Specifications
| MD-81 | MD-82 / MD-88 |
MD-83 | MD-87 | |||
|---|---|---|---|---|---|---|
| Cockpit crew | Two | |||||
| Seating capacity, typical |
172 (1-class) 155 (2 class) |
139 (1-class) 130 (2 class) |
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| Length | 147 ft 8 in (45.01 m) | 130 ft 4 in (39.73 m) | ||||
| Wingspan | 107 ft 8 in (32.82 m) | |||||
| Wing area | 1,209 sq ft (112.3 m2) | |||||
| Tail height | 29 ft 7 in (9.02 m) | 30 ft 4 in (9.25 m) | ||||
| Fuselage width | 11 ft (3.35 m) | |||||
| Cargo capacity | 1,253 cu ft (35.5 m3) | 1,103 cu ft (31.2 m3) | 937 cu ft (26.5 m3) | |||
| Empty weight | 77,900 lb (35,300 kg) | 78,000 lb (35,400 kg) | 79,700 lb (36,200 kg) | 73,300 lb (33,200 kg) | ||
| Maximum take-off weight (MTOW) |
140,000 lb (63,500 kg) | 149,500 lb (67,800 kg) | 160,000 lb (72,600 kg) | 140,000 lb (63,500 kg) | ||
| Cruising speed | Mach 0.76 (504 mph, 811 km/h) | |||||
| Maximum range, fully loaded |
1,570 nmi (2,910 km; 1,810 mi) | 2,050 nmi (3,800 km; 2,360 mi) | 2,500 nmi (4,600 km; 2,900 mi) | 2,370 nmi (4,390 km; 2,730 mi) | ||
| Runway length requirement |
5,000 ft (1,500 m) dry, or 5,700 ft (1,700 m) for wet runway |
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| Fuel capacity | 5,850 US gal (22,100 L) | 5,850 US gal (22,100 L) | 7,000 US gal (26,000 L) | 5,840 US gal (22,100 L) | ||
| Engines (×2) | Pratt & Whitney JT8D-200 series | |||||
| Thrust (×2) | 18,500–21,000 lbf (82–93 kN) | |||||
Sources: Official MD-80 specifications, MD-80 Airport report
Read more about this topic: McDonnell Douglas MD-80