Airworthiness Directive

AD 2006-20-09 71 FR 57407 Active

Federal Aviation Administration · 14 CFR part 39

FR document
E6-15958
Amendment
39-14778
Published
2006-09-29
Effective
2006-11-03
Models covered
4

Last live check: 2026-08-19

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AD

2006-20-09

FR doc E6-15958 · 71 FR 57407

AD 2006-20-09Published 2006-09-29Effective 2006-11-03

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires replacing certain crankshafts.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for certain Lycoming Engines (L)O-360, (L)IO-360, AEIO-360, O-540, IO-540, AEIO-540, (L)TIO-540, IO-580, and IO-720 series reciprocating engines. This AD requires replacing certain crankshafts. This AD results from reports of 23 confirmed failures of similar crankshafts in Lycoming Engines 360 and 540 series reciprocating engines. We are issuing this AD to prevent failure of the crankshaft, which will result in total engine power loss, in-flight engine failure, and possible loss of the aircraft.

More directives for Lycoming IO-580

  1. AD 2012-19-01 Airworthiness Directives; Lycoming Engines Reciprocating Engines Effective 2012-10-24

All Lycoming IO-580 directives

Applies to 4 models in our index