AD 53-09-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Viking Air Limited | DHC-2 Mk.I | Airworthiness Directives de Havilland Model DHC-2 Beaver Aircraft |
| aircraft | Viking Air Limited | DHC-2 Mk.II | Airworthiness Directives de Havilland Model DHC-2 Beaver Aircraft |
| aircraft | Viking Air Limited | DHC-2 Mk.III | Airworthiness Directives de Havilland Model DHC-2 Beaver Aircraft |
Unsafe Condition
Skin cracks on the fuselage side panel at front door step.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect as soon as practical but not later than the next 100-hour flying time and at 100-hour intervals thereafter for skin cracks. Stop drill cracks at each end and repair according to sketch directions if found.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
as soon as practical but not later than the next 100-hour flying time
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Viking Air Limited DHC-2 Mk.I, DHC-2 Mk.II, DHC-2 Mk.III aircraft
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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