Boeing, which merged with McDonnell Douglas in 1997, continued to manufacture C-17s for export customers following the end of deliveries to the U.S. Air Force. Aside from the United States, the C-17 is in service with the United Kingdom, Australia, Canada, Qatar, United Arab Emirates, NATO Heavy Airlift Wing, India, and Kuwait. The final C-17 was completed at the Long Beach, California plant and flown on 29 November 2015.
Variants
C-17A: Initial military airlifter version.
C-17A "ER": Unofficial name for C-17As with extended range due to the addition of the center wing tank. This upgrade was incorporated in production beginning in 2001 with Block 13 aircraft.
C-17B: A proposed tactical airlifter version with double-slotted flaps, an additional main landing gear on the center fuselage, more powerful engines, and other systems for shorter landing and take-off distances. Boeing offered the C-17B to the U.S. military in 2007 for carrying the Army's Future Combat Systems (FCS) vehicles and other equipment.
MD-17: Proposed variant for civilian operators, later redesignated as BC-17 after 1997 merger.
Specifications (C-17)
General characteristics- Crew: 3: 2 pilots, 1 loadmaster
- Capacity:
- 102 paratroopers or
- 134 troops with palletized and sidewall seats or
- 54 troops with sidewall seats (allows 13 cargo pallets) only or
- 36 litter and 54 ambulatory patients and medical attendants or
- Cargo, such as one M1 Abrams tank, three Strykers, or six M1117 Armored Security Vehicles
- Payload: 170,900 lb (77,520 kg) of cargo distributed at max over 18 463L master pallets or a mix of palletized cargo and vehicles
- Length: 174 ft (53 m)
- Wingspan: 169.8 ft (51.75 m)
- Height: 55.1 ft (16.8 m)
- Wing area: 3,800 ft² (353 m²)
- Empty weight: 282,500 lb (128,100 kg)
- Max. takeoff weight: 585,000 lb (265,350 kg)
- Fuel capacity: 35,546 U.S. gal (134,556 L)
- Powerplant: 4 × Pratt & Whitney F117-PW-100 turbofans, 40,440 lbf (180 kN) each
- Cruise speed: Mach 0.74 (450 knots, 515 mph (829 km/h))
- Range: 2,420 nmi (2,785 mi (4,482 km)) ; 5,610 nmi (10,390 km) with paratroopers
- Service ceiling: 45,000 ft (13,716 m)
- Max. wing loading: 150 lb/ft² (750 kg/m²)
- Minimum thrust/weight: 0.277
- Takeoff run at MTOW: 7,600 ft (2,300 m)
- Landing distance: 3,000 ft (910 m)
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