Airworthiness Directive

AD 2005-19-11 70 FR 54618 Active

Federal Aviation Administration · 14 CFR part 39

FR document
05-18323
Amendment
39-14276
Published
2005-09-16
Effective
2005-10-21
Models covered
2
Last live check
2026-10-02
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AD

2005-19-11

FR doc 05-18323 · 70 FR 54618

AD 2005-19-11Published 2005-09-16Effective 2005-10-21

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 (formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360, AEIO-540, IO-540, O-540, and TIO-540 series reciprocating engines rated at 300 horsepower (HP) or lower. This AD requires replacing certain crankshafts. This AD results from reports of 12 crankshaft failures in Lycoming 360 and 540 series engines rated at 300 HP or lower. 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.

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All Lycoming O-360 directives

Applies to 2 models in our index