Airworthiness Directives (ADs)
CAA-2017-12-001(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.
-
Issue Date
- 2017/12/08
-
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.
-
Model Number
- A318, A319, A320 and A321 aeroplanes
-
CAA AD Number
- CAA-2017-12-001(已有後續修訂版)
-
Aeronautics Authority of Original AD
- EASA
-
Original AD Number
- 2017-0237
-
Effective Date
- 2017/12/18
-
Subject
- Flights Controls – Trimmable Horizontal Stabilizer Actuator – Inspection
-
Reference Publications (Revision/ATA/SB)
- ATA 27. This AD supersedes EASA AD 2014-0147(CAA-2014-06-006) dated 11 June 2014. Ref. Publications: Airbus SB A320-27-1164 Revision 02 dated 30 March 2005, or Revision 03 dated 24 August 2005, or Revision 04 dated 17 July 2006, or Revision 05 dated 11 January 2007, or Revision 06 dated 01 April 2008, or Revision 07 dated 23 June 2009, or Revision 08 dated 06 July 2010, or Revision 09 dated 02 May 2012, or Revision 10 dated 27 March 2014, or Revision 11 dated 15 December 2014, or Revision 12 dated 23 March 2016, or Revision 13 dated 08 August 2016. and Airbus SB A320-27-1245 original issue dated 06 March 2017. and Airbus SB A320-27-1246 original issue dated 20 March 2015, or Revision 01 dated 04 November 2016. and Airbus SB A320-27-1247 original issue dated 06 March 2017.
-
Remarks
-
Download
-
