AD/A320/51 - Main Landing Gear Rear Pintle Pin

Airworthiness Directive - AD/A320/51 - Main Landing Gear Rear Pintle Pin Airworthiness Directive - AD/A320/51 - Main Landing Gear Rear Pintle Pin CASA Airworthiness Directive Jurisdiction:Commonwealth of Australia;CorporateName:Civil Aviation Safety Authority; Issue 5/1995,Aircraft above 5700 kg,Airbus Industrie A319, A320 and A321 Series Aeroplanes,Main Landing Gear Rear Pintle Pin,51 DellaCa, Donna 2 0 2022-10-28T00:27:00Z 2022-10-28T00:27:00Z 1 117 673 Office of Parliamentary Counsel 5 1 789 16.0000 2006-09-22T00:00:00Z Toolkit http://www.activepdf.com 2022-10-28T00:00:00Z COMMONWEALTH OF AUSTRALIA   (Civil Aviation Regulations 1998) , PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES   Airbus Industrie A319, A320 and A321 Series Aeroplanes   AD/A320/51   Main Landing Gear Rear Pintle Pin   5/95 Applicability:   A320 S/N 002 to 008, 010 to 014 and 016 to 021.   Requirement:   Replace the rear pintle pin in the main landing gear in accordance with Airbus Industrie Service Bulletin A320-32-1024.   Note: DGAC AD 94-240-061(B) refers.   Compliance:   Before 20000 landings or during the next main landing gear overhaul, whichever occurs first.   Background:   Three cracked pins have been found on the fatigue specimen. To improve the fatigue performance, A320-100 pins are replaced by A320-200 pins on aircraft in service.