Airworthiness Directive
AD 2005-19-22: Airbus Model A330-322, -341, and -342 Airplanes; and Airbus Model A340-200 and -300…
Airworthiness Directives; Airbus Model A330-322, -341, and -342 Airplanes; and Airbus Model A340-200 and -300 Series Airplanes
- Effective
- Oct 7, 2005
- Published
- Sep 22, 2005
- Registered aircraft
- 2
Models this AD may apply to
AI-extracted — verify against originalMatched from the AD's applicability section. Applicability must be confirmed by a mechanic against the aircraft's records.
Aircraft
- Airbus A330-322
- Airbus A330-342
- Airbus A340-211
- Airbus A340-311
- Airbus A340-312
- Airbus A340-313
- Airbus A340-313
- Airbus A340-313
- Serial numbers per Airbus Service Bulletin A330-53-3132, Revision 02, and Airbus Service Bulletin A340-53-4139, Revision 02, dated April 26, 2004
Applicability
From the AD text(c) This AD applies to Airbus Model A330-322, -341, and -342 airplanes; and Model A340-211, -212, -213, -311, -312, and -313 airplanes; certificated in any category; as identified in Airbus Service Bulletin A330-53-3132, Revision 02, dated April 26, 2004, and Airbus Service Bulletin A340-53-4139, Revision 02, dated April 26, 2004, as applicable. Unsafe Condition (d) This AD results from a report of fatigue cracks that initiated in the duct structure of the ram air outlet, which is adjacent to the hydraulics compartment. The FAA is issuing this AD to prevent fatigue cracks in the duct structure of the ram air outlet, which could lead to hot air damage and consequent loss of function of the hydraulics systems.
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