Reims-Cessna F406 Caravan II

Utility aircraft From Wikipedia, the free encyclopedia

The Reims-Cessna F406 Caravan II is a turboprop twin engine utility aircraft manufactured and designed by Reims Aviation in cooperation with Cessna.

TypeTwin-engined utility
National originFrance
United States
StatusIn service, production to recommence
Quick facts F406 Caravan II, General information ...
F406 Caravan II
A Cessna F406 from HM Coastguard
General information
TypeTwin-engined utility
National originFrance
United States
ManufacturerReims Aviation
StatusIn service, production to recommence
Primary usersFrench DGDDI
Number built99[a][1]
History
Manufactured1983–2013
First flight22 September 1983
Developed fromCessna 404 Titan
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Design and development

The F406 Caravan II is a twin turboprop engined, fourteen-seat low-wing monoplane of conventional aluminium (airframe) and steel (engine internal parts, exhaust, landing gear) construction. It is a development of the Cessna 404 Titan with two Pratt & Whitney PT6A turboprop engines. The aircraft first flew on 22 September 1983[2] and was produced by Reims Aviation until the company's 2013 demise.[3] The F406 is aimed at passenger and small cargo transport as well as civilian and military surveillance. For extra cargo capacity, a cargo pod can be fitted to the belly of the aircraft.

Though the F406 is more expensive to operate than single-engine aircraft of the same passenger capacity such as the Cessna 208 Caravan, having two engines made it comply with European regulations regarding commercial operations, which for a long time only allowed multi-engine aircraft for commercial instrument flight.

In March 2014, Reims Aviation was acquired by Chinese-owned Continental Motors Inc and renamed ASI Aviation. Two remaining incomplete airframes were finished in France before a shift to Mobile, Alabama with new avionics, electrical, and hydraulic systems; a new autopilot; and an engine choice of current P&WC PT6A-135 or pistons : Continental GTSIO-520 and/or Continental CD-310 diesel.[4] The Type Certificate transferred but only had approval to produce spare parts and not the whole aircraft.[1]

Operators

Specifications

Data from Jane's All the World's Aircraft 1988–89[14]

General characteristics

  • Crew: One[1]
  • Capacity: 12 passengers
  • Length: 11.89 m (39 ft 0 in)
  • Wingspan: 15.09 m (49 ft 6 in) [1]
  • Height: 4.01 m (13 ft 2 in)
  • Wing area: 23.48 m2 (253 sq ft) [1]
  • Empty weight: 2,283 kg (5,033 lb)
  • Max takeoff weight: 4,246–4,700 kg (9,360–10,361 lb)
  • Powerplant: 2 × Pratt & Whitney Canada PT6A-112 turboprop , 373 kW (500 hp) each

Performance

  • Maximum speed: 424 km/h (263 mph, 229 kn) [b]
  • Cruise speed: 388 km/h (241 mph, 209 kn)
  • Range: 2,135 km (1,327 mi, 1,153 nmi) [c]
  • Service ceiling: 9,145 m (30,000 ft)
  • Rate of climb: 9.4 m/s (1,850 ft/min)

See also

Related development

Aircraft of comparable role, configuration, and era

References and notes

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