AD 2008-13-06

final rule
Data completeness: 80%

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

AD Number
2008-13-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2008-0331
FR Citation
73 FR 35898

Applicability

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

Unsafe Condition

Chafed wiring found on wire bundles in the left and right wings containing the auto-control wing de-ice system, fuel quantity indication, and low fuel annunciation systems.

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

Required Actions

Inspect the left and right wing electrical wire bundles at the anchor attach points for loose and damaged wiring. If damaged wiring is found, repair or replace the damaged wire. Inspect the wire bundles for correct attachment to the anchor points and correct any deficient attachments.

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

Compliance Time

Within the next 200 hours time-in-service after July 30, 2008, or within 12 months after July 30, 2008, whichever comes first.

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 20800415) and 208B (serial numbers 208B0001 through 208B1299).

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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