AD 2015-25-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B2-1C | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracks of the pylon side panels (upper section) at rib 8, which could lead to reduced structural integrity 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
Repetitive inspections for cracking of pylons 1 and 2 side panels (upper section) at rib 8 with reduced compliance times, and corrective actions if necessary. Repetitive post-repair and post-modification inspections and repair if necessary. Optional modification (installing a doubler) to terminate repetitive inspections.
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 B2-1C, B2-203, B2K-3C, B4-103, B4-203, B4-2C airplanes; Model A310 series airplanes; Model A300 B4-600 series airplanes; and Model A300 B4-600R series airplanes, excluding airplanes with Airbus Mod 03599.
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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