AD 2010-05-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; BAE SYSTEMS (Operations) Limited Model ATP Airplanes |
Unsafe Condition
Fatigue cracking of certain structural elements, which could result in reduced structural integrity of the airplane and consequent rapid decompression of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the fuselage for fatigue cracking and corrosion, and depending on findings, repair or replace damaged components as defined in BAE Systems (Operations) Limited Service Bulletin ATP-51-002, Revision 3.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the timeframes specified in BAE Systems (Operations) Limited Service Bulletin ATP-51-002, Revision 3.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
BAE SYSTEMS (Operations) Limited Model ATP Airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.