AD 47-25-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bellanca Aircraft Corporation | 14-13 | Airworthiness Directives; Bellanca Model 14- 13, 14-13-2 |
| aircraft | Bellanca Aircraft Corporation | 14-13-2 | Airworthiness Directives; Bellanca Model 14- 13, 14-13-2 |
Unsafe Condition
Cracks in the fin and stabilizer fittings to which the tail bracing tie rods attach could lead to structural failure of the tail assembly.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the fin and stabilizer fittings for cracks at each 25-hour inspection up to the next 100-hour check. Replace cracked fittings by the next 100-hour check or September 1, 1947, whichever comes first, and install reinforcing gussets.
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Compliance Time
prior to August 1, 1947
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Affected Aircraft
Bellanca Model 14-13, 14-13-2, serial numbers 1060 through 1560 inclusive
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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