AD 63-19-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | D & R Nevada LLC | 30 | Airworthiness Directives; GENERAL DYNAMICS Models 30 and 30A Aircraft |
| aircraft | D & R Nevada LLC | 30A | Airworthiness Directives; GENERAL DYNAMICS Models 30 and 30A Aircraft |
Unsafe Condition
Frayed or damaged horizontal stabilizer trim control cables in the vicinity of the aft pressure bulkhead could result in loss of control of the horizontal stabilizer trim system.
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Required Actions
Conduct a close visual inspection of the horizontal stabilizer trim control cables within 50 hours' time in service after the effective date (or within the last 950 hours' time in service). Inspections must be repeated every 1,000 hours' time in service. Replace frayed or damaged cables before further flight. Repetitive inspections may be discontinued after FAA-approved modification.
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Compliance Time
Within the next 50 hours' time in service after the effective date unless already accomplished within the last 950 hours' time in service
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Affected Aircraft
GENERAL DYNAMICS Models 30 and 30A Aircraft, all serial numbers
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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