| Antonov 22 Specifications:
| Max Take Off Weight: |
225,000kg 496,040lb |
| Structural Payload: |
60,000kg 132,280lb |
| Fuel Capacity: |
43,000kg 94,795lb |
| Main Deck Useable Volume: |
638m 3 1,876ft 3 10in 3 |
| Cargo Area Width: |
4.4m 14ft 5in |
| Cargo Area Length: |
33m 108ft 2in |
| Cargo Area Height: |
4.4m 14ft 5in |
| Main Cargo Door Width: |
3m 10ft |
| Main Cargo Door Height: |
3.9m 12ft 9in |
| Wing Span: |
64m 211ft 3in |
| Overall Length: |
58m 189ft 8in |
| Overall Height: |
12.5m 41ft 1in |
Antonov 72 Specifications:
| Country of Origin |
Russia |
| Builder |
ANTONOV |
| Role |
Medium-transport, STOL |
| Similar Aircraft |
C-160 Transall, G.222 |
| Wing Span |
84 ft, 9 in (25.8 m) |
| Length |
87 ft, 2 in (26.6 m) |
| Height |
8.2 m |
| Weight |
26,500 kg takeoff weight
30,500 kg Max. takeoff weight |
| Engine |
2 Lotarev D-36, 62.8 kN thrust each |
| Maximum speed |
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| Cruising speed |
720 km/h |
| Landing speed |
165 km/h |
| Airfield |
Takeoff roll: 400-450 m
Landing roll: 350-400 m |
| Range |
3200 km maximum
1200 km with maximum payload |
| Ceiling |
11000 m maximum
8000 m cruise |
| Armament |
None |
| Payload |
32 passengers or 5000 kg of cargo |
| Crew |
Three |
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