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Most species of Bothriolepis were relatively small, benthic, freshwater detritivores, averaging around 30 centimetres (12 in) in length.[1] However, the largest species, B. maxima, had a carapace about 100 centimetres (39 in) in length. Bothriolepisfossils are found in Middle and Late Devonian strata (387–360 million years ago).[2] Because the fossils are found in freshwater sediments, Bothriolepis is presumed to have spent most of its life in freshwater rivers and lakes, but was probably able to enter salt water as well because its range appeared to have corresponded with the Devonian continental coastlines. Many paleontologists[who?] hypothesize that they were anadromous, that is, they lived most of their lives in saltwater, and returned to freshwater only to breed, similar to salmon. Its box-like body was enclosed in armor plates, providing protection from predators.

Being a typical antiarch, it had a heavily armoured head attached to the thoracic shield. It had a long pair of spine-likepectoral fins, jointed at the base, and again a little more than halfway along. These spike-like fins were probably used to lift the body clear off the bottom; its heavy armor would have made it sink quickly as soon as it lost forward momentum.[1][2]Bothriolepis had a peculiar spiral, sediment-filled gut and probably grubbed in the mud. It may also have used its pectoral fins to throw sediment (mud, sand or otherwise) over itself.

There are two openings through its head: a keyhole opening along the midline on the upper side for the eyes and nostrils and a mouth on the lower side near the front. It also had a special feature on its skull, a separate partition of bone below the opening for the eyes and nostrils enclosing the nasal capsules called a preorbital recess. It had gills in addition to a pair of pouches off the esophagus that, according to scientific speculation, may have functioned as lungs. It has been hypothesized that these lungs, coupled with the jointed arms and rigid, supportive skeleton, would allow Bothriolepis to travel on land. Bothriolepis had a slender fish-like tail that extended behind the heavily armored portion, which is unfortunately rarely preserved in fossils.

O-360
Lycoming IO-360-A1B6
Type
National originUnited States
ManufacturerLycoming Engines
First run1952
1963 (injected version)
Major applicationsAmerican Champion Decathlon
Cessna 172 R & S
Cessna 177 Cardinal
Piper Archer & Arrow
Robinson R22
Tecnam P2010
Zlín Z 242
Produced1955–present
Developed intoLycoming IO-390
Lycoming O-540
Lycoming IO-720
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The Lycoming O-360 is a family of four-cylinder, direct-drive, horizontally opposed, air-cooled, pistonaircraft engines. Engines in the O-360 series produce between 145 and 225 horsepower (109 to 168 kW), with the basic O-360 producing 180 horsepower.[1]

The engine family has been installed in thousands of aircraft, including the Cessna 172, Piper Cherokee/Archer, Grumman Tiger, and many home-built types. It has a factory rated time between overhaul (TBO) of 2000 hours[1] or twelve years.[2] O-360 family engines are also widely used in airboats, most notably in the Hurricane Aircats used by the US Army during the Vietnam War.[3]

The first O-360 certified was the A1A model, certified on 20 July 1955 to United States CAR 13 effective March 5, 1952 as amended by 13-1 and 13-2.[4] The Lycoming IO-390 is an O-360 which has had its cylinder bore increased by 3⁄16 inch (4.76 mm), developing 210 hp (157 kW).[5][6]

Series[edit]

The O-360 family of engines comprises 167 different models with 12 different prefixes. All have a 361-cubic-inch (5.92-liter) displacement and 5.125 and 4.375 in (130.2 and 111.1 mm) bore and stroke.[4][7][8][9]

  • O-360carbureted series
  • HO-360 horizontally mounted series for helicopter installation
  • LO-360 same as O-360, but with left-hand rotating crankshaft, for use in pairs on twin-engined aircraft[10]
  • TO-360turbocharged series
  • LTO-360 turbocharged left-hand rotation series
  • IO-360fuel-injected series
  • LIO-360 same as IO-360, but with left-hand rotating crankshaft
  • AIO-360 inverted mount (dry sump aerobatic) fuel-injected series
  • AEIO-360aerobatic fuel-injected series
  • HIO-360 horizontally mounted fuel-injected series for helicopters
  • LHIO-360 left-hand rotation, fuel-injected, horizontally mounted for helicopters
  • TIO-360 turbocharged and fuel-injected series

