AD Amdt-39-9882

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A300 Series Airplanes

AD Number
Amdt-39-9882
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 92-NM-225-AD
FR Citation
62 FR 1383

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300 Airworthiness Directives; Airbus Model A300 Series Airplanes

Unsafe Condition

Fatigue cracking initiating at hole ``I'' of frame 47 on certain Airbus Model A320 series airplanes.

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

Required Actions

Conduct detailed visual inspections to detect cracking of fuselage frame 47, repair if necessary, and provide optional terminating action for repetitive inspections.

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

Affected Aircraft

Airbus Model A320 series airplanes with inadvertently omitted models now included.

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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