The aircraft shall be a twin rear-engine, all metal. low wing monoplane with cantilever swept wings and empennage, monocoque fuselage of cross section, and fully retractable tricycle landing gear.
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| The aircraft shall be equipped with a pressurized cabin and an auxilliary power unit shall be installed.
The aircraft shall be a high performance short-to-medium haul commercial passenger and cargo transport which powered by two Rolls Royce RB 183 MK 555-15P/12 turbofan engine. | |
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| | Dimensions |
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| | Overall Length | : | 29.61 m (97 ft. 1.4 in) | | Wing Span | : | 25.07 m (82 ft 3.0 in) | | Height | : | 8.47 m (27 ft 9.5 in) | | Fuselage Length | : | 26.76 m (87 ft 9.5 in) | | Diameter | : | 3.30 m (10 ft 9.9 in) | | |
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| | Design Criteria |
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| | Cabin Length (ecxl. flight comp) | : | 15.31 m (50 ft 3.0 in) | | Max. Height | : | 2.02 m (6 ft 7.5 in) | | Max. Width | : | 3.10 m (10 ft 2.0 in) | | Floor Width | : | 2.88 m (9 ft 5.3 in) | | Max. Usable Floor Area | : | 44 m (474 ft) | | Height to Cabin Floor | : | 2.10 m (6 ft 10.6 in) | | Number of Seat | : | Y80 | | Max. Take-Off Weight | : | 32,207 kg (73,000 lbs) | | Max. Landing Weight | : | 29,848 kg (65,800 lbs) | | Max. Zero Fuel Weight | : | 26,083 kg (57,500 lbs) | | |
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| | Cargo Capacity |
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| | Forward Belly | : | 8.78 cu.m (308 cu ft) | | Rear Belly | : | 4.8 cu. m (171 cu. ft) | | Rear Cabin Luggage Compartment | : | 2.3 cu. m (80 cu. ft) | | |
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| | Powerplant | : | Rolls Royce RB 183 MK 555-15P/12 Turbofan Engine | |
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