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| | Airbus Model A300 B4-600, B4-600R, and F4-600R |
 | | The actions specified by this AD are intended to prevent failure of the vertical stabilizer-to-fuselage attachment fittings or transverse (side) load fittings, or rudder-to-vertical stabilizer attachment fittings, which could result in loss of the vertical stabilizer and/or rudder and consequent loss of control of the airplane. |
 | | Note 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. |
 | | For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (e) of this AD. |
| www.airweb.faa.gov /Regulatory_and_Guidance_Library/rgAD.nsf/0/4B0F74B7DF3ACED086256B19005571D5?OpenDocument (2269 words) |
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