AD Amdt-39-10879
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | de Havilland | DHC-7 | Airworthiness Directives; de Havilland Model DHC-7 Series Airplanes |
Unsafe Condition
Fatigue cracking in certain significant structural areas could reduce the structural integrity of the airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct an additional structural inspection to detect and correct fatigue cracking.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All de Havilland Model DHC-7 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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.