AD 2016-16-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE | Systems (Operations) Limited | Airworthiness Directives; BAE Systems (Operations) Limited Airplanes |
Unsafe Condition
Corrosion and cracking of the wing fixed leading edge and front spar structure, which could result in reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Revise inspection procedures to terminate a previously approved inspection method. Conduct repetitive inspections of the wing fixed leading edge and front spar structure for corrosion and cracking, and repair if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 12 years or 36,000 flight cycles, whichever occurs earlier, for airplanes without enhanced corrosion protection. Within 6 years or 36,000 flight cycles, whichever occurs earlier, for airplanes with enhanced corrosion protection.
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 and Avro 146 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
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