← FAA Federal Register actions

Airworthiness Directives; Airbus Airplanes

airworthiness · Rule · Final rule. · Published 2016-11-29 · Effective 2017-01-03 · 81 FR 85837

Document

Document number
2016-28335
Federal Register citation
81 FR 85837
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus
Publication date
2016-11-29
Effective date
2017-01-03
FAA docket
Docket No. FAA-2016-5596

Abstract

We are superseding Airworthiness Directive (AD) 2014-12-06 for certain Airbus Model A300 B4-600, B4-600R, and F4-600R series airplanes, and Model A300 C4-605R Variant F airplanes (collectively called Model A300-600 series airplanes); and Airbus Model A310 series airplanes. AD 2014-12-06 required repetitive ultrasonic or detailed inspections of the external area of the aft cargo door sill beam for cracking, and repair if necessary, and provided an optional one-time high frequency eddy current (HFEC) inspection that would terminate the repetitive inspections. This new AD requires the previously optional terminating HFEC inspection, and requires that it be done repetitively. This AD was prompted by findings of multiple fatigue cracks in the aft cargo door that indicated the need for additional, repetitive, HFEC inspections. We are issuing this AD to address the unsafe condition on these products.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown