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JL-9 (FTC-2000 Mountain Eagle) Chinese Supersonic Advanced Attack Aircraft

JL-9

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Basic Information
Name
JL-9 (FTC-2000 Mountain Eagle) Chinese Supersonic Advanced Attack Aircraft
Designation
JL-9
Alternate Designation
Equipment Type
Manufacturer
Guizhou Aviation Industry Import/Export Company (GAIEC)
Date of Introduction
2003
Description

The Guizhou JL-9, also known as the FTC-2000 Mountain Eagle, is a two-seat supersonic fighter-trainer developed by the Guizhou Aviation Industry Import/Export Company (GAIEC) for the People's Liberation Army Air Force (PLAAF) and the People's Liberation Army Naval Air Force (PLANAF). The FTC-2000 is a JJ-7/FT-7 with a new wing, a forward fuselage with side air intakes, and a glass cockpit. The engine, empennage, and mechanical controls of the JJ-7/FT-7 are retained. The FTC-2000G is a multi-role combat fighter aircraft and one of the cheapest multirole fighters on the market with the aim to replace old legacy fighters like the J-7/F-7. It has 7 hardpoints. It also features a diverter less supersonic inlet. It made its first flight in September 2018. Compared to the FTC-2000 trainer variant, the FTC-2000G is heavier, slower due to new wing design, and has less endurance than the FTC-2000. The JL-9G is a modified JL-9 for aircraft carrier training. It is designed for ski-jump ramp takeoffs and simulated arrested landings (land-based). and includes a tail hook.

Air & Air Defense Specifications
Crew 2
Engine Turbojet (43 hp)
Max Speed 1100.0 km/h
Cruise Speed 870.0 km/h
Range 863.0 km
Endurance 3.00 hrs
Service Ceiling 16000 m
System
Alternate Designation(s) GL-9; FTC-2000 Mountain Eagle
Primary Function / Type Two-seat supersonic fighter-trainer
Manufacturer Guizhou Aviation Industry Import/Export Company (GAIEC)
Crew 2
Number of Engines 1
Number of Hard Points 5 with a capacity of 2,000 kg (4,409 lb) maximum.
Additional Fuel Tanks up to 3 x fuel tanks
Dimensions
Length 14.6 m
Height 4.1 m
Width (Wing Span) 8.32 m
Wing Area 26.15 m2
Gross Weight 7,800 kg clean 7,900 kg normal
Maximum Takeoff Weight 9,800 kg
Automotive
Engine Name 1 × Guizhou Liyang WP-13F (C)
Number of Engines 1
Engine Type afterburning turbojet
Engine Power 43.15 kN (9,700 lbf) thrust dry, 63.25 kN (14,220 lbf) with afterburner
Maximum Speed 1,100 km/h
Minimum Flying Speed 210 km/h
Cruise Speed 870 km/h
Stall Speed 125 km/h
Maximum Range 863 km on internal fuel
Ferry Range 2,400 km with maximum internal and external fuel
Endurance 3 hours
Service Ceiling 16,000 m
G Limits +8 -3
Rate of Climb 150 m/s at sea level
Take-Off Run 400–500 m
Landing Run 700 m
Main Gun System
Name INA
Type 1x 23mm cannon
Ammunition
Type Rifle
Caliber 23 mm
Cartridge INA
Basic Load INA
Main Missile Systems
Note typically 2x PL-8 AAMs on inboard pylons + 2x PL-9 AAMs on outboard pylons
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 Yes
Details
Country of Origin China
Category Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
J
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
14.6 m
Width
8.32 m
Height
4.1 m
Weight
7800 kg
Operators (1)
China
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