Airworthiness Directives (ADs)
CAA-2017-06-005
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
- 2017/06/13
-
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 (MSN), except those on which Airbus modification (mod) 160000 (A319 and A320 structural reinforcement for sharklet installation) or mod 160021 (A321 structural reinforcement for sharklet installation) was implemented in production.
-
Model Number
- AIRBUS A318, A319, A320, and A321 aeroplanes
-
CAA AD Number
- CAA-2017-06-005
-
Aeronautics Authority of Original AD
- EASA
-
Original AD Number
- 2017-0099
-
Effective Date
- 2017/06/22
-
Subject
- Wings – Front Spar Vertical Stringers – Inspection
-
Reference Publications (Revision/ATA/SB)
- ATA 57. This AD supersedes EASA AD 2014-0069(CAA-2014-03-016) dated 19 March 2014. Ref. Publications: Airbus SB A320-57-1016 Revision 02 dated 20 January 1998. and Airbus SB A320-57-1017 original issue dated 03 September 1991, or Revision 01 dated 17 March 1997. and Airbus SB A320-57-1178 Revision 01 dated 28 May 2014, or Revision 02 dated 20 November 2015, or Revision 03 dated 29 November 2016. and Airbus SB A320-57-1200 original issue dated 20 November 2015.
-
Remarks
-
Download
-
