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At a glance
Measured figures
Length
Single source14.5 m (47.6 ft)[source]
FTC-2000 · excluding nose-probe
Single sourceConfiguration
| Specification | AIDC T-5 Brave Eagle | Guizhou JL-9 |
|---|---|---|
| Type | Advanced jet trainer[source] | Advanced jet trainer Light combat aircraft[source] |
| National origin | Taiwan[source] | — |
| Manufacturer | Aerospace Industrial Development Corporation[source] | Guizhou Aviation Industry Import/Export Company (GAIEC)[source] |
| Designer | Aerospace Industrial Development Corporation and National Chung-Shan Institute of Science and Technology[source] | Aero Engine Research Institute of Guizhou Aviation Industry Corporation |
14.555 m (47 ft 9 in) excluding nose-probe[source]
2 × Honeywell/ITEC F124 -200TW turbofan thrust each
Single source2 × Honeywell/ITEC F124 -200TW turbofan , 27.8 kN (6,250 lbf) thrust each[source]
FTC-2000 · 1 × Guizhou Liyang WP-13F (C) afterburning turbojet thrust dry
Single sourceFTC-2000 · thrust dry and
Single sourceFTC-2000 · with afterburner
Single sourceFTC-2000 · with afterburner (1 × WP-14C Kunlun-3 for FTC-2000G
Single source1 × Guizhou Liyang WP-13F (C) afterburning turbojet, 43.15 kN (9,700 lbf) thrust dry, 63.25 kN (14,220 lbf) with afterburner (1 × WP-14C Kunlun-3 for FTC-2000G, 53.89 kN (12,110 lbf) thrust dry and 76.53 kN (17,200 lbf) with afterburner.)[source]
FTC-2000 · Wing area
Single source26.15 m 2 (281.5 sq ft)[source]
FTC-2000 · Endurance
Single source3 hours[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | In service[source] | In service[source] |
|---|
| Primary user | Republic of China Air Force[source] | — |
|---|
| Number built | 4 prototypes and 56 serials (May 2026)[source] | — |
|---|
| Manufactured | 2020–2026[source] | — |
|---|
| Introduction date | 2021[source] | — |
|---|
| First flight | June 10, 2020[source] | 13 December 2003[source] |
|---|
| Developed from | AIDC F-CK-1 Ching-kuo[source] | Chengdu JJ-7[source] |
|---|
| Hardpoints | 2 (fitted for but not with ) , with provisions to carry combinations of:[source] | 5 with a capacity of 2,000 kg (4,409 lb) maximum, with provisions to carry combinations of: Other: up to 3 x fuel tanks[source] |
|---|
| Missiles | Sky Sword I , AIM-9 and AGM-65 (fitted for but not with )[source] | ** Short range air-to-air missile 2 × PL-8 AAMs (on inboard pylons) 2 × PL-9 AAMs (on outboard pylons) Beyond-visual-range air-to-air missiles SD-10 (Only on FTC-2000G) Anti-radiation missiles CM-102 (Only on FTC-2000G)[source] |
|---|
| Role | Taiwanese transonic advanced jet trainer aircraft[source] | — |
|---|
| Source measurement | The Advanced Jet Trainer Program (AJT) began in the early 2000s as the Republic of China Air Force sought a replacement for its fleet of AIDC AT-3 and Northrop F-5 advanced trainers with 66 newly built aircraft. Three designs were proposed, a modernized, upgraded version of AT-3 branded as the AT-3 MAX, an evolution of the AIDC F-CK-1 Ching-Kuo combat aircraft to be called the XAT-5, or the Italian Alenia Aermacchi M-346 Master . In 2014 AIDC signed a memorandum of understanding with Alenia Aermacchi to assemble the M-346 in Taiwan. The engines of all M-346 are assembled in Taiwan by International Turbine Engine Company (ITEC), a joint partnership of Honeywell and AIDC. The MOD also evaluated the South Korean KAI T-50 Golden Eagle aircraft.