AD 99-26-17
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE Systems (Operations) Limited | 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 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 cable looms, wires, electrical connectors, and hardware for damage; replace damaged parts; reroute and modify flexible duct cable loom and inlet duct power loom; install new connector boots and backshells on electrical connectors, per ATP-30-056.
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Compliance Time
Within 180 days after the effective date
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Affected Aircraft
BAe Model ATP airplanes, constructor’s numbers 2002 through 2063 inclusive
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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