P2002 JF

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.

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Quick facts

0NM

Max Range

With this range you can use it cross country.

122 kts

Max Cruise Speed

226 km/h

0

Seating

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

17 l/h

Fuel Consumption

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

Exteriors

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.

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!


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.

Avionics

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

Standard Avionics

Standard Garmin Avionics Package

GMA 340 Audio Panel
GNC 255A COM/NAV
GTX 335 Transponder ADS-B OUT
ELT 406 Mhz KANNAD
Antennas:
– Transponder
– VHF
– Marker Beacon
– ELT
Speakers
Microphone
Stick Push-To-Talk Switch-Pilot/Copilot
Mic& Phone Jacks-Pilot/Copilot


Option 1

P2002jf-VFR

VFR NIGHT VERSION
Includes the following equipment:

Heated Pitot
GILL 25A Battery
Instrument Light
Map Light
Dimmer
Aux Alternator

Non additive, replaces standard avionics.


Option 2

P2002JF-g500

GLASS COCKPIT G500
Includes the following equipment:

GARMIN G500 PFD
GTN 650 Com/Nav/Gps with Antennas and installation – exchange GNC225A
Airspeed Indicator and Altimeter back up TSO
Aux Alternator

Non additive, replaces standard avionics.


Option 3

P2002JF-g500

GLASS COCKPIT G500 + VFR NIGHT
Includes the following equipment:

GARMIN G500 PFD
GTN 650 Com/Nav/Gps with Antennas and installation – exchange GNC225A
Airspeed Ind. and Altimeter back up TSO
Heated Pitot
GILL 25A Battery
Instrument Light
Map Light
Dimmer
Aux Alternator

Non additive, replaces standard avionics.

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

Standard Equipment

Flight instruments and indicators

Magnetic Compass
Airspeed Ind., Kts
Altimeter (In)
Vertical Speed
Attitude Gyro
Directional Gyro
Turn And Bank Indicator
Flaps Indicator
Pitot System
Static System
Stabilator Trim Position Indicator

Engine Instruments

RPM Indicator
Hour Recorder
Oil Press
Oil Temp.
Head Temp.
Fuel Press.
Voltmeter
Ammeter
LH + RH Fuel Qty

Other Instruments/Warnings

Chronometer
O.A.T. Indicator
Generator Warning Light
Vacuum Suction Gauge

Flight controls

Hydraulic Brakes
Parking Brake
Electrical Flaps
Dual Flight Controls
Steerable Nose Wheel
Stabilator Trim (electric actuated from stick)
Engine Controls
_ Throttle, Two
_ Carburettor Heat
_ Choke
Flight Trim Controls
_ Stabilator With Indicator
Fuel Control Selector with On/Off
Panel Switches:
_ Starter
_ Fuel Pump
_ Engine LH And RH Ignition Switches

Electrical system

12 VOLT 18AMP. Battery
12 VOLT Alternator 20 AMP.
Switches
_Nav. Lights
_Landing Light
_Strobe Light
External Power Supply Receptable
Circuit Breaker Panel

Fuel system

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

Interiors

Pilot And Copilot Seats
_ adjustable fore and aft
Seat Belts & Shoulder Harness, all seats
Wall To Wall Carpeting
Luggage Compartments
Fire Extinguisher
Radio Call Plate
Soundproofing
First Aid Kit
Emergency Hammer

Product Support/Documents

Manufacturer Full Two Year Limited Warranty
Pilots Operation Handbook
Maintenance Manual
Parts Catalog
Aircraft Log Book
Engine Log Book

Exterior

Epoxy Corrosion Proofing, all structure
Sliding Canopy with Lock And Key
Rear Window
Tie Down Rings
Main Wheels, 5,00 X 5 Cleveland
Nose Wheel, 5,00 X 5

Exteriors lights

Nav. Lights LED with strobe AVEO Full LED TSO
Taxi Light LED

Cabin comfort system

Windshield Defroster
Ventilator Adjustable, 2 Place
Heating System

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
Propeller Spinner
Air Filter
Oil Filter
Oil And Water Coolers
Carburettor Heat with Manual Control
Thermostat Valves Oil and Water

Standard GARMIN Avionics Package

GMA 340 Audio Panel
GNC 255A COM/NAV
GTX 335 Transponder ADS-B OUT
ELT 406 Mhz KANNAD
Antennas:
– Transponder
– VHF
– Marker Beacon
– ELT
Speakers
Microphone
Stick Push-To-Talk Switch-Pilot/Copilot
Mic & Phone Jacks-Pilot/Copilot

Paint Schemes

 

 

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.

Optional Equipment

Special Controls

1006 Rudder, throttle and brakes hand controls

Instruments

114/A Turn & Slip Ind. 2 1/4″

Radio And Navigation

GARMIN COM/NAV/GPS

120/A GTR225 COM 25 Mhz with Antenna and Installation
120/B GTR225A COM 8.33 Khz with Antenna and Installation
119 MD200 VOR Indicator Only for GNC255A
121 GTN 650 Com/Nav/Gps with Antennas, Triplex & Installation with GI106A Indicator
121/A GTN 650 Com/Nav/Gps with Antennas, Triplex & Installation with GI106A Indicator (Exch. for Std. GNC255A)
122 GTN 750 Com/Nav/Gps with Antennas, Triplex & Installation with GI106A Indicator.
122/A GTN 750 Com/Nav/Gps with Antennas, Triplex & Installation with GI106A Indicator (Exch for Std. GNC255A)

GARMIN GPS

128 AERA 500 with Antenna, Panel Support and Installation
132 795 with Antenna, Panel Support and Installation

BENDIX KING

137 KR 87 ADF with KI227 Indicator
139 DME KN63-14 with KDI 572 Indicator

Other Equipment

157 Head Sets, Two
157/A BOSE A 20 Head Sets, Two

Aircraft Equipment

174 Tinted Windows
176 Toe Brakes (see note # 1)
178 Central Quadrant with single throttle lever
182 Fuselage Cover
185 Battery Gill G25 (Exchange for standard battery)
209 Control Lock
210 Towing Bar

Engine Equipment

187 Aux. Alternator

Exterior

201/A (JF) Special Paint Two Colours

 

Note:

#1 TOE BRAKES INCLUDES:

  • New Pedals
  • 4 Brakes Pumps
  • Parking Brake Selector
Specification

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

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

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