|
|
|
| |
|
|---|
| Cockpit crew | Two |
Seating capacity,
typical |
|
| 184 (1-class)
160 (2-class) |
|
| Seat pitch | 30 in for 1-class, high-density; 32 in for 1-class, standard; 34 in for 2-class, business; 36 in for 2-class, first class |
| Seat width | 17.2 in (1-class, 6 abreast seating) |
| Overall length |
|
| 129 ft 6 in (39.5 m) |
|
| Wingspan | 117 ft 5 in (35.7 m) |
| Overall height |
| 41 ft 2 in (12.5 m) |
| Wing sweepback | 25.02° (437 mrad) |
| Wing aspect ratio | 9.45 |
| Fuselage width | 12 ft 4 in (3.76 m) |
| Fuselage Height | 13 ft 2 in (4.01 m) |
| Maximum cabin width | 11 ft 7 in (3.54 m) |
| Cabin height | 7 ft 3 in (2.20 m) |
| Operating empty weight |
|
| 91,108 lb (41,413 kg) |
|
| Maximum take-off weight |
|
| 174,200 lb (79,010 kg) |
|
| Maximum landing weight |
|
| 146,300 lb (66,361 kg) |
| Cargo capacity |
|
| 1,591 ft³ (45.1 m³) |
|
| Takeoff run at MTOW |
|
| 8,181 ft (2,450 m) |
| Service ceiling | 41,000 ft (12,500 m) |
| Cruising speed | Mach 0.785 (514 mph, 828 km/h) |
|
| Maximum speed | Mach 0.82 (544 mph, 876 km/h, 473 kt) |
| Range fully loaded |
|
| 3,060 NM (5,665 km) |
|
| Max. fuel capacity | 6,875 US gal (26,020 L) |
|
| Engine (x 2) |
|
| CFM 56-7B27 |
|
| Max. thrust (x 2) |
|
| 27,300 lbf (121.4 kN) |
| Cruising thrust (x 2) |
| 5,480 lbf (24.38 kN) |
| Fan tip diameter | 61 in (1.55 m) |
| Engine length | 98.7 in (2.51 m) |
| Engine ground clearance | 18 in (46 cm) |
SPECIFICATIONS General characteristics Crew: 2 pilots Capacity: 11 - 18 passengers Payload: 6,500 lb (2,950 kg) Length: 99 ft 9 i...