Airworthiness directives › 2012-23-10
AD 2012-23-10 Airworthiness Directives; Airbus Airplanes
Models named: A318-111, -112, -121, -122, A319-111, -113, -114, -115, -131, -132. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to all Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any category; all manufacturer serial numbers.
Compliance
You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.
Required actions
Except as provided by paragraph (i) of this AD, within 36 months after the effective date of this AD: Modify the escape slide rafts that have a part number (P/N) specified in table 1 to paragraph (g) of this AD, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A320-25-1723, dated December 17, 2010 (for Model A319, A320, and A321 series airplanes); or Airbus Service Bulletin A320-25-1724, dated December 17, 2010 (for Model A318 series airplanes). Table 1 to Paragraph ( g ) of This AD—Escape Slide Raft Air Cruisers and Aerazur escape slide rafts part number if fitted with a reservoir and valve assembly P/N D18309-105 or P/N D18309-205 D30664-105 D30664-107 D30664-109 D30664-305 D30664-307 D30664-309 D30664-311 D30665-105 D30665-107 D30665-109 D30665-305 D30665-307 D30665-309 D30665-311
Unsafe condition
This AD was prompted by reports of the escape slide of the raft inflation system not deploying when activated due to the rotation of the cable guide in a direction which resulted in jamming of the inflation control table. We are issuing this AD to prevent non-deployment of the inflation system of the escape slide raft, which could result in delayed evacuation from the airplane during an emergency, and consequent injury to the passengers.
Affected ADs
None.
Read the original on the Federal Register →
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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