AD 2010-17-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A330-201 | Airworthiness Directives; Airbus Model A330-201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342, and -343 Airplanes, Model A340-211, -212, -213, -311, -312, and -313 Airplanes, and Model A340-541 and -642 Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A330-201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342, and -343 Airplanes, Model A340-211, -212, -213, -311, -312, and -313 Airplanes, and Model A340-541 and -642 Airplanes |
Unsafe Condition
Loose pneumatic quick-disconnect unions on Goodrich pitot probes P/N 0851HL, potentially due to mis-torque at equipment manufacturing level, could lead to an air leak, resulting in incorrect total pressure measurement and erroneous Calibrated Airspeed (CAS)/MACH parameters delivered by the Air Data Computer (ADC).
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Required Actions
Inspect the pneumatic quick-disconnect union on Goodrich P/N 0851HL pitot probes for adequate torque. Apply torque if the union is not adequately torqued. Install pitot probes marked with a red torque check-indicating mark without further action.
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Compliance Time
Before further flight
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Affected Aircraft
Airbus Model A330-201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes, Model A340-211, -212, -213, -311, -312, and -313 airplanes, and Model A340-541 and -642 airplanes.
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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