McDonnell Douglas DC-9
The McDonnell Douglas DC-9 first flew and entered airline service in 1965. It is a twin-engine, single-aisle jet airliner and was designed for frequent, short flights. The final DC-9 was delivered in October 1982. Delta Air Lines was the first to fly with the DC-9 on December 8, 1965. The DC-9 was a commercial success with 976 built when production ended in 1982.
Cargo Capacity | |
---|---|
Average Useful Capacity | 3,500 cu ft |
Average Payload | 32,000 lbs |
Minimum Runway Length | 5,900 ft |
Cargo Door Dimensions | |
Main | 135"W X 80"H |
Crew | 2 |
Propulsion | 2 Turbofan Engines |
Engine Model | Pratt & Whitney JT8D-17A |
Engine Power (each) | 16000 lbf |
Speed | 255 kts |
Service Ceiling | 35,000 ft |
Range | 1,421 nm |
Empty Weight | 64,675 lbs |
Max. Takeoff Weight | 114,000 lbs |
Max. Landing Weight | 110,000 lbs |
Wing Span | 93.3 ft |
Wing Area | 1001 ft² |
Length | 133.6 ft |
Height | 28.0 ft |
First Flight | 25.02.1965 |
Production Status | Out of production |
Total Production | 976 |
The McDonnell Douglas DC-9 first flew and entered airline service in 1965. It is a twin-engine, single-aisle jet airliner and was designed for frequent, short flights. The final DC-9 was delivered in October 1982. Delta Air Lines was the first to fly with the DC-9 on December 8, 1965. The DC-9 was a commercial success with 976 built when production ended in 1982.
Cargo Capacity | |
---|---|
Average Useful Capacity | 3,500 cu ft |
Average Payload | 32,000 lbs |
Minimum Runway Length | 5,900 ft |
Cargo Door Dimensions | |
Main | 135"W X 80"H |
Crew | 2 |
Propulsion | 2 Turbofan Engines |
Engine Model | Pratt & Whitney JT8D-17A |
Engine Power (each) | 16000 lbf |
Speed | 255 kts |
Service Ceiling | 35,000 ft |
Range | 1,421 nm |
Empty Weight | 64,675 lbs |
Max. Takeoff Weight | 114,000 lbs |
Max. Landing Weight | 110,000 lbs |
Wing Span | 93.3 ft |
Wing Area | 1001 ft² |
Length | 133.6 ft |
Height | 28.0 ft |
First Flight | 25.02.1965 |
Production Status | Out of production |
Total Production | 976 |