Airworthiness Directive

AD 2026-11-06 91 FR 33584 Active

Federal Aviation Administration · 14 CFR part 39

Requires repetitive inspections for cracking and corrosion of the affected barrel nuts and applicable corrective actions.

FR document
2026-11217
Amendment
39-23367
Published
2026-06-04
Effective
2026-07-09
Models covered
1

Last live check: 2026-10-04

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AD

2026-11-06

FR doc 2026-11217 · 91 FR 33584

AD 2026-11-06Published 2026-06-04Effective 2026-07-09

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires repetitive inspections for cracking and corrosion of the affected barrel nuts and applicable corrective actions.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for all De Havilland Aircraft of Canada Limited Model DHC-8 airplanes. This AD was prompted by reports of cracked barrel nuts at the wing front spar and horizontal stabilizer to vertical stabilizer joint. This AD requires repetitive inspections for cracking and corrosion of the affected barrel nuts and applicable corrective actions. The FAA is issuing this AD to address the unsafe condition on these products.

More directives for de Havilland DHC-8 Dash 8

  1. AD 2026-08-07 Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type ... Effective 2026-06-03
  2. AD 2025-19-05 Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type ... Effective 2025-10-31
  3. AD 2025-05-06 Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type ... Effective 2025-04-16
  4. AD 2024-22-07 Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type ... Effective 2024-12-31
  5. AD 2024-12-06 Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type ... Effective 2024-08-21

All de Havilland DHC-8 Dash 8 directives

Applies to 1 model in our index