AD 2004-18-01

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Hoffmann Propeller GmbH & Co KG Models HO-V343 and HO-V343K Propellers

AD Number
2004-18-01
Status
final_rule
Effective Date
Product Category
propeller
Docket
Docket No. FAA-2004-18958
FR Citation
69 FR 53603

Unsafe Condition

A blade separating from either a model HO-V343 or HO-V343K propeller, potentially due to propeller hub failure and blade separation from an unknown root cause.

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

Required Actions

Initial and repetitive visual inspections of propeller blades for blade shake and blade nut preload. Initial and repetitive eddy current inspections of blade hubs for damage or cracks.

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

Compliance Time

Within 50 flight hours after the effective date of this AD.

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Affected Aircraft

Hoffmann Propeller GmbH & Co KG models HO-V343 and HO-V343K propellers installed on general aviation airplanes, possibly having an FAA-approved Supplemental Type Certificate.

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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