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Douglas DC-9-30
The DC-9-30 stretched the DC-9 by about 15 feet to 119 ft 4 in, with a longer 93 ft 4 in wing, and first flew on August 1, 1966. It could carry up to 115 passengers. Boeing's planning manual gives its DC-9-32 version a maximum take-off weight of 108,000 pounds and 13,926 liters of usable fuel, and the DC-9-33F freighter has a cargo door and room for 4,195 cubic feet of freight. Two Pratt & Whitney JT8D turbofans sit on the rear fuselage below the T-tail. A few still fly in US airspace.
- Engines
- Two Pratt & Whitney JT8D turbofans at the tail
- Max takeoff weight
- 108,000 lb (48,988 kg)

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Specifications
| Length | 119 ft 3 in (36.36 m) |
|---|---|
| Wingspan | 93 ft 4 in (28.44 m) |
| Height | 27 ft 9 in (8.46 m) |
| Fuselage width | 11 ft 0 in (3.35 m) |
| Fuel capacity | 3,680 US gal (13,926 L) |
| First flight | August 1, 1966 |
| Status | Still flying with a few operators |
| Type codes | ICAO DC93 |
Who flies it now
31 flights by other operators
From flights seen in US airspace in the last 14 days (public flight data).
In the air now
No aircraft of this type in the air right now
Flights of this type in the air now, from public flight data.