title: Reims-Cessna F406 Caravan II
text: # Reims-Cessna F406 Caravan II
  
  The Reims-Cessna F406 Caravan II is a turboprop twin engine utility aircraft manufactured and designed by Reims Aviation in cooperation with Cessna.
  
  ## Design and development
  
  The F406 Caravan II is a twin turboprop engined, fourteen-seat low-wing monoplane of conventional aluminium and steel 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, and was produced by Reims Aviation until the company's 2013 demise. The F406 is aimed at passenger and small cargo transport, and 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 makes it comply with European regulations regarding commercial operations, which only allow 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. The Type Certificate transferred only had approval to produce spare parts and not the whole aircraft.
  
  ## Operators
  
  ### Australia
  
  * Customs and Border Protection Service
  * Aerologistics Survey
  
  ### France
  
  * French Army
  * Air Saint-Pierre
  
  ### Greece
  
  * Hellenic Coast Guard
  
  ### Namibia
  
  * Fisheries and Marine Resources
  * Westair Aviation
  
  ### South Korea
  
  * Republic of Korea Navy
  
  ### United Kingdom
  
  * HM Coastguard
  * Environment Agency
  * RVL Aviation
  
  ## Specifications
  
  Data from Jane's All the World's Aircraft 1988–89
  
  General characteristics
  
  * Crew: One
  * Capacity: 12 passengers
  * Length: 11.89 m (39 ft 0 in)
  * Wingspan: 15.09 m (49 ft 6 in)
  * Height: 4.01 m (13 ft 2 in)
  * Wing area: 23.48 $m^2$ (253 sq ft)
  * 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)
  * Cruise speed: 260 km/h (160 mph, 140 kn)
  * Range: 2,135 km (1,327 mi, 1,153 nmi)
  * Service ceiling: 9,145 m (30,000 ft)
  * Rate of climb: 9.4 m/s (1,850 ft/min)
  