Fieseler Fi 158

The Fieseler Fi 158 was a civilian German experimental aircraft the Gerhard Fieseler Werke.

Developed the aircraft 1938 as an experimental aircraft for record purposes. The aircraft was a cantilever low- wing monoplane of wooden construction with retractable landing gear normal. Attached great importance to the designers, the aerodynamic optimization of the cell. The rudder was designed as a double tail. When driving an air-cooled six-cylinder in-line engine Hirth HM 506 served with 160 hp.

Specifications

Fieseler Fi 158

  • Wingspan: 7.0 m
  • Length: 6.6 m
  • Height: 1.7 m
  • Wing area: 7.0 m²
  • Empty weight: 494 kg
  • Max. Start Weight: 646 kg
  • Maximum speed: 350 km / h
  • Service ceiling: 6700 m
  • Range: 370 km
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