AD 2016-14-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A319 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Fatigue cracking of the forward pressure bulkhead at Frame (FR) 35 on the left-hand (LH) side and right-hand (RH) side, which could result in reduced structural integrity of the airplane.
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Required Actions
Reinforce the forward pressure bulkhead at Frame 35, stringer 30, on both the left-hand and right-hand sides. Measure the diameters of certain fastener holes and, if not oversized, perform a rotating probe inspection for cracking. Cold expand crack-free holes or repair oversize or cracked holes using a method approved by the FAA, EASA, or Airbus's EASA Design Organization Approval (DOA).
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Compliance Time
Before further flight
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Affected Aircraft
All Airbus Model A319, A320, and A321 series airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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