Airworthiness Directive 2019-22-04

recurring
Official AD 2019-22-04 · FR doc 2019-24995 · 2019-11-19 · airframe

Airworthiness Directives; Airbus SAS Airplanes

What this AD requires

The FAA is superseding Airworthiness Directive (AD) 96-25-04, which applied to certain Airbus SAS Model A320 series airplanes. AD 96- 25-04 required repetitive inspections of the wire looms in the wing and the horizontal stabilizer and in certain areas of the main landing gear (MLG) bays; repair or replacement, protection, and realignment, if necessary; installation of protective sleeves; and realignment of certain bundles. This AD partially retains the requirements of AD 96-25-04 and requires modification of the wing electrical installation; as specified in a European Aviation Safety Agency (EASA) AD, which is incorporated by reference. This AD was prompted by a determination that there were issues with protective sleeves previously installed as specified in AD 96-25-04. The FAA is issuing this AD to address the unsafe condition on these products.

Repetitive inspection. Re-inspect. The next-due date/hours depend on this aircraft’s time in service — a records report computes it from the logbooks.

Which aircraft AD 2019-22-04 applies to

MakesAirbus
ModelsA320-211, A320-212, A320-231, A320

Applies to airplanes identified in EASA AD 2018-0200, dated September 6, 2018.

Whether AD 2019-22-04 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:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 2019-22-04 complied with on your aircraft?

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.