Airworthiness directives › 2016-06-13
AD 2016-06-13 Airworthiness Directives; Airbus Airplanes
Models named: A319-111, -112, -113, -114, -115, -131, -132, -133, A320-211, -212. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to the airplanes identified in paragraphs (c)(1) through (c)(3) of this AD, certificated in any category, all manufacturer serial numbers, except those on which Airbus Modification 26925 has been embodied in production. (1) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (2) Airbus Model A320-211, -212, -214, -231, -232, and -233 airplanes. (3) Airbus Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
Within 24 months after the effective date of this AD, modify the BDDV having a part number listed in the column “Old Part Number” in table 1 to paragraph (g) of this AD; modify the drain hose of the affected BDDV; check for the presence of water, ice, and hydraulic fluid; and re-identify the BDDV to the corresponding part number, as applicable, as listed as “New Part Number” in table 1 to paragraph (g) of this AD; and do all applicable related investigative and corrective actions; in accordance with the Accomplishment Instructions of Airbus Service Bulletin A320-32-1415, dated September 2, 2014. Do all applicable related investigative and corrective actions before further flight. Table 1 to Paragraph ( g ) of This AD—BDDV Part Number Re-Identification Old part number New part number A25434006-3 A25434006-3000 A25434005-101 A25434005-1010 A25434005-201 A25434005-2010 A25434005-301 A25434005-3010 A25434005-401 A25434005-4010 A25434006-101 A25434006-1010 Note 1 to table 1 to paragraph (g) of this AD: The part number listed in table 1 to paragraph (g) of this AD can have an “A” or “B” suffix, which is an indication of the amendment level of the BDDV. This does not affect compliance with this AD.
Unsafe condition
This AD was prompted by investigations that revealed that the cover seal of the BDDV was damaged and did not ensure efficient sealing. We are issuing this AD to prevent damage to the BDDV, which could lead to water ingestion in the BDDV and freezing of the BDDV in flight, possibly resulting in loss of braking system function after landing.
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