Boeing CC-137

Length
46.61 m
Flat Wing Span
44.42 m
Height
12.93 m
Flat Wing Area
280 m²
Max Seating
170
Cruise Speed
994 km/h
Max Ceiling
12000 m
Number of Engines
4
Aircraft Engine
First Flight
1970-01-01
Entry Into service
1972-01-01
Number Built
5
Maximum Take-Off Weight
148 t (paragliders: kg)
Maximum Range
9300 km

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Boeing CC-137 148 9300

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
Boeing C-137 Stratoliner 46.61 44.42 Compare
Northrop Grumman E-8 Joint STARS Pratt & Whitney JT3D 46.61 44.42 Compare
Boeing 707 Pratt & Whitney JT3D 46.3296 44.196 194 Compare
Boeing E-3 Sentry 46.3296 44.196 Compare
Vickers VC10 Rolls-Royce Conway 48.1584 44.5008 151 Compare
Boeing E-6 Mercury 45.72 45.1104 Compare
All data (24 fields)
Name
Boeing CC-137
Manufacturer
Boeing
Description
The Boeing CC-137 is a retired transport and tanker aircraft which served with the Canadian Forces from 1970 to 1997.
First Flight
1970-01-01
Entry Into service
1972-01-01
Service End
1997-01-01
Designer
Boeing
Type
Military transport aircraft
Length (m)
46.61
Height (m)
12.93
Cockpit Crew
3
Max Seating
170
Cruise Speed (km/h)
994
Max Ceiling (m)
12000
Capacity Description
170 passengers and 90,000 lb (41,000 kg) payload
Number Built
5
Powerplant Description
4 × Pratt & Whitney JT3D-7 turbofans, 87.6 kN thrust each
Primary Users
Canadian Forces
Status
Retired
Wikipedia Article (URL)
en.wikipedia.org/wiki/Boeing_CC-137
Flat Wing Span (m)
44.42
Flat Wing Area (m²)
280
Aircraft Engine
Pratt & Whitney JT3D
Number of Engines
4