AD 2004-03-06

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A319 and A320 Series Airplanes

AD Number
2004-03-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2002-NM-183-AD
FR Citation
69 FR 5909

Applicability

TypeManufacturerModelDetails
aircraft Airbus A319 and A320 Airworthiness Directives; Airbus Model A319 and A320 Series Airplanes

Unsafe Condition

Fatigue cracking in the wing/fuselage joint cruciform fittings could result in reduced structural integrity of the wing/fuselage.

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

Required Actions

Conduct repetitive ultrasonic inspections for fatigue cracking in the wing/fuselage joint cruciform fittings at a reduced inspection threshold and repetitive interval. Take corrective actions if necessary.

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

Affected Aircraft

All Airbus Model A320 series airplanes, including additional airplanes added to the applicability by this amendment.

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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