AD 95-23-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE Systems (Operations) Limited | BAe 146-100A | Airworthiness Directives; Avro Model BAe 146 Series Airplanes |
| aircraft | BAE Systems (Operations) Limited | BAe 146-200A | Airworthiness Directives; Avro Model BAe 146 Series Airplanes |
| aircraft | BAE Systems (Operations) Limited | BAe 146-300A | Airworthiness Directives; Avro Model BAe 146 Series Airplanes |
Unsafe Condition
Cracking and damage of the fastener holes in the butt strap at rib 2 at the lower surface of the right-hand wing due to reduced edge margin between fastener hole centers and the edge of the butt strap, leading to a decrease in the long-term damage tolerance residual strength of the wing.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive eddy current inspections and visual inspections of the four fastener holes at rib 2 butt strap on the lower surface of the right-hand wing to detect cracking, scoring, or incorrect hole diameter. Repair discrepancies by oversizing holes and installing new bolts as per Service Bulletin 57-40.
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
Avro Model BAe 146 series airplanes with constructors' numbers E2188, E2192, E3190, and E3194.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.