AD 69-19-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | D & R Nevada LLC | 22 | Airworthiness Directives; GENERAL DYNAMICS Models 22 and 22M Aircraft |
| aircraft | D & R Nevada LLC | 22M | Airworthiness Directives; GENERAL DYNAMICS Models 22 and 22M Aircraft |
Unsafe Condition
Cracks originating near the center jack pad on the lower surface of the main landing gear axle beam, progressing upward and causing failure above the pivot pin due to stress corrosion or hydrogen embrittlement.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect and rework axle beam assemblies per specified service bulletins. Removal of beam material exceeding .006 inch depth requires individual evaluation by FAA Western Region.
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Compliance Time
within the next 2000 hours' time in service after the effective date of this AD or before the accumulation of 9000 hours' total time in service, whichever occurs later
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Affected Aircraft
GENERAL DYNAMICS Model 22 Aircraft with axle beam P/N 9729-68-1 and Model 22M Aircraft with axle beam P/N 1057-68-1
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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