
U.S. Navy Fact Sheet CH-53D Sea Stallion helicopter Description Background |
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| Service Marine Corps | ||
| Point Of Contact Naval Air Systems Command Public Affairs Department 47123 Buse Road, Unit IPT Bldg. 2272, Suite 075 Patuxent River, MD 20670-5440 (301)757-1487 | ||
| General Characteristics | ||
| Contractor: Sikorsky Aircraft Division of United Technologies Corp. | ||
| Date Deployed: First flight: Oct 14, 1964; Operational: November 1966. | ||
| Propulsion: Two General Electric T64-GE-413 turboshaft engines (3,925 shaft horsepower each) | ||
| Length: Fuselage: 67.5 feet (20.3 meters); Rotors turning: 88 feet 3 inches (26.5 meters). | ||
| Height: 24 feet 11 inches (7.2 meters). | ||
| Rotor Diameter: 72 feet 3 inches (21.7 meters). | ||
| Weight: 21 tons (max gross) (18.9 metric tons). | ||
| Airspeed: 160 knots (184 miles, 294 km per hour). | ||
| Ceiling: 12,450 feet. | ||
| Range: 578 nautical miles (665 statute miles, 1064 km); 886 nautical miles ferry range. | ||
| Crew: Two pilots, one aircrewman. | ||
| Load: 37 troops or 24 litter patients plus four attendants or 8,000 pounds (3,600 kg) cargo. | ||
| Last Update: 18 February 2009 | ||