AD Amdt-39-10851

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A320 Series Airplanes

AD Number
Amdt-39-10851
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 98-NM-29-AD
FR Citation
63 FR 56542

Applicability

TypeManufacturerModelDetails
aircraft Airbus A320 Airworthiness Directives; Airbus Model A320 Series Airplanes

Unsafe Condition

Fatigue cracking of the lower surface panel on the wing center box, which could result in reduced structural integrity of the airplane.

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

Required Actions

Conduct repetitive inspections to detect fatigue cracking of the lower surface panel on the wing center box. Repair the panel if necessary. Modify the lower surface panel on the wing center box as a terminating action for the repetitive inspections.

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

Affected Aircraft

Airbus Model A320 series airplanes, as specified in the AD.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.