AIDC T-CH-1

Airplanes

Length

10.26 m

Flat Wing Span

12.19 m

Height

3.66 m

Flat Wing Area

25.18 m²

Flat Wing Aspect Ratio

Cruise Speed

314.8397 km/h

Max Speed

592.6395 km/h

Max Ceiling

9753.6 m

Number of Engines

First Flight

1973-11-23

Number Built

Maximum Take-Off Weight

5.057 t (paragliders: kg)

Total Fuel Capacity

963

Maximum Range

2010 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
AIDC T-CH-1	5.057	963	2010

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Douglas SBD Dauntless		10.0584	12.4968	Compare
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All data (24 fields)

Name: AIDC T-CH-1
Manufacturer: Aerospace Industrial Development Corporation
Description: The AIDC T-CH-1 Chung Hsing () was a turboprop-powered military trainer aircraft produced in Taiwan (Republic of China).
First Flight: 1973-11-23
Designer: Aerospace Industrial Development Corporation
Type: Trainer
Length (m): 10.26
Height (m): 3.66
Cockpit Crew: 2
Max Speed (km/h): 592.6395
Cruise Speed (km/h): 314.8397
Min Speed (km/h): 92.5999
Max Ceiling (m): 9753.6
Rate of Climb (m/s): 17.272
National Origin: Taiwan
Number Built: 52
Powerplant Description: 1 × Avco Lycoming T53-L-701 turboprop, 1082 kW (1451 hp) each
Primary Users: Republic of China Air Force
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/AIDC_T-CH-1
Flat Wing Span (m): 12.19
Flat Wing Area (m²): 25.18
Flat Wing Aspect Ratio: 6
Number of Engines: 1