AD Amdt-39-11477
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | British | Aerospace BAe Model ATP | Airworthiness Directives; British Aerospace BAe Model ATP Airplanes |
Unsafe Condition
Chafing and subsequent damage to the engine intake de-icing system wiring, and contamination of electrical connectors and plugs, which could result in loss of engine intake de-icing capability, accretion of ice in the intake duct, ice ingestion, and consequent engine flameout.
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Required Actions
Within 180 days after the effective date, inspect the cable looms, wires, electrical connectors, and associated hardware for damage; replace damaged parts; reroute and modify the flexible duct cable loom and inlet duct power loom; and install new connector boots and backshells on electrical connectors on the engine intake de-icing system, in accordance with British Aerospace Service Bulletin ATP-30-056.
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Compliance Time
Within 180 days after the effective date of this AD.
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Affected Aircraft
British Aerospace BAe Model ATP airplanes, constructor's numbers 2002 through 2063 inclusive, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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