AD 50-36-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Kelowna Flightcraft R & D Ltd. | 240 Series | CONVAIR Model 240 Aircraft |
Unsafe Condition
Cracks in the nose strut inner cylinder (P/N 155285) below the scissors lug boss approximately 4 inches above the axle housing, particularly at the machined radius just below the scissors lug boss.
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Required Actions
Visually inspect P/N 155285 with an 8-power or higher glass for cracks in the specified area. Clean and remove paint from the area. Replace part if cracks are found; repair is allowed per Bendix Service Bulletin LG 518.
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Compliance Time
At next No. 1 operation unless already accomplished, on all nose landing gear struts whose total time exceeds 1,000 hours, and at each No. 3 operation thereafter.
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Affected Aircraft
CONVAIR Model 240 Aircraft incorporating original type nose strut inner cylinders, Bendix P/N 155285.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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