Entry Into service
2001-04-21
Maximum Take-Off Weight
77.5643 t (paragliders: kg)
Total Fuel Capacity
26024.71
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Boeing C-40 |
77.5643 |
26024.71 |
5926.4 |
Similar airplanes
All data (25 fields)
- Name
- Boeing C-40
- Manufacturer
- Boeing
- Description
- The Boeing C-40 is a military transport aircraft derived from the Boeing 737 Next Generation.
- ICAO Code
- B737
- First Flight
- 2000-04-01
- Entry Into service
- 2001-04-21
- Production End
- 2019-01-01
- Designer
- Boeing
- Type
- Military transport aircraft
- Length (m)
- 33.528
- Height (m)
- 12.4968
- Cockpit Crew
- 100
- Max Seating
- 121
- Max Speed (km/h)
- 988.9671
- Max Ceiling (m)
- 12496.8
- Capacity Description
- ; C-40A passenger configuration: 121 passengers; C-40A cargo configuration: 8 pallets; C-40A combination configuration: 3 pallets, 70 passengers; C-40B: 26 to 32 passengers; C-40C: 42 to 111 passenge…
- National Origin
- United States of America
- Number Built
- 28
- Powerplant Description
- 2 × CFM International CFM56-7B turbofan engines
- Primary Users
- United States Navy, United States Air Force, United States Marine Corps
- Status
- In service
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Boeing_C-40
- Flat Wing Span (m)
- 34.1376
- Wake Category
- M
- Number of Engines
- 2