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Information About

Pac 750xl




A utility aircraft, combing the engine and wings of the PAC Cresco with a new large fuselage and modified tail, the PAC 750 is a conventional metal monoplane with tricycle undercarriage; all versions to date have been powered by a 750 hp (560 kW) Pratt & Whitney Canada PT6A turboprop. It is designed and manufactured in Hamilton , New Zealand by the Pacific Aerospace Corporation .


OVERVIEW


The design made its maiden flight in 2001, (with a slightly different horizontal tail surfaces). The PAC 750 received full FAA certification in 2004. It was marketed initially to Sky Diving operators but is now widely used for agricultural applications, passenger and freight operations and Aerial Photography and surveying . The Cresco’s (predecessor) high lift wings enable the type to take a load of parachutists to 12,000 feet (3,700 m) and return to land in a quarter of an hour. The singled engine PAC 750's running costs are a fraction of the twin-engined DHC-6 "Twin Otter" , making it an economical replacement for the skydiving industries workhorse. One aircraft has been extensively modified for geo-survey work, being fitted with a Magnetic Anomaly Detector sting tail. Military and bush flying roles are also foreseen, and studies have been completed for ski and float conversions. About 30 aircraft have been manufactured in New Zealand by mid-2005. Recently an airframe has been delivered to the Taumarunui Aerial Co-op for use as a top dresser.

The type is marketed in the U.S. by the Utility Aircraft Corporation .


General characteristics

  • Crew: 1 pilot, 9 passengers or 17 skydivers.

  • Wing loading: 24.59 lb/ft&2 (120 kg/m&2)

  • Empty: 3100 lb (1410 kg)

  • Loaded: 7500 lb (3400 kg)

  • Powerplant: 750 hp (560 kW) Pratt & Whitney Canada PT6A turboprop



Performance

  • Cruising speed: 170 kt (315 km/h)

  • Range: 582 nautical miles (1078 km) (max load and 45 minute reserve)

  • Service ceiling: 20,000 ft (6100 m)

  • Endurance: 5 hours fully loaded with 45 minute reserves.

  • Ground roll: 1244 ft (379 m)

  • Rate of climb: At least 1000 ft/min (5 m/s) at maximum take-off load.



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