AD 2002-22-17
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 | Various | Airworthiness Directives; Cessna Aircraft Company Models 208 and 208B Airplanes |
Unsafe Condition
Cracks in the inboard forward 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
Inspect the inboard forward flap bellcranks for cracks using eddy current inspection upon the accumulation of 4,000 landings or within 250 landings after December 31, 2002, whichever occurs later. Repetitively inspect thereafter at every 500 landings. Replace bellcranks depending on usage.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Initially upon the accumulation of 4,000 landings or within 250 landings after December 31, 2002, whichever occurs later. Repetitive inspections must be conducted every 500 landings thereafter.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cessna Aircraft Company Models 208 and 208B airplanes, all serial numbers, certificated in any category.
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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