AD 2010-10-22
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE | SYSTEMS (Operations) Limited Model BAe 146 | Airworthiness Directives; BAE SYSTEMS (Operations) Limited Model BAe 146 Airplanes and Model Avro 146-RJ Airplanes |
Unsafe Condition
Fatigue cracking of certain structural elements could adversely affect the structural integrity of these airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Revise the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness to incorporate new and more restrictive life limits for certain items. Conduct inspections to detect fatigue cracking in certain structures. Revise the airworthiness limitations to include critical design configuration control limitations for the fuel system.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the compliance times specified in the revised ALS.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All BAE SYSTEMS (Operations) Limited Model BAe 146-100A, -200A, and -300A series airplanes; and Model Avro 146-RJ70A, 146-RJ85A, and 146-RJ100A airplanes, certificated in any category.
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.