AD 2010-19723
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A380-800 | Airworthiness Directives; Airbus Model A380-800 Series Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A380-800 Series Airplanes |
Unsafe Condition
A crack has been found on the Droop Nose (DN) 1 master sidestay bracket on the inboard leading edge of an Airbus A380 flight test aeroplane. In case of failure of the master bracket, the sub-master bracket would be able to sustain limit loads but not ultimate loads, which could lead to a DN failure affecting the structural integrity of that wing area.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a detailed visual inspection (DVI) of the left-hand and right-hand DN 1 master sidestay brackets to detect cracks. If no cracks are found, repeat the inspection at intervals not to exceed 1,250 flight cycles. If any crack is found, replace the cracked DN 1 master sidestay bracket and perform a DVI for cracks of the associated DN 1 sub-master sidestay bracket.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before the accumulation of 1,250 total flight cycles or within 30 days after the effective date of this AD, whichever occurs later.
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Affected Aircraft
Airbus Model A380-841, -842, and -861 airplanes, certificated in any category, all serial numbers.
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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