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Airworthiness directives › 2026-16-13

AD 2026-16-13 Airworthiness Directives; Pratt & Whitney Canada Corp. Engines

2026-08-31
2026-08-14
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Engine
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Models named: PW210A, PW210A1, PW210S. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to all Pratt & Whitney Canada Corp. Model PW210A, PW210A1, and PW210S engines.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

For the purpose of this AD, an “engine start” includes the start of an engine for any reason, even if it is not followed by a flight.

Unsafe condition

This AD was prompted by reports of circumferential cracks found at the turbine exhaust frame external surface caused by thermal stress from engine starts. The FAA is issuing this AD to prevent failure of the turbine exhaust frame. The unsafe condition, if not addressed, could result in turbine exhaust frame failure, which could lead to loss of axial containment, release of parts, and damage to the helicopter.

Affected ADs

This AD replaces AD 2026-13-09, Amendment 39-23391 (91 FR 38991, June 29, 2026).

Read the original on the Federal Register →

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1