AD 2005-19-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAe | Systems (Operations) Limited Model ATP | Airworthiness Directives; BAe Systems (Operations) Limited Model ATP Airplanes |
Unsafe Condition
Fatigue cracking in certain structures and significant structural items, and insufficient life limits for certain equipment and components.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Revise the Airworthiness Limitations Section of the Instructions for Continued Airworthiness to incorporate life limits for certain items, conduct new inspections to detect fatigue cracking, and revise life limits for certain equipment and components.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All 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 6, 2026
Rights: U.S. Government Public Domain
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