AD 58-22-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Thompson Aircraft Sales | T-28A | Airworthiness Directives; North American Model T-28A Aircraft |
Unsafe Condition
Fatigue cracks emanating from the bolt holes in the main landing gear trunnion shaft.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the main landing gear trunnion shaft every 200 hours with a borescope or equivalent method for fatigue cracks. Replace all defective shafts.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
every 200 hours
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
North American Model T-28A Aircraft Certificated in the Restricted Category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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