AD 2003-21-04

final rule
Data completeness: 80%

Airworthiness Directives; Cessna Aircraft Company Models 208 and 208B Airplanes

AD Number
2003-21-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2003-CE-41-AD
FR Citation
68 FR 59707

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company Models 208 and 208B Airworthiness Directives; Cessna Aircraft Company Models 208 and 208B Airplanes
aircraft Bell crank for cracks Airworthiness Directives; Cessna Aircraft Company Models 208 and 208B Airplanes

Unsafe Condition

Reports of cracks and missing/incomplete welds in the right inboard forward flap bell crank, which could lead to failure of the flap bell crank due to cracks, deformation, or missing/incomplete welds.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect the right inboard forward flap bell crank for cracks, deformation, and missing/incomplete welds. If found, immediately replace the flap bell crank or temporarily incorporate certain flap limitations.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within a certain time frame (as specified in the referenced service bulletin).

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Cessna Aircraft Company Models 208 (serial numbers 20800001 through 20800369) and 208B (serial numbers 208B0001 through 208B1014, 208B1017, 208B1018, 208B1020 through 208B1024, 208B1026, and 208B1029 through 208B1033).

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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