Boeing 737NG: Difference between revisions
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New page: {{Infobox Aircraft Type |type= Narrowbody Jetliner |country= USA |manufacturer= Boeing |status= In Production |number built= 1825 |unit cost= 36.000.000v... |
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|Engine ground clearance || colspan=3 | 18 in (46 cm) || colspan=2 | 19 in (48 cm) | |Engine ground clearance || colspan=3 | 18 in (46 cm) || colspan=2 | 19 in (48 cm) | ||
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[[Category:Narrowbody Jetliners]] | |||
Revision as of 15:47, 3 May 2009
| Boeing 737NG at a Glance | |
|---|---|
| Role | Narrowbody Jetliner |
| Country of Origin | USA |
| Manufacturer | Boeing |
| Status | In Production |
| Number Built | 1825 |
| Unit Cost | 36.000.000v$-70.000.000v$ |
| File:Airplanes-Boeing 737NG.jpg | |
The Boeing 737NG (Next Generation) series is a group of narrowbody jetliners produced by Boeing.
Boeing 737-600
Boeing 737-700
Boeing 737-800
Boeing 737-900
Specifications
| Measurement | 737-600 | 737-700/ 737-700ER |
737-800 | 737-900ER | |
|---|---|---|---|---|---|
| Cockpit crew | Two | ||||
| Seating capacity | 132 (1-class, dense), 123 (1-class, standard)) |
149 (1-class, dense), 140 (1-class, standard) |
189 (1-class, dense), 175 (1-class, standard) |
215 (1-class, high-density), 204 (1-class, dense), 177 (1-class, standard) | |
| Seat pitch | 30 in (1-class, dense), 32 in (1-class, standard) | 28 in (1-class, high-density), 30 in (1-class, dense), 32 in(1-class, standard) | |||
| Seat width | 17.2 in (1-class, 6 abreast seating) | ||||
| Length | 102 ft 6 in (31.2 m) |
110 ft 4 in (33.6 m) |
129 ft 6 in (39.5 m) |
138 ft 2 in (42.1 m) | |
| Wingspan | 117 ft 5 in (35.7 m) | ||||
| Height | 41 ft 3 in (12.6 m) |
41 ft 2 in (12.5 m) | |||
| Wing sweepback | 25.02° (437 mrad) | ||||
| Aspect ratio | 9.45 | ||||
| Fuselage width | 12 ft 4 in (3.76 m) | ||||
| Fuselage Height | 13 ft 2 in (4.01 m) | ||||
| Cabin width | 11 ft 7 in (3.54 m) | ||||
| Cabin height | 7 ft 3 in (2.20 m) | ||||
| Empty weight | 80,031 lb (36,378 kg) |
84,100 lb (38,147 kg) |
91,108 lb (41,413 kg) |
98,495 lb (44,676 kg) | |
| Maximum take-off weight | 145,500 lb (66,000 kg) |
Basic: 154,500 lb (70,080 kg) ER: 171,000 lb (77,565 kg) |
174,200 lb (79,010 kg) |
187,700 lb (85,130 kg) | |
| Maximum landing weight | 121,500 lb (55,112 kg) |
128,928 lb (58,604 kg) |
146,300 lb (66,361 kg) | ||
| Cargo capacity | 756 ft³ (21.4 m³) |
966 ft³ (27.3 m³) |
1,591 ft³ (45.1 m³) |
1,852 ft³ (52.5 m³) | |
| Takeoff run at MTOW | 8,016 ft (2,400 m) | 8,283 ft (2,480 m) | 8,181 ft (2,450 m) | ||
| Service ceiling | 41,000 ft (12,500 m) | ||||
| Cruising speed | 0.785 (514 mph, 828 km/h) | 0.78 (511 mph, 823 km/h) | |||
| Maximum speed | 0.82 (544 mph, 876 km/h, 473 kt) | ||||
| Range fully loaded | 3,050 NM (5,648 km) | Basic: 3,365 NM (6,230 km) WL: 3,900 NM (7,220 km) ER: 5,375 NM (9,955 km) |
3,060 NM (5,665 km) | 2,700 NM (4,996 km) in 1 class layout, 3,200 NM (5,925 km) in 2 class layout with 2 aux. tanks | |
| Max. fuel capacity | 6,875 US gal (26,020 L) |
7,837 US gal (29,660 L) | |||
| Engine (x 2) | CFM 56-7B20 | CFM 56-7B26 | CFM 56-7B27 | CFM 56-7 | |
| Max. thrust (x 2) | 20,600 lbf (91.6 kN) | 26,300 lbf (116.0 kN) | 27,300 lbf (121.4 kN) | ||
| Cruising thrust (x 2) | 5,210 lbf (23.18 kN) | 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) | 19 in (48 cm) | |||