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Thu, Feb 04, 2016

AD: Airbus Airplanes

AD NUMBER: 2016-02-01

PRODUCT: Certain Airbus Model A320-211 and -231 airplanes.

ACTION: Final Rule

SUMMARY: The FAA is superseding Airworthiness Directive (AD) 96-18-06 for the products listed above.

AD 96-18-06 required visual inspections to detect cracks of the pressurized floor fittings at frame 36, and renewal of the zone protective finish or replacement of fittings with new fittings if necessary.

Since AD 96-18-06 was issued, an extended service goal analysis by the manufacturer revealed that the compliance times and repetitive inspection intervals should be reduced to meet the design service goal.

This AD retains the requirements of AD 96-18-06, with reduced compliance times and repetitive inspection intervals. This AD also adds Model A320-212 airplanes to the applicability.

The FAA is issuing this AD to detect and correct fatigue cracking in the pressurized floor fittings at frame 36, which could result in failure of a floor fitting and subsequent depressurization of the fuselage.

DATES: This AD becomes effective March 3, 2016.

FMI: AD

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