AD 2019-20-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | SAS | Airworthiness Directives; Airbus SAS Airplanes |
Unsafe Condition
fatigue cracking, damage, or corrosion in principal structural elements, which could result in reduced structural integrity of the airplane.
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Required Actions
revise the existing maintenance or inspection program, as applicable, to incorporate the information specified in Airbus A310 Airworthiness Limitations Section (ALS), Part 2, Damage Tolerant Airworthiness Limitation Items (DT-ALI), Revision 03, dated December 14, 2018, as supplemented by Airbus A310 ALS, Part 2, DT-ALI, Variation 3.1, Issue 01, dated December 20, 2018.
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Compliance Time
Within 90 days after the effective date of this AD
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Affected Aircraft
Airbus SAS Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplanes, certificated in any category, all manufacturer serial numbers.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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