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JL-8 (Jiaolian-8) Training aircraft-attack

JL-8 (Jiaolian-8) Training aircraft-attack. First flight: 1993 © Konstantinos Panitsidis
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Technical specifications

DESIGNER Nanchang
COUNTRY China
TYPE
Training aircraft-attack
CREW 2
POWER-PLANT One Garrett TFE731-2A (WS-11) turbofan engine
Thrust, kgf  
- with afterburning
1x1632 (1x1.710)
- without afterburner
-
DIMENSIONS
 
Length, m
11,60
Height, m
4,21
Wing span, m
9,63
Wing area m2
17,02
WEIGHT  
Maximum take-off, kg 4.330
Normal take-off, kg 3.630
Empty aircraft, kg 2.687
Internal fuel, kg 780
Weight of transported fuel with external tanks, kg 390 (2x250)
Warload, kg  1.000
PERFORMANCE  
Maximum speed, km/h 800
Cruising speed, km/h -
Maximum speed in low height, km/h 680
Combat range, km
1.400
Range, km -
Ferry range, km 2.140
Endurance (with external fuel tanks), h 4,25
Service ceiling, m 13.600
Rate of climb, m/min 1.620
Maximum overload, g 7,33
ARMAMENT Two 23 mm cannon Type 23-1. Number external hardpoints: 4. Possibility of transport 4 Air-to-air missile PL-2, PL-5, PL-7  or R.550 Magic, 4x250 kg bombs, BL755, 4x Launcher 55 mm or 90 mm or 4x pods with 30 mm or 23 mm cannons.



 


Photos JL-8 (K-8E)