Airworthiness Directive 2006-06-16

one-time
Official AD 2006-06-16 · FR doc 06-2759 · 2006-03-23 · reciprocating engine

Airworthiness Directives; Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, and LO-360 Series Reciprocating Engines

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for certain Lycoming Engines (formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, and LO-360 series reciprocating engines. This AD requires replacing certain crankshafts. This AD results from a crankshaft failure in a Lycoming LO-360-A1H6 reciprocating engine. We are issuing this AD to prevent failure of the crankshaft, which could result in total engine power loss, in-flight engine failure, and possible loss of the aircraft.

Which aircraft AD 2006-06-16 applies to

MakesLycoming
ModelsAEIO-360-A1B6, AEIO-360-A1E6, IO-360-A1B6, IO-360-A1B6D, IO-360-A3B6, IO-360-A3B6D, IO-360-C1C6, IO-360-B1G6, IO-360-C1G6, IO-360-C1E6, LO-360-A1G6D, LO-360-A1H6, O-360-A1F6, AEIO-360, IO-360, O-360, LIO-360, LO-360

Applies to AEIO-360, IO-360, O-360, LIO-360, and LO-360 series engines manufactured new or rebuilt, overhauled, or that had a crankshaft installed after March 1, 1999. The model-designation table is truncated in the source text (cut off after O-360-A1F6); additional designations may exist in the full AD.

Whether AD 2006-06-16 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 2006-06-16 complied with on your aircraft?

Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.

Look up a tail number →Read the full directive (Federal Register)

Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.