| Manufacturer |
Mitsubishi Aircraft Corporation |
Aerospace Industrial Development Corporation |
| Description |
The Mitsubishi G7M was a proposed twin-engine long-range bomber designed for use by the Imperial Japanese Navy in 1941. |
The AIDC XC-2 was a prototype civil transport aircraft designed in the 1970s in Taiwan. |
| First Flight |
|
1979-02-26 |
| Designer |
Mitsubishi Aircraft Corporation |
Aerospace Industrial Development Corporation |
| Type |
|
Civil transport |
| Length (m) |
20 |
20.1 |
| Height (m) |
6.09 |
7.72 |
| Cockpit Crew |
7 |
3 |
| Max Seating |
|
38 |
| Max Speed (km/h) |
544 |
392 |
| Cruise Speed (km/h) |
|
333 |
| Min Speed (km/h) |
|
145 |
| Max Ceiling (m) |
5000 |
8015 |
| Rate of Climb (m/s) |
|
7.62 |
| Armament |
:: 6x 13 mm Type 2 machine guns ::2x 20 mm Type 99 Mark 2 machine gun (classified as machine guns by the IJN); up to 800 kg of bombs |
|
| Capacity Description |
|
38 passengers or 3855 kg cargo |
| National Origin |
|
Taiwan |
| Number Built |
|
1 |
| Powerplant Description |
2 × Mitsubishi MK10A 18-cylinder air-cooled radial piston engines, 1491 kW (2000 hp) each |
2 × Lycoming T53-L-701A turboprops, 1082 kW (1451 hp) each |
| Primary Users |
Imperial Japanese Navy Air Service (planned) |
|
| Status |
|
program cancelled |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Mitsubishi_G7M_Taizan |
en.wikipedia.org/wiki/AIDC_XC-2 |
| Flat Wing Span (m) |
25 |
24.9 |
| Flat Wing Area (m²) |
|
65.4 |
| Flat Wing Aspect Ratio |
|
9.5 |
| Aircraft Engine |
|
Lycoming T53 |
| Number of Engines |
2 |
2 |