AD 2006-07-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A319-131 | Airworthiness Directives; Airbus Model A319-131, -132, and -133; A320-232 and -233; and A321-131, -231, and -232 Airplanes |
Unsafe Condition
Incorrect torque was applied to the attachment bolts during modification of certain engine forward mount assemblies, which could result in structural failure of the secondary load path of the forward engine mount. Combined with failure of the primary load path, this could lead to separation of the engine from the airplane.
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Required Actions
Inspect for cracks or failure of the primary load path components of the engine forward mount, and perform corrective action if necessary. Remove, re-install, and re-torque the attachment bolts for the secondary load path.
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Compliance Time
Within 5 days for Model A321-131, -231, and -232 airplanes; within 10 days for Model A319-131, -132, and -133 airplanes; and within 10 days for Model A320-232 and -233 airplanes, all after the effective date of this AD.
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Affected Aircraft
Airbus Model A319-131, -132, and -133; A320-232 and -233; and A321-131, -231, and -232 airplanes, certificated in any category, as identified in Airbus All Operators Telex A320-71A1036, Revision 1, dated June 28, 2005.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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