| External | | Length: | 99.4 ft |   |   | 30.3 m | | Wingspan: | 94 ft |   |   | 28.6 m | | Wing area (basic): | 1,022 ft | ²  |   | 94.9 m | | Height overall: | 24.8 ft |   |   | 7.6 m | |  | | Internal | | Cabin length: | 48.35 ft |   |   | 14.7 m | | (From cockpit divider to end of pressurized compartment) | | Cabin maximum width: (Centerline) | 8.17 ft |   |   | 2.49 m | | Cabin width: (Floorline) | 6.92 ft |   |   | 2.11 m | | Cabin height: | 6.25 ft |   |   | 1.91 m | | Floor area: (Excluding cockpit) | 353 ft | ² |   | 31.1 m | | Total volume: | 2,140 ft | ³ |   | 60.60 m | | (From cockpit divider to end of pressurized compartment) | |  | | Weights | | A. Maximum ramp weight: | 98,250 lb |   |   | 44,565 kg | | B. Maximum takeoff weight: | 98,000 lb |   |   | 44,452 kg | | C. Maximum landing weight: | 78,600 lb |   |   | 35,652 kg | | D. Maximum zero fuel weight: | 56,000 lb |   |   | 25,401 kg | | E. Basic operating weight: | 51,500 lb |   |   | 23,360 kg | | F. Maximum fuel weight: | 44,975 lb |   |   | 20,400 kg | | Manufacturer’s weight empty (±1%): | 49,750 lb |   |   | 22,566 kg | | Maximum payload (D-E): | 4,500 lb |   |   | 2,041 kg | | Payload – full fuel (A-E-F): | 1,775 lb |   |   | 805 kg | | Fuel with maximum payload: | 42,250 lb |   |   | 19,162 kg | | NBAA IFR fuel reserve (8 pax): | 3,100 lb |   |   | 1,406 kg | | Operations at a reduced MGTOW: | 75,000 lb |   |   | 34,019 kg | |  | | PERFORMANCE | | Range | | Maximum range at M 0.85: | 6,150 NM | | 11,389 km | | (NBAA IFR Reserves, ISA, with 8 pax/4 crew and maximum fuel) | |  | | Speed | Mach | kts | mph | km/h | | High-speed cruise | 0.89 | 513 | 590 | 950 | | Typical cruise speed | 0.85 | 488 | 562 | 904 | |  | | Ceiling | | Maximum operating altitude: | 51,000 ft |   |   | 15,545 m | | Climb to cruise altitude of 43,000 ft | 30 min |   |   |   | | (13,106 m): | |  | | Cabin noise level | | Average fleet: | 51.8 dbM(SIL)/69.4 dbA | |