Warner Scarab Junior

From Wikipedia, the free encyclopedia
  (Redirected from Warner Scarab Jr)
Jump to: navigation, search
Scarab Junior
Type Radial engine
Manufacturer Warner Aircraft Corporation
First run November 1930
Developed from Warner Scarab

The Warner Scarab Junior was an American, five-cylinder, air-cooled, radial aero engine first produced in 1930. It was a scaled-down derivative of the seven-cylinder Warner Scarab, developing 90 hp (70 kW) against the Scarab's 110 hp (80 kW).

Applications[edit]

Specifications (Warner Scarab Junior 50)[edit]

Data from FAA Type Certificate Data Sheet (TCDS).[1]

General characteristics

  • Type: Five-cylinder, air-cooled, radial piston engine
  • Bore: 4.25 in (108 mm)
  • Stroke: 4.25 (108 mm)
  • Displacement: 301 cu in (4.93 L)
  • Length: 14 in (35.5 cm)
  • Height: 36.5 in (93 cm)
  • Dry weight: 237 lb (107.5 kg)

Components

  • Valvetrain: 1 inlet and 1 exhaust valve per cylinder
  • Fuel system: 1 Holley carburetor
  • Fuel type: 54 octane Avgas

Performance

See also[edit]

Related development
Comparable engines
Related lists

References[edit]

  1. ^ FAA TCDS - E-54 Retrieved: November 19, 2010.]