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AD 95-NM-216-R1 March 12, 1997
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REDUCED STRUCTURAL INTEGRITY OF THE FUSELAGE AND RESTRICTED OPERATION OF THE MAIN LANDING GEAR (MLG) FREE-FALL SYSTEM\AIRBUS INDUSTRIE\A320-111\A320-200\A320-211\A320-212\A320-214\A320-231\A320-232\A3 20-233
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