DC-9 -30 (T-Tail Twin Jets)

TTJ_DC_9_30


Name: Douglas DC-9 -30
Type: Narrow-body jet airliner
Crew: 2
Max seating: 115
Length: 36.36 m (119 ft 3.6 in)
Wing span: 28.44 m (93 ft 3.6 in)
Height: 8.5 m (27 ft 9 in)
Wing area: 93 m² (1,000 sq ft)
Weight Empty: 25,789 kg (56,855 lb)
Max Takeoff Weight: 48,980 kg (107,982 lb)
Internal Fuel: 14,000 L (3,700 US gal)
Cruise speed: 792 km/h (428 kt)
Max Mach at altitude: 0.9
Range: 2,800 km (1,500 nmi)
Service ceiling: 11,000 m (36,091 ft)
Takeoff distance: 2,100 m (6,758 ft)
Landing distance: 1,500 m (4,827 ft)
Powerplant: 2 x Pratt & Whitney JT8D-9 Low-bypass turbofans, 54.5 kN (12,250 lbf) each


The Douglas DC-9 (McDonnell Douglas DC-9 in later) is a domestic range narrow-body airliner and cargo aircraft designed by Douglas Aircraft Company in the United States. It has two turbofan engines JT8D on its tail with T-Tail style.