AD 75-27-07

final rule
Data completeness: 70%

Airworthiness Directives; Pilatus Model PC-6 Airplanes (all variants)

AD Number
75-27-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Pilatus Aircraft Limited PC-6 Airworthiness Directives; Pilatus Model PC-6 Airplanes (all variants)
aircraft Pilatus Aircraft Limited PC-6-H1 Airworthiness Directives; Pilatus Model PC-6 Airplanes (all variants)
aircraft Pilatus Aircraft Limited PC-6-H2 Airworthiness Directives; Pilatus Model PC-6 Airplanes (all variants)
aircraft Pilatus Aircraft Limited PC-6/350 Airworthiness Directives; Pilatus Model PC-6 Airplanes (all variants)
aircraft Pilatus Aircraft Limited PC-6/350-H1 Airworthiness Directives; Pilatus Model PC-6 Airplanes (all variants)
aircraft Pilatus Aircraft Limited PC-6/350-H2 Airworthiness Directives; Pilatus Model PC-6 Airplanes (all variants)
aircraft Pilatus Aircraft Limited PC-6/A Airworthiness Directives; Pilatus Model PC-6 Airplanes (all variants)
aircraft Pilatus Aircraft Limited PC-6/A-H1 Airworthiness Directives; Pilatus Model PC-6 Airplanes (all variants)
aircraft Pilatus Aircraft Limited PC-6/A-H2 Airworthiness Directives; Pilatus Model PC-6 Airplanes (all variants)
aircraft Pilatus Aircraft Limited PC-6/B-H2 Airworthiness Directives; Pilatus Model PC-6 Airplanes (all variants)

Unsafe Condition

Fatigue failure of the pilot and copilot rudder bar junction welded seam due to non-continuous (250 degrees) weld design.

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

Required Actions

Visually inspect the junction fillet welds for coverage and cracks using specified methods. If cracks are found, repair or replace the rudder bars. Replace rudder bars with improved 360-degree weld design within specified timeframes.

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

Compliance Time

Within the next 10 hours' time in service after the effective date, and subsequent inspections at intervals not to exceed 100 hours' time in service.

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

Affected Aircraft

Pilatus Aircraft Ltd. and Fairchild Hiller Model PC-6 airplanes (all variants), serial numbers 338 through 623 and 2001 through 2067.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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