AD Amdt-39-9730

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A320-111, -211, and -231 Series Airplanes

AD Number
Amdt-39-9730
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 95-NM-249-AD
FR Citation
61 FR 46703

Applicability

TypeManufacturerModelDetails
aircraft Airbus A320-111 Airworthiness Directives; Airbus Model A320-111, -211, and -231 Series Airplanes

Unsafe Condition

Fatigue cracking found on the pressurized floor fitting at frame 36 under the lower surface panel.

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

Required Actions

Perform visual inspections to detect cracks of the fittings of the pressurized floor at frame 36. Renew the zone protective finish or replace the fittings with new fittings if necessary.

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

Compliance Time

Before further flight

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

Affected Aircraft

Airbus Model A320-111, -211, and -231 series airplanes

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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