SPECIFICATIONS
| Passengers | :153 (2 class), 172 (1 class) | |
|---|---|---|
| Max Take-off Weight | :156,000 lb (70,760 kg) | |
| Take off run at MTOW | :7450 ft (2.270 m) | |
| Range | :2,085 nmi (3,860 km) | |
| Cruise Speed, typical | :Mach 0.76 (504 mph, 811 km/h) | |
| Length | :152 ft 7 in (46.5 m) | |
| Wing span | :107 ft 10 in (32.87 m) | |
| Height | :30 ft 6 in (9.4 m) | |
| Power plant (2 x) | :IAE V2525-D5 25,000 lbf (111.21 kN) Optional: IAE V2528-D5 28,000 lbf (124.55 kN) | |
General Specs
- Crew: 1
- Capacity: 3-9 passengers
- Payload: 615 lb (279 kg)
- Length: 42 ft 7 in (12.98 m)
- Wingspan: 46 ft 11 in (14.30 m)
- Height: (4.19 m)
- Empty weight: 6,765 lb (3,069 kg)
- Useful load: 3,835 lb (1,740 kg)
- Max takeoff weight: 10,700 lb (4,853 kg)
- Powerplant: 2 × Williams FJ44-1AP turbofan, 1,965 lb (8.74 kN) each
- Cruise speed: 389 ktas (720 km/h)
- Stall speed: 83 kcas (153 km/h)
- Range: 1,300 nm (2,408 km)
- Service ceiling: 41,000 ft (12,497 m)
- Rate of climb: 3,290 ft/min (1,003 m/min)
Source:wikipedia
Specs
| Cockpit crew | :Two | |||
|---|---|---|---|---|
| Seating capacity | :180 (1-class, maximum) 164 (1-class, typical) 150 (2-class, typical) | |||
| Cargo capacity | :37.41 m3 (1,321 cu ft) 7× LD3-46 | |||
| Length | :37.57 m (123 ft 3 in) | |||
| Wingspan | :34.10 m (111 ft 11 in) | |||
| Wing area | :122.6 m2 (1,320 sq ft) | |||
| Wing sweepback | :25 degrees | |||
| Tail height | :11.76 m (38 ft 7 in) | |||
| Cabin width | :3.70 m (12 ft 2 in) | |||
| Fuselage width | :3.95 m (13 ft 0 in) | |||
| Operating empty weight | :42,600 kg (94,000 lb) | |||
| Maximum zero-fuel weight (MZFW) | :62,500 kg (138,000 lb) | |||
| Maximum take-off weight (MTOW) | :78 t (170,000 lb) | |||
| Cruising speed | :Mach 0.78 (828 km/h/511 mph at 11,000 m/36,000 ft) | |||
| Maximum speed | :Mach 0.82 (871 km/h/537 mph at 11,000 m/36,000 ft) | |||
| Maximum range, fully loaded | :3,200 nmi (5,900 km; 3,700 mi) | |||
| Take off run at MTOW (sea level, ISA) | :2,090 m (6,860 ft) | |||
| Maximum fuel capacity | :24,210 L (5,330 imp gal; 6,400 US gal) standard 30,190 L (6,640 imp gal; 7,980 US gal) optional | |||
| Service ceiling | :12,000 m (39,000 ft) | |||
| Engines (×2) | :IAE V2500 series or CFM International CFM56-5 series | |||
| Thrust (×2) | :111–120 kN (25,000–27,000 lbf) | |||
SPECS
| Cockpit crew | : Two | |||||
|---|---|---|---|---|---|---|
| Seating capacity, typical | : 301 (3-class) 400 (2-class) 440 (maximum) | |||||
| Length | : 209 ft 1 in (63.7 m) | |||||
| Wingspan | : 199 ft 11 in (60.9 m) | |||||
| Wing sweepback | : 31.64° | |||||
| Tail height | : 60 ft 9 in (18.5 m) | |||||
| Cabin width | : 19 ft 3 in (5.87 m) | |||||
| Fuselage width | : 20 ft 4 in (6.20 m) | |||||
| Maximum cargo capacity | : 5,720 cu ft (162 m3) 32× LD3 | |||||
| Empty weight, operating | : 297,300 lb (134,800 kg) | |||||
| Maximum landing weight | : 445,000 lb (201,840 kg) | |||||
| Maximum Takeoff Weight (MTOW) | : 545,000 lb (247,200 kg) | |||||
| Typical cruise speed | : 0.84 Mach (560 mph, 905 km/h, 490 knots) at a cruise altitude of 35,000 ft (11,000 m) | |||||
| Maximum cruise speed | : 0.89 Mach (590 mph, 950 km/h, 512 knots) at a cruise altitude of 35,000 ft (11,000 m) | |||||
| Maximum range | : 5,240 nmi (9,700 km) | |||||
| Takeoff distance at MTOW ISA+15 MSL | : 8,200 ft (2,500 m) | |||||
| Maximum fuel capacity | : 31,000 US gal (117,348 L) | |||||
| Service ceiling | : 43,100 ft (13,140 m) | |||||
| Engine (×2) | : PW 4077 RR 877 GE90-77B | |||||
| Thrust (×2) | : PW: 77,000 lbf (342 kN) RR: 76,000 lbf (338 kN) GE: 77,000 lbf (342 kN) | |||||