Specifications .28GSO-526.29 Continental O-526




1 specifications (gso-526)

1.1 general characteristics
1.2 components
1.3 performance





specifications (gso-526)

data jane s world s aircraft 1955-56.


general characteristics

type: 6-cylinder air-cooled horizontally opposed aircraft piston engine
bore: 5.125 in (130.2 mm)
stroke: 4.25 in (108 mm)
displacement: 526 cu in (8.62 l)
length: 52.8 in (1,340 mm)
width: 36 in (910 mm)
height: 23.9 in (610 mm)
dry weight: 540 lb (240 kg)dry

components

fuel type: 91/96 octane
cooling system: air-cooled

performance

power output: 320 hp (240 kw) @ 3,000 rpm take-off
specific power: 0.58 hp/in³ (26.5 kw/l)
compression ratio: 6.0:1
power-to-weight ratio: 0.593 hp/lb (0.97 kw/kg)




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