AD 2017-14-14

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Airbus Airplanes

AD Number
2017-14-14
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2016-9498
FR Citation
82 FR 33002

Applicability

TypeManufacturerModelDetails
aircraft Airbus A321 Airworthiness Directives; Airbus Airplanes

Unsafe Condition

Cracks could develop in the cabin floor beam junction at fuselage frame locations FR 35.1 and FR 35.2, on both left-hand (LH) and right-hand (RH) sides.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Repetitive inspections for cracking in the cabin floor beam junction at fuselage frame locations FR 35.1 and FR 35.2, on both LH and RH sides, are required. Repair is necessary if cracking is detected.

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

All Airbus Model A321 series airplanes.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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