AD 2004-05-24

final rule
Data completeness: 70%

Airworthiness Directives; Lycoming Engines (Formerly Textron Lycoming) AEIO-540, IO-540, LTIO-540, O-540, and TIO-540 Series Reciprocating Engines

AD Number
2004-05-24
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2002-NE-31-AD
FR Citation
69 FR 12057

Applicability

TypeManufacturerModelDetails
aircraft Textron Various Airworthiness Directives; Lycoming Engines (Formerly Textron Lycoming) AEIO-540, IO-540, LTIO-540, O-540, and TIO-540 Series Reciprocating Engines

Unsafe Condition

Failure of zinc-plated crankshaft gear retaining bolts could lead to loss of all engine power and possible forced landing.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Replace zinc-plated crankshaft gear retaining bolts using one of the specified kits. The AD expands the affected engine population and adds five additional kits as alternative methods of compliance.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Lycoming Engines (formerly Textron Lycoming) AEIO-540, IO-540, LTIO-540, O-540, and TIO-540 series reciprocating engines, including 161 engines not previously identified.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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