AD 47-30-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Gores, William | 65-CA (Army L-3F) | Airworthiness Directives; Aeronca Models 65-CA, S-65-CA and 65-LA |
| aircraft | Gores, William | 65-LA | Airworthiness Directives; Aeronca Models 65-CA, S-65-CA and 65-LA |
| aircraft | Gores, William | S-65-CA | Airworthiness Directives; Aeronca Models 65-CA, S-65-CA and 65-LA |
Unsafe Condition
Failure of the seat belt anchorage during a crash landing due to insufficient reinforcement of the seat installation.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Bolt the rear sliding lugs to the slide tube with 3/16-inch AN bolts if the seat is not adjustable. If adjustable, reinforce with two 0.094 inch 1025 steel gussets welded between the seat cross tube and slide lugs as specified.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
not later than September 30, 1947
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Affected Aircraft
Aeronca Models 65-CA, S-65-CA, and 65-LA
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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