Document ID: chunk:federal_register_of_legislation:F2005L02089:body:0:p1
Version: federal_register_of_legislation:F2005L02089
Segment Type: other
Provision Reference: 
Character Range: 0–3377

AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.001(1) of CASR 1998.  The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

Airbus Industrie A319, A320 and A321 Series Aeroplanes
AD/A320/181  Engine - Forward Bolt Mount  9/2005

Applicability:  Airbus A319-131, A319-132, A319-133, A320-232, A320-233, A321-131, A321-231 and A321-232 aircraft models, all aircraft serial numbers that are powered by IAE V2500 series engine with the following engine serial numbers:

                V10002, V10008, V10009, V10010, V10012, V10013, V10015, V10017, V10019, V10020, V10021, V10023, V10024, V10025, V10027, V10030, V10031, V10032, V10034, V10043, V10044, V10045, V10046, V10048, V10049, V10050, V10051, V10056, V10057, V10058, V10059, V10060, V10063, V10064, V10065, V10066, V10068, V10070, V10072, V10073, V10074, V10076, V10077, V10078, V10081, V10082, V10083, V10085, V10086, V10087, V10090, V10091, V10092, V10094, V10095, V10097, V10098, V10099, V10105, V10106, V10108, V10109, V10110, V10115, V10129, V10133, V10140, V10143, V10144, V10146, V10150, V10153, V10157, V10158, V10159, V10162, V10163, V10165, V10167, V10170, V10171, V10182, V10183, V10189, V10191, V10197, V10212, V10213, V10214, V10215, V10217, V10218, V10222, V10224, V10225, V10226, V10227, V10232, V10233, V10239, V10244, V10248, V10280, V10281, V10288, V10289, V10291, V10292, V10302, V10304, V10305, V10306, V10308, V10311, V10316, V10317, V10319, V10323, V10327, V10333, V10345, V10350, V10351, V10353, V10354, V10357, V10358, V10359, V10365, V10367, V10368, V10372, V10373, V10374, V10376, V10377, V10378, V10388, V10390, V10394, V10395, V10402, V10406, V10409, V10419, V10428, V10444, V10484, V10511, V10545, V10592, V10602, V10640, V10707, V10740, V10747, V10769, V10770, V10842, V10847, V10989, V11111, V11116, V11162, V11181, V11185, V11262, V11307, V11311, V11345, V11346, V11437, V11438,

                V10022, V10029, V10038, V10041, V10047, V10052, V10053, V10054, V10062, V10067, V10069, V10071, V10075, V10088, V10089, V10104, V10121, V10131, V10133, V10135, V10137, V10138, V10139, V10141, V10142, V10164, V10166, V10186, V10206, V10238, V10240, V10245, V10246, V10283, V10414, V10416, V10443, V10479, V10522, V10598, V10599, V10664, V10665, V10684, V10709, V10755, V10765, V10796.
Requirement:       1. Perform a detailed inspection of the forward engine mount primary load path components and apply all necessary corrective actions in accordance with Airbus All Operator Telex (AOT) A320-71A1036 revision 1.  Accomplishment of A320 MPD check reference 712111-03 or engine shop visit are equivalent if already done within less than 2250 flight cycles before the effective date of this AD.

                2. Remove and reinstall the bolts attaching the engine forward mount to the engine, in accordance, with AOT A320-71A1036 revision 1.