Airworthiness Directive 05-24525
one-timeAirworthiness Directives; Airbus Model A320-111 Airplanes, and Model A320-200 Series Airplanes
What this AD requires
This document corrects information in an existing airworthiness directive (AD) that applies to certain Airbus Model A320- 111 airplanes, and Model A320-200 series airplanes. That AD currently requires a detailed inspection of the tail cone triangle to determine its position, and corrective actions if necessary. This document corrects the applicability by specifying that the AD affects only airplanes identified in Airbus Service Bulletin A320-27-1132, Revision 01, dated June 19, 2002. This correction is necessary to ensure that only affected airplanes are subject to the requirements of the AD.
Which aircraft AD 05-24525 applies to
Whether AD 05-24525 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.
How AD compliance is recorded
A valid compliance record (14 CFR 43.9) states:
Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.
Look up a tail number →Read the full directive (Federal Register)Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.