AD 43-07-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fairchild Hiller Corporation | M-62A | Airworthiness Directives; Fairchild M-62 Series Aircraft |
| aircraft | Fairchild Hiller Corporation | M-62A-3 | Airworthiness Directives; Fairchild M-62 Series Aircraft |
| aircraft | Fairchild Hiller Corporation | M-62B | Airworthiness Directives; Fairchild M-62 Series Aircraft |
Unsafe Condition
Wood deterioration and weakened glue joints due to moisture accumulation in the wing center-section front and rear spars.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
At each periodic inspection, examine the wing center-section front and rear spars for wood deterioration and weakened glue joints. Follow Fairchild Service Maintenance Bulletin 45-62-1, dated March 10, 1945, for inspection methods and repairs if needed.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
At each periodic inspection
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Affected Aircraft
Fairchild Hiller Corporation M-62A, M-62A-3, M-62B aircraft
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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