CTHRepealedLegislation
AD/A320/172 - Main Landing Gear Support Rib 5
Airbus Industrie A319, A320 and A321 SerAirbus Industrie A319, A320 and A321 Series Aeroplanes
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Airbus Industrie A319, A320 and A321 Series Aeroplanes
| AD/A320/172 | Main Landing Gear Support Rib 5 | 6/2005 |
|---|
| Applicability: | All Model A319, A320, and A321 aircraft; except aircraft with Airbus Modification 32025 incorporated in production, or Airbus Service Bulletin A320-57-1118 incorporated in service. |
|---|---|
| Requirement: | Action in accordance with the requirements of DGAC AD F-2005-035.Note: Airbus Alert Service Bulletin A320-57A1136, or a later EASA approved revision, refers. |
| Compliance: | As specified in the Requirement document, with a revised effective date of 9 June 2005. |
| This Airworthiness Directive becomes effective on 9 June 2005. | |
| Background: | A report was received of a crack in the forward lug of the right hand main landing gear support rib 5. Such cracking could affect the structural integrity of the main landing gear. |
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David Villiers
Delegate of the Civil Aviation Safety Authority
26 April 2005