Document

Airworthiness Directives; Airbus Airplanes

We are superseding Airworthiness Directive (AD) 2005-15-07 for certain Airbus Model A320-111 airplanes and Model A320-200 series airplanes. AD 2005-15-07 required installing ins...

We are superseding Airworthiness Directive (AD) 2005-15-07 for certain Airbus Model A320-111 airplanes and Model A320-200 series airplanes. AD 2005-15-07 required installing insulator and cable ties to the electrical cables of the S routes at the gaps in the raceway in the wing trailing edge and the wing tip and wing root areas. This new AD requires additional modifications in the trailing edges of both wings. This new AD also removes airplanes from the applicability. This AD was prompted by reports of wire chafing in the left-hand wing trailing edge. We are issuing this AD to prevent wire chafing in the trailing edge of the wings, which could result in a short circuit in the vicinity of the fuel tanks, consequently resulting in a potential source of ignition in a fuel tank vapor space and consequent fuel tank explosion.

Legal Citation

Federal Register Citation

Use this for formal legal and research references to the published document.

81 FR 64051

Web Citation

Suggested Web Citation

Use this when citing the archival web version of the document.

“Airworthiness Directives; Airbus Airplanes,” thefederalregister.org (September 19, 2016), https://thefederalregister.org/documents/2016-22191/airworthiness-directives-airbus-airplanes.