AD 2017-11-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A318-111 and -112 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracks in the 3 o'clock and 9 o'clock pivot fittings of a CFM56 engine's thrust reverser (T/R), caused by a combination of stress and fatigue effects.
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Required Actions
Conduct repetitive inspections for cracking and corrosion of the 3 o'clock and 9 o'clock pivot fittings of a CFM56 engine's T/R. Take corrective actions if necessary.
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Compliance Time
Within 60 months of the effective date.
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Affected Aircraft
All Airbus Model A318-111 and -112 airplanes; Model A319-111, -112, -113, -114, and -115 airplanes; Model A320-211, -212, and -214 airplanes; and Model A321-111, -112, -211, -212, and -213 airplanes, equipped with CFM56-5A or CFM56-5B series engines.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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