AD 58-06-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Kelowna Flightcraft R & D Ltd. | 240 Series | CONVAIR Model 240 Series Aircraft |
Unsafe Condition
Cracking and failures of the main landing gear axle at the 2.9998-2.9990-inch diameter adjacent to the brake flange, leading to complete axle failure and loss of main landing gear wheel.
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Required Actions
Inspect for cracks in the specified axle area using dye penetrant or equivalent procedure. Replace or rework parts with cracks. Discontinue inspections after rework per Bendix Service Bulletin L.G.595 or FAA-approved equivalent.
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Compliance Time
Not later than May 15, 1958, and at each 300 hours of operation or next regular inspection nearest thereto.
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Affected Aircraft
CONVAIR Model 240 Series Aircraft equipped with Bendix Main Landing Gear Assemblies Nos. 155150-1, 155370-1, 159695-6, and 159589-90.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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