AD 2017-06-12

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Airplanes

AD Number
2017-06-12
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2014-0922
FR Citation
82 FR 15281

Applicability

TypeManufacturerModelDetails
aircraft Airbus A319 and A320 Airworthiness Directives; Airbus Airplanes

Unsafe Condition

Fatigue cracking could appear at certain fastener locations in the longeron area below the emergency exit cut-outs, which could lead to failure of the fasteners and reduced structural integrity of the airplane.

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

Required Actions

Modify certain fastener locations in the longeron area below the emergency exit cut-outs on the left-hand (LH) and right-hand (RH) sides of the fuselage.

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Compliance Time

Before further flight

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Affected Aircraft

Airbus Model A319 and A320 series airplanes, excluding those with Airbus Modification 152637 embodied in production.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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