Airworthiness Directives (ADs)
CAA-2014-10-001(已有後續修訂版)
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
- 2014/10/06
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Applicability
- Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112,
A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211,
A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233,
A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231
and A321-232 aeroplanes, all manufacturer serial numbers.
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Model Number
- A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2014-10-001(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2014-0221
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Effective Date
- 2014/10/14
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Subject
- Landing Gear – Main Landing Gear Door Actuator – Monitoring /
Inspection / Replacement / Modification
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Reference Publications (Revision/ATA/SB)
- ATA 32. This AD supersedes EASA AD 2013-0288(CAA-2013-12-007) dated 06 December 2013. Ref. Airbus AFM TR 437 dated 06 June 2014. and Airbus AOT A320-32A1390 original issue dated 10 February 2011. and Airbus SB A320-32-1390 Revision 01 dated 21 September 2011, or Revision 02 dated 23 October 2013, or Revision 03 dated 13 July 2014.
Airbus AOT A32N001-13 original issue dated 24 June 2013. and Airbus SB A320-32-1409 original issue dated 19 March 2013. and Airbus SB A320-32-1407 original issue dated 14 May 2013, or Revision 01
dated 03 July 2014. and Airbus SB A320-31-1414 original issue dated 19 December 2012, or Revision 01 dated 21 March 2013, or Revision 02 dated 30 July 2013. and GE SB 114122-32-105 original issue dated 17 January 2013.
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Remarks
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