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Airworthiness directives › 2020-05-17

AD 2020-05-17 Airworthiness Directives; Airbus SAS Airplanes

2020-04-24
2020-03-20
39-19867
FAA-2019-0863
Airframe
—

Applicability*9

This AD applies to Airbus SAS Model A318-112, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, A320-214, A320-216, A320-231, A320-232, A320-233, A320-251N, and A320-271N airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2019-0197, dated August 14, 2019 (“EASA AD 2019-0197”).

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, EASA AD 2019-0197.

Unsafe condition

This AD was prompted by a report of marginal clearance between certain fuel sensor covers on rib 24 and the crown of stringer 15 on both left-hand (LH) and right-hand (RH) wings. A possible contact between the shield and the stringer, and/or possible motion between the stringer and the shield, can make the gap more susceptible to sparking in case of lightning strike. The FAA is issuing this AD to address this condition, which could create a source of ignition in a fuel tank vapor space, possibly resulting in a fire or explosion and consequent loss of the airplane.

Affected ADs

None.

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1