AD 2020-10-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Weatherly | Various | Airworthiness Directives; Weatherly Aircraft Company |
Unsafe Condition
fatigue cracking of the center wing and outer wing spar hinge brackets due to corrosion pitting
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
repetitive inspections of the wing hinge brackets, pins, and wing spar structure with repair or replacement of parts as necessary
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 5 years after the effective date of this AD, or within 5 years after the initial inspection required by paragraph (g) of this AD, whichever occurs later
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Weatherly Aircraft Company Models 201, 201A, 201B, 201C, 620, 620A, 620B, 620B-TG, and 620TP airplanes
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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