AD 47-07-04
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
The control sticks may become disengaged from the socket due to insufficient safetying of the AN393-51 clevis pin, leading to loss of control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Rework both front and rear control sticks by drilling through the stick and socket, installing an AN393-51 clevis pin with washer AN 960-10L and cotter AN 380-2-2, and properly safetying the pin.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
next 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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