AD 2015-18-51

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Helicopters

AD Number
2015-18-51
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2015-3877
FR Citation
80 FR 60030

Applicability

TypeManufacturerModelDetails
aircraft Airbus Helicopters Model AS332C Airworthiness Directives; Airbus Helicopters

Unsafe Condition

T/R de-icing system power supply box stuck in a 'closed' position providing an uncontrolled and un-annunciated power supply to the system, causing overheating and potential structural damage to the T/R blades.

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

Required Actions

Inspect each T/R blade for burn marks, disbonding of leading edge protection, or cracks at the junction of the skin and leading edge protection. Replace all T/R blades if any damage is found. Deactivate the rotor de-icing system, revise the rotorcraft flight manual (RFM) to state the system is deactivated and flight into known icing is prohibited, and install a placard indicating the system is deactivated.

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 Helicopters Model AS332C, AS332C1, AS332L, and AS332L1 helicopters with T/R de-icing installation unit part number 204ZP01Y01 and T/R blade part number 332A12-0055-XX (where XX is any dash number).

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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