Summary
The FAA proposes to adopt a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-401 and -402 airplanes. This proposed AD was prompted by multiple in-service reports of cracks in elevator power control unit (PCU) brackets (fittings) and the elevator front spar. This proposed AD would require replacing bushings and installing new washers on the elevator PCU arm fitting assembly, installing doublers at the front spar of the elevator structure assembly, replacing horizontal stabilizer rear spar elevator PCU fittings, and applicable on-conditions actions. The FAA is proposing this AD to address the unsafe condition on these products.
Directive Details
AD Number
FAA-2025-5402
Document Number
2026-00117
Type
Proposed Rule
Publication Date
January 7, 2026
Comments Close
February 23, 2026
Affected Manufacturer
De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.)
Criticality
routine
Emergency
No
Docket ID
Docket No. FAA-2025-5402
Topics
Official Documents
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