Boeing VC-25

· Boeing
Airplanes
Length
70.4088 m
Flat Wing Span
59.7408 m
Height
19.2024 m
Max Seating
76
Cruise Speed
925.9992 km/h
Max Speed
1013.969 km/h
Max Mach
0.92 Mach
Max Ceiling
13746.48 m
Number of Engines
4
First Flight
1987-05-16
Entry Into service
1990-08-23
Number Built
2
Maximum Take-Off Weight
377.8424 t (paragliders: kg)
Maximum Range
12593.6 km

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Boeing VC-25 377.8424 12593.6

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
Boeing E-4 General Electric CF6 70.4088 59.436 Compare
747-100 Pratt & Whitney JT9D 68.6 59.6 366 Compare
Boeing Dreamlifter Pratt & Whitney PW4000 71.628 64.3128 Compare
Boeing YAL-1 70.6 64.4 Compare
747-400 Pratt & Whitney PW4000 70.66 64.44 416 Compare
Lockheed C-5 Galaxy 75.2856 67.6656 Compare
All data (26 fields)
Name
Boeing VC-25
Manufacturer
Boeing
Description
The Boeing VC-25 is a military version of the Boeing 747 airliner, modified for presidential transport and commonly operated by the United States Air Force (USAF) as Air Force One, the call sign of any US Air Force aircraft carrying the president of the United States.
ICAO Code
B742
First Flight
1987-05-16
Entry Into service
1990-08-23
Designer
Boeing
Type
Presidential transport
Length (m)
70.4088
Height (m)
19.2024
Cockpit Crew
26
Max Seating
76
Max Speed (km/h)
1013.969
Cruise Speed (km/h)
925.9992
Max Ceiling (m)
13746.48
Capacity Description
76 passengers
Max Mach (Mach)
0.92
National Origin
United States of America
Number Built
2
Powerplant Description
4 × General Electric CF6-80C2B1 turbofan engines
Primary Users
United States Air Force
Status
In service
Wikipedia Article (URL)
en.wikipedia.org/wiki/Boeing_VC-25
Flat Wing Span (m)
59.7408
Wake Category
H
Number of Engines
4