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333 km/h (207 mph, 180 kn) at 3,050 m (10,000 ft) (econ. cruise)
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16:
Prototype transport aircraft by the
Aerospace Industrial Development Corporation
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A single prototype was built and was not selected for production.
108:
was a prototype civil transport aircraft designed in the 1970s in
498:
33:
Prototype AIDC XC-2 (68-5001) on display in
Taichung (Shueinan)
300:
1,661 km (1,032 mi, 897 nmi) with maximum fuel
234:
3,028 L (666 imp gal; 800 US gal)
273:
392 km/h (244 mph, 212 kn) at sea level
285:
145 km/h (90 mph, 78 kn) (flaps down)
533:
334:
Aircraft of comparable role, configuration, and era
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89:
81:
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61:
51:
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258:, 3.05 m (10 ft 0 in) diameter
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526:Aerospace Industrial Development Corporation
68:Aerospace Industrial Development Corporation
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503:
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18:
294:463 km/h (288 mph, 250 kn)
146:Jane's All The World's Aircraft 1980-81
449:Jane's All The World's Aircraft 1980–81
413:
160:3 (pilot, co-pilot and flight engineer)
477:. London: Studio Editions. p. 44.
432:
420:
139:Specifications (performance estimated)
7:
355:de Havilland Canada DHC-6 Twin Otter
254:3-bladed Hamilton Standard 53C51-17
248:, 1,082 kW (1,451 hp) each
194:65.40 m (704.0 sq ft)
176:20.10 m (65 ft 11 in)
182:24.90 m (81 ft 8 in)
170:3,855 kg (8,500 lb) cargo
188:7.72 m (25 ft 4 in)
14:
604:Abandoned civil aircraft projects
312:7.6 m/s (1,500 ft/min)
27:
614:Twin-turboprop tractor aircraft
475:Jane's Encyclopedia of Aviation
228:12,474 kg (27,500 lb)
473:Taylor, Michael J. H. (1989).
322:Landing run from 15 m (50 ft):
222:7,031 kg (15,501 lb)
1:
451:. London: Jane's Publishing.
306:8,015 m (26,296 ft)
132:, maximising internal space.
609:Aircraft first flown in 1979
316:Takeoff run to 15 m (50 ft):
128:on either side of the boxy
630:
324:826 m (2,710 ft)
318:778 m (2,552 ft)
56:Taiwan (Republic of China)
594:1970s Taiwanese airliners
256:variable-pitch propellers
26:
151:General characteristics
112:. It was a high-wing
535:Fixed-wing aircraft
489:luftfahrt-archiv.de
226:Max takeoff weight:
39:General information
599:High-wing aircraft
445:Taylor, John W. R.
435:, pp. 177–178
400:Let L-410 Turbolet
375:CASA C-212 Aviocar
290:Never exceed speed
120:engines. The main
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575:
340:Short SC.7 Skyvan
102:
101:
77:program cancelled
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385:PZL M28 Skytruck
304:Service ceiling:
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98:26 February 1979
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528:(AIDC) aircraft
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467:Further reading
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124:was carried in
116:powered by two
52:National origin
47:Civil transport
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483:External links
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447:, ed. (1980).
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166:38 passengers
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589:AIDC aircraft
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458:0-7106-0705-9
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277:Cruise speed:
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220:Empty weight:
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283:Stall speed:
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242:Lycoming T53
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199:Aspect ratio
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105:
103:
95:First flight
82:Number built
63:Manufacturer
433:Taylor 1980
421:Taylor 1980
395:Harbin Y-12
360:Dornier 228
264:Performance
252:Propellers:
238:Powerplant:
583:Categories
491:(archived)
408:References
246:turboprops
192:Wing area:
370:IAI Arava
365:GAF Nomad
350:Short 360
345:Short 330
180:Wingspan:
164:Capacity:
144:Data from
118:turboprop
114:monoplane
106:AIDC XC-2
329:See also
244:-L-701A
130:fuselage
126:sponsons
212:NACA 65
208:Airfoil
186:Height:
174:Length:
90:History
558:T-CH-1
548:F-CK-1
455:
298:Range:
110:Taiwan
74:Status
553:PL-1B
203:9.5:1
158:Crew:
563:XC-2
543:AT-3
453:ISBN
240:2 ×
216:-218
104:The
44:Type
22:XC-2
568:T-5
585::
168:or
518:e
511:t
504:v
461:.
292::
214:3
210::
201::
85:1
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
