McDonnell Douglas DC-9-82 (MD-82)

 * Cockpit crew Two
 * Seating capacity, typical 172 (1-class) 155 (2 class)
 * Length 147ft 10in (45.06m)
 * Wingspan 107ft 10in (32.87m)
 * Wing area 1,209 sq ft (112.3 m2)
 * Tail height 29ft 7in (9.02m)
 * Fuselage width 11ft (3.35m)
 * Cargo capacity 1,253cu ft (35.5m3)
 * Empty weight 78,000lb (35,400kg)
 * Maximum take-off weight (MTOW) 149,500lb (67,800kg)
 * Cruising speed Mach 0.76 (504mph, 811km/h)
 * Maximum range, fully loaded 2,050nm (3,800km; 2,360mi)
 * Runway length requirement 5,000ft (1,500m) dry, or 5,700ft (1,700m) when wet runway
 * Maximum fuel capacity 5,845 US gal (22,130 L)
 * Engines (2) Pratt & Whitney JT8D-200 series
 * Thrust (2) 18,500-21,000 lbf (82-93 kN)