European Aviation Safety Agency

ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitation Section Part 2 – Damage Tolerant Airworthiness Limitation Items – Implementation - Airbus Models: A320-251N, A320-271N
 N AD 2016-0239

Annotation

Reason:

The airworthiness limitations for Airbus A320 family aeroplanes are currently included in Airbus A318/A319/A320/A321 Airworthiness Limitations Section (ALS) documents. The Damage Tolerant Airworthiness Limitation Items are published in ALS Part 2, approved by EASA. The instructions contained in the ALS Part 2 have been identified as mandatory actions for continued airworthiness. Failure to comply with these instructions could result in an unsafe condition.

Previously, EASA issued AD 2015-0083 to require accomplishment of all maintenance tasks as described in ALS Part 2 at Revision 03. Since that AD was issued, Airbus issued Revision 04, and later on Revision 05 of the ALS Part 2, including new and/or more restrictive items, and new A320 models were certified.

For the reason described above, this AD retains the requirements of EASA AD 2015-0083, which is superseded, expands the Applicability by adding the models A320-251N and A320-271N, requires accomplishment of all maintenance tasks as described in the ALS Part 2, Revision 05 (hereafter referred to as ‘the ALS’ in this AD), and provides specific compliance times for ALS task 572021-01-1 (Wide Spread Fatigue Damage related).

Автоматический перевод:

ATA 05 – Сроки / Проверки Обслуживания – Часть 2 Раздела Ограничения Летной годности – Наносят ущерб Терпимым Позициям Ограничения Летной годности – Внедрению - Модели Аэробуса: A320-251N, A320-271N