AD 2016-08-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Fatigue cracking of the inner rear spar, 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
Modify the inner rear spar web of the wing, cold expand the attachment holes of the forward pintle fitting and the actuating cylinder anchorage of the main landing gear, perform repetitive ultrasonic inspections for cracking of the rear spar of the wing, and take corrective action if necessary. The previously optional terminating action is now required.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 12 months of the effective date (June 8, 2016).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A320 series airplanes.
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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