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| Design Criteria |
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| Max. Ram Weight | : | 49,442 kg (108,999 lbs) | Max. Take-Off Weight | : | 48,989 kg (108,000 lbs) | Max. Landing Weight | : | 44.498 kg (98,000 lbs) | Max. Zero Fuel Weight | : | 39,463 kg (87,000 lbs) | Average Basic Weight | : | 28,000 kg (61,729 lbs) | Max. Payload Weight | : | 10,000 kg (22.046 lbs) | Number of Seat | : | C 20 - Y 76 | |
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| Powerplant | : | Pratt and Whitney JT8D-15 Turbofan | |
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