AD/A320/75 - Longitudinal Floor Beams at Frame 43
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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Airbus Industrie A319, A320 and A321 Series Aeroplanes
AD/A320/75 Longitudinal Floor Beams at Frame 43 2/97
Applicability: Airbus A320, all models, all serial numbers, without Airbus Industrie Modification 20904 or Airbus Industrie Service Bulletin (SB) A320-53-1008 incorporated.
Requirement: Inspect the bottom flanges of the longitudinal floor beams at frame 43 in accordance with Airbus Industrie SB A320-53-1085.
Note: French DGAC AD 96-236-089(B) refers.
Compliance: Inspect before exceeding 20 000 flights. Re-inspect at intervals not exceeding 6000 flights or, if cracks are detected, re-inspect at the intervals defined in Airbus Industrie SB A320-53-1085.
Note: Modification of the aircraft in accordance with Airbus Industrie SB A320-53-1008 is terminating action for this Directive.
This Airworthiness Directive becomes effective on 30 January 1997.
Background: During the full-scale fatigue test of the airframe, cracks were detected in the bottom flange of the longitudinal floor beams, which attach the pressure diaphragm at frame
- This directive is issued to detect cracks in this area before the structural integrity of the airframe is affected.