Infrastructure

Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes

🇺🇸United States··Proposed Rule·Medium Impact·View source ↗

AI-generated summary for informational purposes only. Not legal advice. See the original source for the authoritative text.

🇬🇧 English

The FAA is proposing to supersede AD 2021-11-08 for all Pilatus PC-6 series airplanes. This new proposed rule requires operators to revise the Airworthiness Limitations Section (ALS) of the aircraft maintenance manual or instructions for continued airworthiness to incorporate new or more restrictive tasks and limitations issued by EASA. Key additions include life limits for the control column pitch trim relay. The proposal shortens the compliance window to 30 days after the effective date instead of 12 months. It also mandates corrective actions if discrepancies are found during required tasks. The goal is to prevent failure of structural components and loss of airplane control due to corrosion, wear, cracks, or unaddressed life-limited parts.

AI-generated summary. May contain errors. Refer to official sources for legal decisions.

Key Changes

  • Supersedes AD 2021-11-08 and incorporates EASA AD 2025-0281 by reference
  • Requires revision of ALS in AMM or ICA within 30 days after effective date
  • Introduces new life limits for the control column pitch trim relay

+ 3 more changes with Pro

Affected Parties

Owners and operators of Pilatus Model PC-6 series airplanes registered in the United StatesMaintenance organizations performing inspections and ALS revisions on these aircraft+1 more…

Tags

airworthiness directive,Pilatus PC-6,FAA regulation
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