AD 2004-19-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320 | Airworthiness Directives; Airbus Model A320 Series Airplanes |
Unsafe Condition
Fatigue cracking in certain areas of the rear spar of the wing, which may lead to reduced structural integrity of the wing and the main landing gear (MLG).
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect for fatigue cracking in certain areas of the rear spar of the wing. Modify the inner rear spar web of the wing as specified. Perform cold expansion of certain attachment holes for the forward pintle fitting and certain holes at the actuating cylinder anchorage of the main landing gear (MLG).
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Compliance Time
Within 500 flight cycles after June 11, 1993, or within 2,000 flight cycles after February 14, 1994, whichever occurs later, or prior to the accumulation of 12,000 total flight cycles.
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Affected Aircraft
Airbus Model A320 series airplanes, certificated in any category, except those modified in accordance with Airbus Modification 24591.
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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