTRUMENTS |
|
|
AUDIO, RADIO & NAVIGATION EQUIPMENTS |
|
|
GARMIN-COM/NAV/GPS |
|
|
120/B |
GARMIN GTR225A COM 8.33 Khz with Antenna and Installation |
|
BENDIX KING |
|
|
137 |
ADF KR 87 with KI227 Indicator |
|
OTHERS |
|
|
216 |
Power Flarm AT-1 |
|
157 |
Head Sets Clearcom, Two |
|
157/A |
Head Sets BOSE A 20, Two |
|
AIRCRAFT EQUIPMENT |
|
|
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 |
Powerplant
| 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 |
Performance
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 |