Document ID: chunk:federal_register_of_legislation:F2006B01935:body:0
Version: federal_register_of_legislation:F2006B01935
Segment Type: other
Provision Reference: 
Character Range: 0–1051

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/A320/45 Fuselage - Fasteners at Skin Panel to Frame 13 and 14 Joint

 Applicability: A320 series aircraft MSN 005 to 030 inclusive.

5/95

            Requirement: Perform an external detailed visual inspection for missing or broken rivet heads at fuselage frames 13 and 14 on the left and right hand sides between stringers 1 and 7. Inspect in accordance with Airbus Industrie SB A320-53-1036.

            Note: DGAC AD 92-199-028(B) refers.

            Compliance: Inspect before 10000 flights or before 27 May 1995, whichever is the later. Repeat inspections at intervals not exceeding 6000 flights.

            Modification in accordance with Airbus Industrie SB A320-53-1010 cancels the requirement of this AD.

 Background: A number of damaged or missing rivet heads were found on the fatigue test article.