AD 2004-17-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna | Aircraft Company Models 208 and 208B | Airworthiness Directives; Cessna Aircraft Company Models 208 and 208B Airplanes |
| aircraft | Bell | crank with a life limit of 40 | Airworthiness Directives; Cessna Aircraft Company Models 208 and 208B Airplanes |
Unsafe Condition
Cracks in the flap bellcranks could result in failure of this part, leading to damage to the flap system and surrounding structure, and potentially reduced or loss of control of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Repetitively inspect the flap bellcranks for cracks. Eventually replace the bellcranks. Install a newly designed bellcrank with a life limit of 40,000 landings to terminate repetitive inspections.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours after the effective date of this AD.
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Affected Aircraft
Cessna Aircraft Company Models 208 and 208B airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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