Airworthiness Directives (ADs)
CAA-2011-12-003
The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.
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Issue Date
- 2011/12/14
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Applicability
- Airbus A319-112, A319-113, A319-132, A320-211, A320-212, A320-214, A320-231, A320-232, A321-111 and A321-131 aeroplanes models, manufacturer serial numbers 0259, 0260, 0264, 0266 to 0270 inclusive, 0275, 0276, 0278, 0287, 0296, 0300, 0303, 0312, 0320, 0321, 0323, 0325, 0328, 0332, 0334, 0335, 0337, 0346, 0352, 0353, 0356, 0365, 0369, 0375, 0377, 0382, 0383, 0396, 0398, 0401, 0412, 0413, 0416, 0419, 0421, 0431, 0432, 0438, 0440, 0441, 0445, 0453, 0458, 0459, 0466, 0468, 0473, 0474, 0482, 0484, 0491, 0493, 0497, 0498, 0501, 0502, 0505, 0507, 0509, 0518, 0520, 0521, 0529, 0531, 0534, 0537, 0538, 0544, 0549, 0554, 0555, 0560, 0563, 0577, 0578, 0585, 0598, 0600, 0608, 0612, 0618, 0621, 0625, 0637, 0660, 0685, 0976, 1010, 1092, 1096, 1103, 1139, 1143, 1158, 1251, 1356 and 1511.
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Model Number
- A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2011-12-003
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2011-0231
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Effective Date
- 2011/12/23
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Subject
- Fuselage – Windshield Central Lower Node Continuity Fittings – Inspection / Repair
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Reference Publications (Revision/ATA/SB)
- ATA 53
Ref. Airbus Service Bulletin A320-53-1245 Revision 01 dated 17 May 2011.
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Remarks
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