AD 2009-15-09

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A380-841, -842, and -861 Airplanes

AD Number
2009-15-09
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2009-0644
FR Citation
74 FR 35780

Applicability

TypeManufacturerModelDetails
aircraft Airbus A380-841 Airworthiness Directives; Airbus Model A380-841, -842, and -861 Airplanes
aircraft Aviat Various Airworthiness Directives; Airbus Model A380-841, -842, and -861 Airplanes

Unsafe Condition

Overheat Detection System (OHDS) installation non-conformities along the bleed air ducting may lead to degraded leak detection capability, potentially allowing undetected hot air leakage and causing damage to the airplane structure and components.

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

Required Actions

Inspect the OHDS installation along the bleed air ducting, including specific sensing elements and insulation muffs. Revise the installation to a compliant configuration if non-conformities are found.

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 A380-841, -842, and -861 airplanes, serial numbers 3, 5, 6, 8, 10, 11, 12, 13, 14, 15, 16, 20, and 22.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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