P2002-JF Two-seat light single (training aircraft). First flight: 2009 © Konstantinos Panitsidis

Artistic illustration P2002 JF © Konstantinos Panitsidis


 Technical specifications      Photos      Video

 

 

It is a single-engine, low-wing, two-seat, training aircraft with fixed tricycle landing gear. The aircraft was developed in 2009 by the Italian "Costruzioni Aeronautiche Tecnam".
In October 11, 2018 Hellenic Air Force acquired the first aircraft for the initial training of pilots. The aircraft will join the 360th Squadron of Basic Training "Thalis".

 

P2002-JF © Konstantinos Panitsidis

On July 5, 2018, the procurement of 12 P2002JF training aircraft was signed. On Wednesday, June 12, 2019 delivery was completed for the 12 new training aircraft, TECNAM P2002JF, to the Hellenic Air Force. The P2002JF will gradually replace the available T-41D of the HAF.

 


THREE-VIEW DRAWING

P2002-JF © Konstantinos Panitsidis

 


TECHNICAL SPECIFICATIONS

DESIGNER
Tecnam
COUNTRY
Italy
TYPE
Training aircraft
CREW
2
POWER-PLANT
Bombardier-Rotax GmbH, 912S2
Power, h.p.
1 x 98,5 (constant power 92,5 h.p.)
DIMENSIONS
 
Length, m
6,61
Height, m
2,43
Wing span, m
8,60
Wing area m2
11,5
Propeller diametr, m
1,74
LANDING GEAR 
Fixed main landing gear and steerable nosewheel
Wheel track, m
1,85
Wheel base, m
1,65
WEIGHT
 
Empty aircraft, kg
337
Normal take-off, kg
-
Maximum take-off, kg
600
Useful load, kg
99
PERFORMANCE
 
Maximum speed, km/h
245
Cruising speed, 78% power, km/h
215
Stall speed (flaps), km/h
85
Takeoff speed at take-off, km/h
124
Landing speed during landing, km/h
95
Service ceiling, m
4.500
Range, km
1.100
Rate of climb, m/min
6,9
Maximum flight duration, h
5,9
Maximum overload (shunting, g)
3,8
Payload, kg 
263
- maximum weight of baggage, kg
20
ARMAMENT
-