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AD/A320/214 - Rear Fuselage Structure Reinforcement
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AD/A320/214 - Rear Fuselage Structure Reinforcement
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| AD/A320/214 | Rear Fuselage Structure Reinforcement | 6/2008 |
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| Applicability: | All Model A321 aircraft, without AIRBUS modification 25791 incorporated in production or AIRBUS Service Bulletin A320-53-1130 incorporated in service. |
|---|---|
| Requirement: | Action in accordance with DGAC AD F-1999-051-125(B).Note: AIRBUS Service Bulletin A320-53-1130 original issue, or later DGAC/EASA approved revision, refers. |
| Compliance: | Unless already accomplished, before 5 July 2008. |
| This Airworthiness Directive becomes effective on 5 June 2008. | |
| Background: | The rear fuselage structure requires reinforcement between frames 62 and 64, in order to increase the strength margin in the case of undetected tail scrape of the rear of the fuselage with the ground. |
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David Villiers
Delegate of the Civil Aviation Safety Authority
16 April 2008