[source]AIDC T-5 Brave Eagle · Development / Advanced Jet Trainer Program; only the objects and conditions stated in this passage The design is based on the AIDC F-CK-1 Ching-kuo and shares the same engines, but has 80% new components including a composite body. Compared to the F-CK-1, it will have more advanced avionics, increased fuel capacity, and will be a little larger. The aerofoil is slightly revised, with the wings being thicker than on the F-CK-1 in order to increase stability at low speed and low altitude, as well as to provide increased fuel storage. The ram air scoop of the F-CK-1 has been redesigned in partnership with the Eaton Corporation with two aluminium laser powder bed fusion printed parts replacing 22 original parts. Meggitt will supply the main wheels, carbon brakes and brake control systems as they do on the AT-3 and F-CK-1. Martin-Baker will provide the ejection seat systems. More than 55% of its components are made in Taiwan. It has been reported that the aircraft was designed from the beginning to serve dual peacetime training and wartime combat roles.[source]AIDC T-5 Brave Eagle · Design; only the objects and conditions stated in this passage Length: 14.5 m (47.6 ft)[source]AIDC T-5 Brave Eagle · Specifications; only the objects and conditions stated in this passage Wingspan: 9.2 m (30.3 ft)[source]AIDC T-5 Brave Eagle · Specifications; only the objects and conditions stated in this passage Height: 4.39 m (14 ft 5 in)[source]AIDC T-5 Brave Eagle · Specifications; only the objects and conditions stated in this passage Empty weight: 4,500 kg (9,921 lb)[source]AIDC T-5 Brave Eagle · Specifications; only the objects and conditions stated in this passage Max takeoff weight: 7,500 kg (16,535 lb)[source]AIDC T-5 Brave Eagle · Specifications; only the objects and conditions stated in this passage Powerplant: 2 × Honeywell/ITEC F124 -200TW turbofan , 27.8 kN (6,250 lbf) thrust each[source]AIDC T-5 Brave Eagle · Specifications; only the objects and conditions stated in this passage Maximum speed: 1,030 km/h (640 mph, 556 kn)[source]AIDC T-5 Brave Eagle · Specifications; only the objects and conditions stated in this passage Cruise speed: 1,013 km/h (629 mph, 547 kn)[source]AIDC T-5 Brave Eagle · Specifications; only the objects and conditions stated in this passage Range: 1,350 km (839 mi, 729 nmi)[source]AIDC T-5 Brave Eagle · Specifications; only the objects and conditions stated in this passage Ferry range: 1,350 km (839 mi, 729 nmi)[source]AIDC T-5 Brave Eagle · Specifications; only the objects and conditions stated in this passage Service ceiling: 13,000 m (42,651 ft)[source]AIDC T-5 Brave Eagle · Specifications; only the objects and conditions stated in this passage Rate of climb: 48 m/s (9,500 ft/min)[source]AIDC T-5 Brave Eagle · Specifications; only the objects and conditions stated in this passage ROCAF T-5 in 2020[source]AIDC T-5 Brave Eagle · Gallery; only the objects and conditions stated in this passage | — |
|---|
| Primary users | — | People's Liberation Army Air Force People's Liberation Army Navy Air Force Myanmar Air Force Sudanese Air Force[source] |
|---|
| Fuel capacity | — | 2,000 kg (4,409 lb) internal + up to 1,302 kg (2,870 lb) in external tanks[source] |
|---|
| Guns | — | 1 × 23 mm cannon[source] |
|---|
| Unstick and touchdown speed | — | 260 km/h (160 mph; 140 kn)[source] |
|---|
| Minimum flying speed | — | 210 km/h (130 mph; 110 kn)[source] |
|---|
| Stall speed | — | 125 km/h (78 mph, 67 kn)[source] |
|---|
| g limits | — | + 8 - 3[source] |
|---|
| Wing loading | — | 374.8 kg/m 2 (76.8 lb/sq ft)[source] |
|---|
| Thrust/weight | — | 0.00645 kN/kg (0.658 lb f /lb)[source] |
|---|
| Take-off run | — | 400–500 m (1,300–1,600 ft)[source] |
|---|
| Landing run | — | 700 m (2,300 ft)[source] |
|---|
| Other | — | up to 3 x fuel tanks[source] |
|---|
| Beyond-visual-range air-to-air missiles | — | SD-10 (Only on FTC-2000G)[source] |
|---|
| Anti-radiation missiles | — | CM-102 (Only on FTC-2000G)[source] |
|---|
| Country of origin | — | Volksrepublik China[source]Country of design · Entwurfsland |
|---|
| Reported operators | — |
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