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JL-8 (K-8) Chinese Jet Trainer

JL-8

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Basic Information
Name
JL-8 (K-8) Chinese Jet Trainer
Designation
JL-8
Alternate Designation
Equipment Type
Manufacturer
Hongdu Aviation Industry Corporation Pakistan Aeronautical Complex
Date of Introduction
1994
Description

The Hongdu JL-8 (Nanchang JL-8), also known as the Karakorum-8 or K-8 for short, is a two-seat intermediate jet trainer and a light attack aircraft designed in the People's Republic of China by China Nanchang Aircraft Manufacturing Corporation. Pakistan is also the co-Partner of this project. The primary contractor is the Hongdu Aviation Industry Corporation. Its export variant, K-8 Karakorum is co-produced by the Pakistan Aeronautical Complex for the Pakistan Air Force. The JL-8 / K-8 has a multi-role capability for training and, with little modification, can also be used for airfield defense. The aircraft is supposed to be as cost-effective as possible, with a short turn-around time and low maintenance requirements. The JL-8 for the domestic Chinese market and its export variants, K-8E and K-8P, have different power plants and avionics.

Air & Air Defense Specifications
Crew 2
Engine Turbofan (3500 hp)
Cruise Speed 800.0 km/h
Endurance 4.20 hrs
System
Alternate Designation(s) The Hongdu JL-8 (Nanchang JL-8), also known as the Karakorum-8 or K-8 for short.
Primary Function / Type Jet Trainer
Manufacturer Hongdu Aviation Industry Corporation Pakistan Aeronautical Complex
Crew 2 (pilot, student)
Number of Engines 1 ea
Number of Hard Points 1 x center line hard point for 23-mm cannon pod or fuel tank and 4 wing hard points
Dimensions
Length 11.60 m
Height 4.21 m
Width (Wing Span) 9.63 m
Wing Area 17.02 sq m
Empty Weight 2,687 kg
Combat Weight 700 kg
Payload 950 kg
Takeoff Clean 3,557 kg
Takeoff with Stores 4,235 kg
Automotive
Engine Name 1 x Garrett TFE-731-2A turbofan; or 1 x Progress AI-25TL turbofan
Number of Engines 1
Engine Type Turbofan
Engine Power 3,500 lb (1,588 kg) static thrust (TFE-731-2A)
Internal Fuel Capacity 780 kg
Total Fuel Capacity 1,168 kg
Cruise Speed 800 km/h
Takeoff Speed 185 km/h
Landing Speed 165 km/h
Takeoff Roll 443 m
Standing Run 533 m
Load Factor +7.33/-3.0 g
Rate of Climb 1,811 m/min
Ceiling 13,370 m
Range 2,138 km
Endurance 4.2 hours
Fire Control / Avionics
Fire Control System Type INA
Fire Control Radar INA
Navigation Radar INA
Protection
Stealth Properties None
Heat Signature Reduction INA
Add on Armor INA
NBC Protection INA
EW Counter Measures INA
Chaffs/Flares INA
Details
Country of Origin China
Category Trainers
Air > Trainers
Filter Label
J
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
11.6 m
Width
9.63 m
Height
4.21 m
Weight
700 kg
Operators (14)
China
Pakistan
Angola
Bangladesh
Bolivia
Egypt
Ghana
Myanmar
Namibia
Sri Lanka
Sudan
Venezuela
Zambia
Zimbabwe
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