AD 62-18-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | D & R Nevada LLC | 22 | Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22, 22M, and 30 Series Aircraft |
| aircraft | D & R Nevada LLC | 22M | Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22, 22M, and 30 Series Aircraft |
| aircraft | D & R Nevada LLC | 30 | Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22, 22M, and 30 Series Aircraft |
| aircraft | D & R Nevada LLC | 30A | Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22, 22M, and 30 Series Aircraft |
Unsafe Condition
Loose rudder flight tab balance weights, missing weights, missing attachment nuts/bolts, and elongation of attachment bolt holes in balance weights and attachment arms.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect rudder flight tab balance weight attachments for looseness, missing components, and elongated holes per General Dynamics/Convair Alert Service Bulletins A27-60, A27-31, or A27-32. Correct defects prior to next flight as specified in the bulletins or by FAA-approved equivalent method.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 150 hours' time in service following the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
GENERAL DYNAMICS/CONVAIR Models 22, 22M, and 30 Series 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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