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Ching-Kuo

Ching-Kuo

Multi-Role Fighters
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Basic Information
Name
Ching-Kuo
Designation
Ching-Kuo
Alternate Designation
F-CK-1A (single seat aircraft), F-CK-1B (two-seat aircraft), IDF (Indigenous Defensive Fighter), Shiang-Seng (IDF C/D version)
Equipment Type
Multi-Role Fighters
Manufacturer
AIDC
Date of Introduction
1994
Description

The Ching-Kuo is a light multi-role, single/twin-seat fighter developed by AIDC to meet the requirements of the Taiwanese government for an Indigenous Defensive Fighter (IDF). The IDF program was born in 1982 to provide a credible fighter aircraft to the Taiwanese Air Force after the US arms embargo. The IDF prototype first flew on May 28, 1989. The first production aircraft was delivered to the Republic of China Air Force in January 1994. Production ceased in 1999 with approximately 200+ aircraft build by AIDC. The IDF C/D (single/twin-seat), also known as the Shiang-Seng, is an improved version with enhanced performance and improved equipment being developed by AIDC. The IDF C/D will be delivered to Taiwan's Air Force as both new-build and upgraded aircraft. Externally, the IDF has some traits from the F-16, F/A-18 and Rafale aircraft. General Dynamics worked closely with AIDC in the IDF aircraft development. The twin-engine aircraft is powered by TFE1040, also known as F125, engines each rated at 9,400-lb with afterburning. The Golden Dragon 53 radar is based on the AN/APG-67 and APG-66 and provides air-to-air and air-to-surface modes. The weapons package includes a 20mm M61A1 cannon, dumb bombs, cluster munitions, GBU-12 laser guided bombs, Mavericks, Hsiung Feng II anti-ship missiles, Sky Sword I and Sky Sword II air-to-air missiles. Overall, the IDF fighter has been designed to perform air defense, anti-ship and ground attack missions.

Air & Air Defense Specifications
Crew 1
Max Speed 1295.0 km/h
Service Ceiling 16459 m
Wingspan 8.50 m
Overview (Deagel)
Group Multi-Role Fighters
Status Active
Also Known As F-CK-1A (single seat aircraft), F-CK-1B (two-seat aircraft), IDF (Indigenous Defensive Fighter), Shiang-Seng (IDF C/D version)
Origin Taiwan
Contractor AIDC
Initial Operational Capability (IOC) January 1994
First Flight May 28, 1989
Total Production 131
Specifications (Deagel)
Crew 1
Number of Engines 2
Area — Wing Area 24.3 square meter
Dimensions — Height 4.7 meter
Dimensions — Length 14.2 meter
Dimensions — Main Gun Caliber 20 millimeter
Dimensions — Wingspan 8.5 meter
Mass — Empty Weight 6,485 kilogram
Mass — Max Takeoff Thrust 18,800 pound
Mass — Max Takeoff Weight 12,245 kilogram
Performance — Ceiling 54,000 foot
Speed — Climb Rate 50,000 fpm
Speed — Top Speed at High Altitude 1,295 kph
Gear (Deagel)
Item 1 Air-to-Air Missiles: Sky Sword I (2)
Item 2 Air-to-Air Missiles: Sky Sword II (2)
Item 3 Anti-Ship Missiles: Hsiung Feng II
Item 4 Bombs: GBU-12 Paveway II
Item 5 Fighter Aircraft Engines: F125 (2)
Item 6 Medium Caliber Cannons: M61A1 (1)
Item 7 Standoff Weapons: AGM-65B Maverick
Details
Country of Origin Taiwan
Category Multirole Aircraft
Air > Multirole Aircraft
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
14.2 m
Width
8.5 m
Height
4.7 m
Weight
12245 kg
Operators (1)
Taiwan
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