AD/A320/38 - Nose Section - Structural Reinforcement

Airworthiness Directive - AD/A320/38 - Nose Section - Structural Reinforcement Airworthiness Directive - AD/A320/38 - Nose Section - Structural Reinforcement CASA Airworthiness Directive Jurisdiction:Commonwealth of Australia;CorporateName:Civil Aviation Safety Authority; Issue 9/1994,Aircraft above 5700 kg,Airbus Industrie A319, A320 and A321 Series Aeroplanes,Nose Section - Structural Reinforcement,38 DellaCa, Donna 2 0 2022-10-27T00:45:00Z 2022-10-27T00:45:00Z 1 162 924 Office of Parliamentary Counsel 7 2 1084 16.0000 2006-09-22T00:00:00Z Toolkit http://www.activepdf.com 2022-10-27T00:00:00Z 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/A320/38   Nose Section - Structural Reinforcement   9/94 Applicability:   A320 Aircraft, Serial Numbers 5 to 8 inclusive and 10 to 24 inclusive. Requirement:   Replace the existing angles and fittings at fuselage frames 1 and 2 (fuselage stations 350 and 385) in accordance with the Accomplishment Instructions of Airbus Industrie Service Bulletin A320-53- 1002.   Note: DGAC AD 92-203-032(B) refers.   Compliance:   Accomplish the applicable modifications before 12000 flights for aircraft serial numbers 5 to 8 and 10 to 12 inclusive and before 15000 flights for aircraft serial numbers 13 to 24 inclusive.   This AD is effective from 18 August 1994.   Background:   Fatigue tests have shown that the web and fitting at fuselage frame 2 are susceptible to fatigue damage. The existing fittings are therefore replaced with redesigned fittings providing an improved fatigue life.