AD 47-07-02
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-62A-4 | Airworthiness Directives; Fairchild M-62 Series Aircraft |
| aircraft | Fairchild Hiller Corporation | M-62B | Airworthiness Directives; Fairchild M-62 Series Aircraft |
| aircraft | Fairchild Hiller Corporation | M-62C | Airworthiness Directives; Fairchild M-62 Series Aircraft |
Unsafe Condition
Looseness in elevator hinge attachments to the rear spar of the stabilizer could lead to structural failure of the elevator control system.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect elevator hinge attachments for looseness during each periodic inspection. Tighten any loose hinges by cutting oval-shaped openings in the stabilizer's lower surface forward of the rear spar, then secure nuts with safety devices and cover openings with fabric patches.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
at each periodic inspection
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Fairchild Hiller Corporation M-62A, M-62A-3, M-62A-4, M-62B, M-62C 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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