AD 73-12-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Dowty Propellers | (c) R186/4-30-4/ | DOWTY ROTOL Model (c)R186/4-30-4/16 Propellers |
Unsafe Condition
Cracking of the propeller hub front wall
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Strengthen the propeller hub and hub driving center by incorporating Modification No. (c) VP.2388, Revision 3, in accordance with Dowty Rotol Service Bulletin No. 61-604 (Rev. 2) dated November 24, 1971, or an FAA-approved equivalent.
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Compliance Time
Within the next 200 hours' time in service after the effective date of this AD, or prior to the accumulation of 8,000 hours total time in service, whichever occurs later
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Affected Aircraft
Dowty Propellers Model (c)R186/4-30-4/16 propellers not modified per Modification No. (c) VP.2388 (Rev. 3), installed on Armstrong Whitworth Argosy Type A.W. 650 Series 101 airplanes
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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