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Douglas DC-9-10
The DC-9-10 is the original, shortest DC-9, about 104 ft 5 in long with an 89 ft 5 in wingspan and room for up to 90 passengers. Boeing's planning manual describes its DC-9-15 version as taking off at up to 90,700 pounds with 13,979 liters of usable fuel, and it was also built as the DC-9-15F with a large cargo door. Like every DC-9 it has two Pratt & Whitney JT8D turbofans on the rear fuselage under a T-tail, and its fuselage is 11 feet wide. A few of these early jets still fly in US airspace.
- Engines
- Two Pratt & Whitney JT8D turbofans at the tail
- Max takeoff weight
- 90,700 lb (41,141 kg)
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Specifications
| Length | 104 ft 5 in (31.82 m) |
|---|---|
| Wingspan | 89 ft 5 in (27.25 m) |
| Height | 27 ft 7 in (8.41 m) |
| Fuselage width | 11 ft 0 in (3.35 m) |
| Fuel capacity | 3,690 US gal (13,979 L) |
| First flight | February 25, 1965 |
| Entry into service | December 8, 1965 |
| Status | Still flying with a few operators |
| Type codes | ICAO DC91 |
Who flies it now
19 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.