AD 49-38-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Kelowna Flightcraft R & D Ltd. | 240 Series | CONVAIR Model 240 Aircraft |
Unsafe Condition
Cracking of the nose gear landing struts in the areas directly below the drag link attachment legs due to repeated loadings during landings.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect nose landing gear struts for cracks below drag strut attachment lugs using visual means. Repair by grinding, blending, and polishing if possible; retire struts ineligible for repair. Discontinue inspection if struts are reinforced with support clamp and eyebolts per Bendix Service Bulletins L.G. 510/511.
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Compliance Time
on No. 1 inspection on all nose landing gear struts whose total operating time exceeds 1,000 hours
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Affected Aircraft
CONVAIR Model 240 Aircraft incorporating original type nose strut outer cylinder, Bendix P/N 156842
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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