Variants[edit]

Applications[edit]

Piper PA-44-180 Seminole features two Lycoming O-360 engines
O-360
360
  • Hurricane Aircat (airboat)
LO-360
IO-360
  • Cessna 172R/172S
  • Mooney M20[11]
LIO-360
An LIO-360 on the starboard wing of a Piper PA-34-200 Seneca I.
AIO-360
AEIO-360
HIO-360
LHIO-360
  • Silvercraft SH-3[12]
  • Silvercraft SH-4[12]

Specifications (O-360-A1A)[edit]

Data from Type Certificate Data Sheet E-286[4]

General characteristics

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  • Type: Four-cylinder, dual magneto, horizontally opposed, four-strokeaircraft engine
  • Bore: 5.125 in (130 mm)
  • Stroke: 4.375 in (111 mm)
  • Displacement: 361 cu in (5,916 cc)
  • Dry weight: 258 lb (117 kg)

Components

  • Fuel type: 91/96 avgas minimum grade[13]
  • Oil system: 8 US qt (8 l) wet sump
  • Cooling system: air-cooled

Performance

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  • Power output: 180 hp (134 kW) at 2700 rpm
  • Compression ratio: 8.5:1
  • Fuel consumption: 7.8 US gal (30 L) to 9 US gal (34 L) per hour[14]

See also[edit]

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Related lists

References[edit]

  1. ^ abLycoming (2004). '360 Series'(PDF). Archived from the original(PDF) on 2010-11-26. Retrieved 2008-09-16.
  2. ^Lycoming Engines (8 July 2013). 'Recommended Time Between Overhaul Periods'(PDF). Archived from the original(PDF) on 2013-09-13. Retrieved 8 July 2013.
  3. ^Enfield, Samuel; Burr, R.; Badgett, R.; et al., eds. (April 15, 1966). Airboats(PDF) (Technical report). San Francisco: Army Concept Team in Vietnam. p. 2. R-1590 0 – via DTIC.
  4. ^ abcFederal Aviation Administration (August 2009). 'Type Certificate Data Sheet No. E-286 Revision 20'(PDF). Retrieved 9 September 2011.
  5. ^Lycoming Engines (n.d.). 'Lycoming IO-390-X'. Retrieved 2009-01-07.
  6. ^Lycoming Engines (2004). 'Specialty datasheet'(PDF). Retrieved 2008-12-20.
  7. ^Federal Aviation Administration (10 January 2018). 'Type Certificate Data Sheet No. 1E10 Revision 28'(PDF). Retrieved 26 January 2019.
  8. ^Federal Aviation Administration (March 1986). 'Type Certificate Data Sheet No. E26EA Revision 4'. Retrieved 2009-01-18.
  9. ^Federal Aviation Administration (March 1986). 'Type Certificate Data Sheet No. E16EA Revision 5'. Retrieved 2009-01-18.
  10. ^Federal Aviation Administration (13 July 2004). 'Airplane Flying Handbook'(PDF). Archived from the original(PDF) on 21 September 2012. Retrieved 18 September 2012.
  11. ^Mooney Aircraft, Inc. (March 1967). Executive 21 Owners Manual.
  12. ^ abFederal Aviation Administration (February 2007). 'Docket No. FAA-2006-25948; Directorate Identifier 2006-NE-32-AD; Amendment 39-14951; AD 2007-04-19'. Archived from the original on 2011-07-13. Retrieved 2009-03-09.
  13. ^Lycoming (2010). 'Lycoming Service Instruction 1070Q'(PDF). Archived from the original(PDF) on 17 November 2011. Retrieved 3 November 2011.
  14. ^'O-360, HO-360, IO-360, AIO-360, HIO-360 & TIO-360 Operator's Manual'. lycoming.com. Retrieved 11 July 2018.

External links[edit]

Wikimedia Commons has media related to Lycoming O-360.
  • 'Operator's Manual O-360, HO-360, IO-360, AIO-360, HIO-360 & TIO-360 Series'(PDF). Lycoming. October 2005.

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