Engine model

Lycoming O-435

Lycoming Engines

Airworthiness Directives
1
Service Bulletins
2
Last live check
2026-08-171 of 1 re-verified
What this page is: a restatement of what the official Federal Register and manufacturer records show as of the date listed below each item. It is not a determination that any specific aircraft or engine is, or is not, in compliance. Under 14 CFR §91.403 and §91.417, the aircraft owner/operator is responsible for maintaining airworthiness and required records. Always verify against the official FAA and manufacturer sources linked below before making a maintenance or airworthiness decision.

Airworthiness Directives

1 record
AD

2004-10-14

FR doc 04-11406 · 69 FR 29210

AD 2004-10-14Published 2004-05-21Effective 2004-06-25

Lycoming Engines (Formerly Textron Lycoming), Direct-Drive Reciprocating Engines

Requires inspection of the crankshaft gear installation and rework or replacement of the gears where necessary after a propeller strike, sudden stoppage, at overhaul, or whenever gear train repair is required.

Full official abstract

Airworthiness Directives; Lycoming Engines (Formerly Textron Lycoming), Direct-Drive Reciprocating Engines

The FAA is adopting a new airworthiness directive (AD) that supersedes an existing AD, for Lycoming Engines (formerly Textron Lycoming), direct-drive reciprocating engines (except O-145, O-320H, O- 360E, LO-360E, LTO-360E, O-435, and TIO-541 series engines). That AD currently requires inspection of the crankshaft gear installation and rework or replacement of the gears where necessary after a propeller strike, sudden stoppage, at overhaul, or whenever gear train repair is required. This AD requires the same actions but makes the correction that the existing gear retaining bolt and lockplate be removed from service and new hardware installed, and revises the definitions for sudden stoppage and propeller strike. This AD results from a change to the definition of a propeller strike or sudden stoppage. We are issuing this AD to prevent loosening or failure of the crankshaft gear retaining bolt, which may cause sudden engine failure.

Source: Federal Register document 04-11406, retrieved 2026-08-16 · re-verified against the live Federal Register API 2026-08-17

Service Bulletins

2 records

This page indexes 1 AD and 2 SBs from primary sources. The FAA may have issued additional directives for this engine that are not yet included.

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