Air Force One
Technical Specs
Crew
26 (passenger/crew capacity: 102)
Model
747-200B
Engines
General Electric CF6-80C2B1
Thrust rating
56,700 pounds, each engine
Long-range mission takeoff gross weight
833,000 pounds
Maximum zero fuel weight
526,500 pounds
Design mission zero fuel weight
46,000 pounds
Maximum landing weight
630,000 pounds
Fuel capacity
53,611 gallons
Range
7,800 statute miles
Wing span
195 feet, 8 inches
Length
231 feet, 10 inches
Height
63 feet, 5 inches
Service ceiling
45,100 feet.
Specifications (VC-25A)
Data from Boeing BDS[16]
General characteristics
- Crew: 26: 2 pilots, flight engineer, navigator,[3] and cabin crew
- Capacity: 76 passengers
- Length: 231 ft 5 in (70.6 m)
- Wingspan: 195 ft 8 in (59.6 m)
- Height: 63 ft 5 in (19.3 m)
- Max. takeoff weight: 833,000 lb (375,000 kg)
- Powerplant: 4 × General Electric CF6-80C2B1F turbofans, 56,700 lbf (250 kN) each
- Zero fuel weight: 526,500 lb (238,800 kg)
Performance
- Maximum speed: Mach 0.92 (630 mph, 1,015 km/h) at 35,000 ft altitude
- Cruise speed: Mach 0.84 (575 mph, 925 km/h) at 35,000 ft altitude
- Range: 6,800 nmi (7,800 mi, 13,000 km)
- Service ceiling: 45,100 ft (13,700 m)
C-130 Hercules
A Hercules deploying flares, sometimes referred to as Angel Flares due to the characteristic pattern.