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U.S. Navy Fact Sheet T-34C Turbomentor training aircraft Description Features |
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| 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 | ||
| Primary Function: Training platform for Navy/Marine Corps pilots. | ||
| Contractor: Raytheon Aircraft Company (Formally Beech Aircraft). | ||
| Date Deployed: Operational: 1977. | ||
| Unit Cost: $1 million. | ||
| Propulsion: Model PT6A-25 turbo-prop engine (Pratt & Whitney Aircraft of Canada). | ||
| Length: 28 feet 8 inches (9 meters). | ||
| Height: 9 feet 11 inches (3 meters). | ||
| Wingspan: 33 feet 5 inches (10 meters). | ||
| Weight: 4,425 Lb., Empty Wt. approx. 3,000 Lb. | ||
| Airspeed: Max: 280 Knots (322 miles per hour or 515 km per hour). | ||
| Ceiling: 25,000 Feet . | ||
| Range: Approximately 600 nautical miles. | ||
| Crew: Two (instructor pilot, student pilot). | ||
| Armament: None. | ||
| Last Update: 18 February 2009 | ||