AD Amdt-39-11401
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | DHC-8-101 | Airworthiness Directives; Bombardier Model DHC-8-101, -102, -103, -106, -201, -202, -301, -311, and -315 Series Airplanes |
Unsafe Condition
Fatigue cracking of the wing ladder plates at over wing access panels between certain stations.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive detailed visual inspections and high frequency eddy current inspections to detect cracking of the wing upper skin and ladder plates. Repair any detected cracking, if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Not specified.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Bombardier Model DHC-8-101, -102, -103, -106, -201, -202, -301, -311, and -315 series airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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