AD 2017-10-23
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A321 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracks could develop on holes at certain fuselage frame locations, specifically at frame (FR) 35.2A between stringers (STR) 22 and STR 23 on the right hand (RH) and left hand (LH) sides, which could reduce the structural integrity of the fuselage.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive special detailed (rototest) inspections (SDI) for cracking on the affected holes at frame 35.2A between stringers 22 and 23, and perform repairs if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
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Affected Aircraft
Airbus Model A321 series airplanes with specific fuselage frame configurations as described in the AD.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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