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Printed from https://aircraftdirectives.com/engines/lycoming-io360-l2a/breakdown · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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Lycoming

IO-360-L2A

Four parallel-valve cylinders, a vertical fuel injector, standard top fuel manifold and four supported nozzle lines.

Rendered exterior of the Lycoming IO-360-L2A engine

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Model accuracy & scope

Reviewed exterior models with fitted geometry. Installed part numbers and component-level manual matching remain unverified unless explicitly identified.

  • Reviewed first exterior; dimensions, routes and materials include fitted approximations. Not exact installed OEM geometry.
  • Parts groups are a browsing aid, not an OEM exploded assembly or an installed parts catalogue.
  • Internal mechanisms, functional flow and maintenance fit are not established.
  • Standard top-manifold configuration only; exact serial and accessory identities remain unknown.
  • Two injector-body sliver topology edges and simplified finish remain deferred.

Use the applicable manufacturer manual and parts catalogue for maintenance and exact installation details.

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Manufacturer references

These references inform the model as a whole. A component is linked to a specific page or figure only when that match has been verified.

  1. Lycoming IO-360-L2A Illustrated Parts Catalog PC-IO-360-L2A

    Document host: www.lycoming.com

    June 2025; some illustration footers retain January 2018

    Reference pages: Figs 9, 18, 21, 22

    L2A component roles with standard Figure 22 manifold arrangement; fitted dimensions and exact installed accessory identities remain unverified.