AD Amdt-39-10803

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes

AD Number
Amdt-39-10803
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 95-NM-109-AD
FR Citation
63 FR 52579

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300 B2 and B4 Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes

Unsafe Condition

Fatigue-related cracking in fuselage, wings, and vertical stabilizer structures due to fatigue-related stress.

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

Required Actions

Inspect for cracks in fuselage, wings, and vertical stabilizer structures; perform repairs or modifications if necessary. Implement new optional terminating actions for certain airplanes.

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

Affected Aircraft

Airbus Model A300 B2 and B4 series airplanes, including additional airplanes under expanded applicability.

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.

View Official Source ↗ Find More ADs for Airbus A300 B2 and B4

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Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes

Unsafe Condition: The FAA is superseding an existing airworthiness directive (AD), which applies to all Airbus Model A300 B2, B4-100, and B4-200 series airplanes. That AD currently requires supplemental structural i...

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2006-26-10

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2006-15-04 Recurring

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Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes; and Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes)

Unsafe Condition: could result in reduced structural integrity of the fuselage, and consequent rapid decompression of the airplane.

Effective: Aug 24, 2006 Category: aircraft

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