AIDC AT-3

AIDC AT-3

KrajuTajwan
RoliSamoloty treningowe
Pierwszy lot16 września 1980
Zbudowany62

Tthe AIDC AT-3 Tzu Chung to zaawansowany samolot szkolno-treningowy eksploatowany przez Siły Powietrzne Republiki Chińskiej (ROCAF).

Źródła: AIDC AT-3 na Wikipedii

AIDC AT-3
FotografówUnknow
LokalizacjaNiewiedzy
Zdjęcia120
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General Characteristics

The AIDC AT-3 Tzu Chung (“Self Reliance”) is a tandem-seat, twin-engine jet aircraft developed by the Aerospace Industrial Development Corporation (AIDC) in Taiwan. Designed primarily as an advanced jet trainer for the Republic of China Air Force (ROCAF), it also possesses significant light attack and ground support capabilities, and served as the platform for the Thunder Tigers Aerobatics Team.

Property Typical Value (AT-3A/B Variant)
Roli Advanced Jet Trainer / Light Attack
Producent Aerospace Industrial Development Corporation (AIDC)
First Flight September 16, 1980
Załogi 2 (Pilot and Instructor, in tandem seating)
Długość 12.90 m (42 ft 4 in)
Rozpiętość 10.46 m (34 ft 4 in)
Max Takeoff Weight 7,940 kg (17,505 lb)
Units Built 62 (Total production)

Design and Powerplant

  • Engines: Two Honeywell/Garrett TFE731-2 non-afterburning turbofan engines.
  • Thrust Output: 15.6 kN (3,500 lbf) thrust each.
  • Cockpit: Features a tandem dual-control cockpit with two Martin-Baker Mk. 10L zero-zero ejection seats. The instructor’s (rear) seat is elevated by 30 cm for better forward visibility.
  • Construction: Predominantly light alloy, with some use of graphite-fiber composites (like the airbrake panels) to reduce weight.
  • Hardpoints: Equipped with five external hardpoints (one centerline and four underwing) plus wingtip launch rails for air-to-air missiles.
  • Attack Role: The AT-3B upgrade introduced a more capable APG-66T radar and a Head-Up Display (HUD) to enhance its ground attack capabilities.

Performance and Armament

  • Maximum Speed: 904 km/h (562 mph, 488 knots) at 11,000 m (36,000 ft).
  • Ferry Range: Approximately 2,280 km (1,420 mi, 1,230 nautical miles).
  • Service Ceiling: 14,650 m (48,060 ft).
  • Maximum External Load: 2,727 kg (6,000 lb) of ordnance.
  • Typical Armament Options:
    • Missiles: AIM-9 Sidewinder or locally produced TC-1 (Sky Sword I) air-to-air missiles.
    • Bombs: General-purpose iron bombs (e.g., Mk 82, Mk 84) and cluster bombs.
    • Guns: 20 mm gun pods or, in some early versions, semi-recessed twin 12.7 mm machine guns in a ventral gun bay.
  • Special Use: A single-seat attack variant, the XA-3, was developed for anti-ship missions, capable of carrying the HF-2 anti-ship missile.

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