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and two seats in tandem. By
September 1973, the first prototype had been completed and on 23 November 1973, it made its first flight. A second prototype, able to carry weaponry, was also produced, and completed its first flight on 27 November 1974. Alongside the two prototypes, a further 50 aircraft
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310 km/h (200 mph, 170 kn) at 15,000 ft (4,600 m) (econ cruise)
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590 km/h (370 mph, 320 kn) at 15,000 ft (4,600 m)
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545:. Aerospace Industrial Development Corporation (AIDC). 14 Aug 2014
595:. Internet Archive. London : Jane's Yearbooks. p. 177.
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2,010 km (1,250 mi, 1,090 nmi) (with maximum fuel)
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Development of the T-CH-1 began in
November 1970. Based on the
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963 L (212 imp gal; 254 US gal)
622:. Internet Archive. London : Jane's. p. 203.
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Aircraft of comparable role, configuration, and era
154:. Unsourced material may be challenged and removed.
278:, with the final aircraft delivered in late 1981.
616:Taylor, John W. R. (John William Ransom) (1984).
589:Taylor, John W. R. (John William Ransom) (1985).
539:"AIDC Privatization Anniversary Press Conference"
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265:training aircraft, the T-CH-1 had a low-wing
33:T-CH-1 at the RoC Air Force Museum in Ganshan
722:Aerospace Industrial Development Corporation
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68:Aerospace Industrial Development Corporation
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592:Jane's all the world's aircraft, 1980-1981
790:1970s Taiwanese military trainer aircraft
471:690 km/h (430 mph, 370 kn)
214:Learn how and when to remove this message
619:Jane's all the world's aircraft, 1984-85
653:Jane's All The World's Aircraft 1980-81
341:Jane's All The World's Aircraft 1980β81
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674:. London: Studio Editions. p. 44.
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462:93 km/h (58 mph, 50 kn)
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379:25.18 m (271.0 sq ft)
152:adding citations to reliable sources
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367:12.19 m (40 ft 0 in)
361:10.26 m (33 ft 8 in)
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565:"T-CH-1 Basic Trainer (1970~1981)"
373:3.66 m (12 ft 0 in)
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800:Single-engined tractor aircraft
672:Jane's Encyclopedia of Aviation
651:Taylor, John W.R., ed. (1980).
489:17 m/s (3,400 ft/min)
435:, 1,082 kW (1,451 hp)
139:needs additional citations for
670:Taylor, Michael J. H. (1989).
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415:5,057 kg (11,149 lb)
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686:AIDC T-CH-1 official web page
655:. London: Jane's Publishing.
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483:9,800 m (32,000 ft)
409:3,402 kg (7,500 lb)
403:2,608 kg (5,750 lb)
810:Aircraft first flown in 1973
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328:Republic of China Air Force
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86:Republic of China Air Force
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505:North American T-28 Trojan
321:Taiwan (Republic of China)
263:North American T-28 Trojan
251:Taiwan (Republic of China)
117:North American T-28 Trojan
56:Taiwan (Republic of China)
16:Taiwanese trainer aircraft
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346:General characteristics
517:Beechcraft T-34 Mentor
274:were ordered for the
271:tricycle landing gear
148:improve this article
731:Fixed-wing aircraft
499:Related development
413:Max takeoff weight:
39:General information
467:Never exceed speed
288:T-CH-1 Chung Hsing
245:-powered military
805:Low-wing aircraft
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602:978-0-7106-0821-5
429:Avco Lycoming T53
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163:"AIDC T-CH-1"
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159:Find sources:
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574:14 September
572:. Retrieved
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547:. Retrieved
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146:Please help
141:verification
138:
105:First flight
92:Number built
82:Primary user
63:Manufacturer
543:aidc.com.tw
441:Performance
425:Powerplant:
257:Development
230:Chung Hsing
779:Categories
525:References
377:Wing area:
204:April 2023
174:newspapers
433:turboprop
365:Wingspan:
339:Data from
307:Operators
267:monoplane
243:turboprop
494:See also
282:Variants
241:) was a
431:-L-701
393:Airfoil
371:Height:
359:Length:
235:Chinese
188:scholar
100:History
77:Retired
47:Trainer
754:T-CH-1
744:F-CK-1
659:
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475:Range:
318:
300:R-CH-1
294:A-CH-1
237::
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74:Status
22:T-CH-1
749:PL-1B
549:5 Sep
353:Crew:
195:JSTOR
181:books
759:XC-2
739:AT-3
657:ISBN
624:ISBN
597:ISBN
576:2023
569:AIDC
551:2024
427:1 Γ
226:The
167:news
44:Type
764:T-5
388:6:1
150:by
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239:δΈθ
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192:Β·
185:Β·
178:Β·
171:Β·
144:.
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