airworthiness · Rule · Final rule. · Published 2015-02-18 · Effective 2015-03-25 · 80 FR 8513
Document
Document number
2015-02697
Federal Register citation
80 FR 8513
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus
Publication date
2015-02-18
Effective date
2015-03-25
FAA docket
Docket No. FAA-2014-0484
Abstract
We are superseding Airworthiness Directive (AD) 2012-09-07 for certain Airbus Model A319-111, -112, and -132 airplanes; Model A320- 111, -211, -212, -214, and -232 airplanes; and Model A321-111, -211, - 212, and -231 airplanes. AD 2012-09-07 required an electrical bonding test between the gravity fill re-fuel adaptor and the top skin panels on the wings; and, if necessary, an inspection for corrosion of the component interface and adjacent area; and repairing the gravity fuel adaptor if necessary. This new AD adds airplanes to the applicability and requires inspecting those airplanes to determine if a repair was done, and doing the electrical bonding test and corrective action if necessary. This AD was prompted by a determination that more airplanes are subject to the identified unsafe condition. We are issuing this AD to detect and correct corrosion and improper bonding, which, in combination with a lightning strike in this area, could create a source of ignition in a fuel tank, resulting in a fire or explosion and consequent loss of the airplane.