Firewall Forward CAM 125

From Wikipedia, the free encyclopedia
Jump to navigation Jump to search
CAM 125
TypePiston aircraft engine
National originCanada
ManufacturerFirewall Forward Aero Engines

The Firewall Forward CAM 125 is a 125 hp (93 kW) four-cylinder, four-stroke, liquid-cooled piston aircraft engine built by Firewall Forward Aero Engines.[1] The engine is based on a Honda automotive piston engine.[2]

Applications

[edit | edit source]

Specifications (CAM 125)

[edit | edit source]

Data from World Directory of Leisure Aviation & Firewall Forward Aero Engines[1][2]

General characteristics

  • Type: Four-cylinder, four-stroke piston engine
  • Bore: 75 mm (2.95 in)
  • Stroke: 84.6 mm (3.33 in)
  • Displacement: 1590 cm3 (97 cu in)
  • Length: 33.25 inches (845 mm)
  • Width: 21.5 inches (550 mm)
  • Height: 23 inches (580 mm)
  • Dry weight: 247 pounds (112 kg)

Components

  • Valvetrain: Overhead camshaft
  • Fuel type: 90 Octane petrol or 100LL aviation petrol
  • Cooling system: Uses a water-glycol mixture with a camshaft belt driven water pump.
  • Reduction gear: 2.4:1 reduction ratio (6,000 rpm engine, 2,500 rpm propeller).
  • Starting system Electric gear reduction starter.

Performance

See also

[edit | edit source]

Related development

Related lists

References

[edit | edit source]

Notes

[edit | edit source]
  1. ^ a b Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  2. ^ a b Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
[edit | edit source]