Overview
The Lockheed C-141 Starlifter was developed as a jet-powered strategic transport for the U.S. Air Force. Entering service in the 1960s, it provided rapid intercontinental airlift capability. The aircraft replaced slower piston-powered transports.
Live Fleet Activity (C141)
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Specifications
Units
- Engine
- 4 × Pratt & Whitney TF33-P-7
- Engine type
- Turbofan
- Thrust
- 4 × 20,250 lbf · 90 kN
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 6
- Crew
- —
- Cabin width
- 10 ft 3 in · 3.12 m
- Cabin height
- 9 ft 1 in · 2.76 m
- Cabin length
- 93 ft 2 in · 28.40 m
- Exterior length
- 168 ft 4 in · 51.30 m
- Tail height
- 39 ft 7 in · 12.07 m
- Fuselage diameter
- 14 ft 9 in · 4.50 m
- Wing span
- 160 ft 1 in · 48.80 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 324,000 lb · 147,000 kg
- Max landing weight
- —
- Max payload
- 91,000 lb · 41,200 kg
- Fuel capacity
- 24,000 gal · 90,800 L · 72,700 kg (Jet A)
- Max cruise speed
- 493 kt · 567 mph · 913 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 120 kt · 138 mph · 222 km/h
- Range
- 2,550 nm · 2,930 mi · 4,720 km
- Fuel burn
- —
- Ceiling
- 41,000 ft · 12,500 m
- Rate of climb
- 2,600 ft/min · 13 m/s
- Takeoff distance
- 5,650 ft · 1,720 m
- Landing distance
- 4,000 ft · 1,220 m
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Live fleet activity details
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