Summary
We are adopting a new airworthiness directive (AD) certain Airbus Model A310-203, -221, and -222 airplanes. This AD was prompted by the manufacturer re-classifying slat extension eccentric bolts as principal structural elements with replacement due at or before their calculated fatigue lives. This AD replaces certain slat extension eccentric bolts with new bolts. We are issuing this AD to prevent fatigue cracking, which could result in the loss of structural integrity of the airplane.
Directive Details
AD Number
FAA-2012-0414
Document Number
2012-18579
Type
Rule
Publication Date
August 7, 2012
Effective Date
September 11, 2012
Affected Manufacturer
Airbus
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2012-0414
Topics
Official Documents
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