AD Amdt-39-9988
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320 | Airworthiness Directives; Airbus Model A320 Series Airplanes |
Unsafe Condition
Fatigue cracking in the front spar of the wing center section can reduce the structural integrity of fuselage frame 36 and the wing center section.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install shims and new fasteners to modify the front spar of the wing center section to reinforce pressure floor fittings.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A320 series airplanes as specified by the manufacturer's report and fatigue testing.
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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