Overview
The McDonnell Douglas C-9 Nightingale was developed as a dedicated aeromedical evacuation aircraft for the U.S. Air Force. Based on the DC-9 airliner, it entered service in the late 1960s. The aircraft provided rapid long-distance medical transport.
Live Fleet Activity (DC9)
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Specifications
Units
- Engine
- 2 × Pratt & Whitney JT8D-9
- Engine type
- Turbofan
- Thrust
- 2 × 14,500 lbf · 64 kN
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 84
- Crew
- —
- Cabin width
- 8 ft 9 in · 2.66 m
- Cabin height
- 6 ft 9 in · 2.05 m
- Cabin length
- —
- Exterior length
- 119 ft 3 in · 36.36 m
- Tail height
- 27 ft 11 in · 8.50 m
- Fuselage diameter
- 10 ft 10 in · 3.30 m
- Wing span
- 93 ft 4 in · 28.44 m
- Baggage volume
- 893 ft³ · 25.3 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 110,000 lb · 50,000 kg
- Max landing weight
- 99,000 lb · 44,900 kg
- Max payload
- 30,100 lb · 13,700 kg
- Fuel capacity
- 3,700 gal · 13,900 L · 11,100 kg (Jet A)
- Max cruise speed
- 500 kt · 575 mph · 926 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 127 kt · 146 mph · 235 km/h
- Range
- 1,739 nm · 2,000 mi · 3,220 km
- Fuel burn
- —
- Ceiling
- 37,000 ft · 11,300 m
- Rate of climb
- 3,000 ft/min · 15 m/s
- Takeoff distance
- 6,900 ft · 2,100 m
- Landing distance
- 4,900 ft · 1,500 m
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