Overview
The Boeing C-40A Clipper is a multi-talented aircraft designed and manufactured by Boeing and certified by Federal Aviation Administration as 737-700 convertible/combination aircraft configured for the transport of cargo and passengers all over the world. It provides critical logistic support in order to meet mission-sensitive needs.
Specifications
Units
- Engine
- 2 × CFM International CFM56-7B
- Engine type
- Turbofan
- Thrust
- 2 × 27,300 lbf · 121 kN
- Avionics
- Honeywell
- Wing tips
- Blended tips
- Seats
- 121
- Crew
- —
- Cabin width
- —
- Cabin height
- 7 ft 0 in · 2.13 m
- Cabin length
- 79 ft 4 in · 24.18 m
- Exterior length
- 110 ft 4 in · 33.63 m
- Tail height
- —
- Fuselage diameter
- —
- Wing span
- 112 ft 7 in · 34.32 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 171,000 lb · 77,500 kg
- Max landing weight
- 134,000 lb · 61,000 kg
- Max payload
- 40,000 lb · 18,100 kg
- Fuel capacity
- 6,900 gal · 26,000 L · 20,800 kg (Jet A)
- Max cruise speed
- 542 kt · 624 mph · 1,004 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 137 kt · 158 mph · 254 km/h
- Range
- 3,000 nm · 3,450 mi · 5,560 km
- Fuel burn
- —
- Ceiling
- 41,000 ft · 12,500 m
- Rate of climb
- 3,000 ft/min · 15 m/s
- Takeoff distance
- 5,500 ft · 1,680 m
- Landing distance
- 4,700 ft · 1,430 m
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