.png "P2002-JF Two-seat light single (training aircraft). First flight: 2009 © Konstantinos Panitsidis")
Artistic illustration P2002 JF © Konstantinos Panitsidis
Technical specifications 
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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".
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
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 |
-
|
