| Design Goals | Final |
Range with IFR (1) reserves |
1,160 nm | 1,178 nm | 18 miles more |
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MMO |
0.70 | 0.70 | on the mark |
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Maximum Ceiling |
41,000 ft | 41,000 ft | with direct climb at MTOW |
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High Speed Cruise |
380 kt | 390 kt | 10 ktas faster |
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Landing Distance (2) |
3,000 ft | 2,699 ft | 301 ft shorter |
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Standard Take-off Field Length (3) |
3,400 ft | 3,400 ft | on the mark |
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Enhanced Take-off Field Length (3) |
n/a | 3,125 ft | 275 ft shorter |
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Engine Thrust |
1,615 lb | 1,695 lb | 5% more thrust |
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Block Fuel for 1,000 nm |
1,960 lb | 1,892 lb | up to 3.6% fuel savings |
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External noise |
Stage IV | Stage IV | with 33 EPNdB margin |
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Main baggage compartment |
45 ft 3 | 53 ft 3 | 22% more space |