AD 2015-20-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A330-200 Freighter | Airworthiness Directives; Airbus Airplanes |
| aircraft | Bell | Various | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracking of rods that attach the belly fairing to the airframe, which could lead to separation of the belly fairing and consequent damage to airplane structure and systems.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect rods for manufacturer identification. For affected parts, inspect rods for any cracking using a high frequency eddy current (HFEC) method. Take corrective actions as necessary to ensure structural integrity of the belly fairing rods. Prohibit installation of affected TAC rods as replacement parts in the belly fairing.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours after the effective date of this AD.
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Affected Aircraft
Airbus Model A330-200 Freighter series airplanes; Model A330-200 and -300 series airplanes; and Model A340-200 and -300 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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