Pilatus P-4

1954

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Pilatus P-4

The Pilatus P-4 represented another attempt by the company to get into the market for civil aircraft, but this five-seat cabin monoplane had little more success than its SB-2 predecessor. Of braced high-wing monoplane configuration, with fixed tailwheel landing gear, a braced tail unit and a 142kW Avco Lycoming O-435 engine, the P-4 had accommodation for a pilot and four passengers. All passenger seats were removable easily so that the P-4 could be used as a cargo carrier, or as an air ambulance accommodating two stretchers and two medical attendants. With a wing span of 11.85m and maximum take-off weight of 1500kg, the P-4 had a maximum speed of 245km/h.

Specification 
 MODELP-4
 CREW1
 PASSENGERS4
 ENGINE1 x Avco Lycoming O-435, 142kW
 WEIGHTS
  Take-off weight1500 kg3307 lb
 DIMENSIONS
  Wingspan11.85 m39 ft 11 in
 PERFORMANCE
  Max. speed245 km/h152 mph

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