AD 2016-18-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B4-203 and A300 B4-2C | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracks found on pylon side panels (upper section) at rib 8, which could lead to reduced strength of the pylon primary structure, possibly resulting in pylon structural failure and in-flight loss of an engine.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a detailed inspection for crack indications of the pylon side panels; conduct a high frequency eddy current (HFEC) inspection to confirm any crack indications; repair any cracking or modify the pylon side panels; and perform repetitive inspections and repair if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within reduced thresholds and intervals as specified in the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A300 B4-203 and A300 B4-2C airplanes, specifically those with cracks found on pylon side panels (upper section) at rib 8.
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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