AD 2024-17-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE | Systems (Operations) Limited | Airworthiness Directives; BAE Systems (Operations) Limited Airplanes |
Unsafe Condition
Cracking on the radius of the rib 0 forward longeron at frame 26, which could lead to failure of adjacent structure, fuselage skin failure, and potential rapid decompression or loss of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a visual and high frequency eddy current inspection for defects of the radius of the rib 0 forward longeron at frame 26. Repair any cracking or defects found before further flight, using an approved method.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 4 months after the effective date of the AD.
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, -300A, and Avro 146-RJ70A, -RJ85A, -RJ100A 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
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