AD 2007-19-14

final rule
Data completeness: 70%

Airworthiness Directives; Pilatus Aircraft Limited Model PC-6 Series Airplanes

AD Number
2007-19-14
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2007-29178
FR Citation
72 FR 53920

Applicability

TypeManufacturerModelDetails
aircraft Pilatus Aircraft Limited Model PC-6 Airworthiness Directives; Pilatus Aircraft Limited Model PC-6 Series Airplanes
aircraft Aviat Various Airworthiness Directives; Pilatus Aircraft Limited Model PC-6 Series Airplanes

Unsafe Condition

Corrosion, wear, and cracks in the upper wing strut fittings may lead to failure of the upper attachment fitting, resulting in wing structure failure and loss of control.

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

Required Actions

Inspect the upper wing strut fitting for cracks, wear, and corrosion. Examine the spherical bearing and replace any cracked fittings.

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

Compliance Time

Before further flight

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

Affected Aircraft

Pilatus Aircraft Limited Model PC-6 Series Airplanes

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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