AD 63-20-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bellanca Aircraft Corporation | 14-13 | Airworthiness Directives; Bellanca Model 14-13 Series Aircraft |
| aircraft | Bellanca Aircraft Corporation | 14-13-2 | Airworthiness Directives; Bellanca Model 14-13 Series Aircraft |
| aircraft | Bellanca Aircraft Corporation | 14-13-3 | Airworthiness Directives; Bellanca Model 14-13 Series Aircraft |
| aircraft | Bellanca Aircraft Corporation | 14-13-3W | Airworthiness Directives; Bellanca Model 14-13 Series Aircraft |
Unsafe Condition
Cracks in the welds and adjacent structure where the brake-cylinder support brackets (P/N 9811-17 and -21) are attached to fuselage cross tube P/N 9802-47.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect welds and adjacent structure for cracks using dye penetrant and 10-power glass or FAA approved equivalent. Remove grease/dirt prior to inspection. Repair or replace cracked parts with FAA approved methods or equivalent part before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 hours' time in service after October 21, 1963, and every 50 hours' time in service thereafter.
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Affected Aircraft
Bellanca Model 14-13, 14-13-2, 14-13-3, 14-13-3W 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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