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EFTA00620791_sub_002 - EFTA00620791_164
i MM REF M HRS 993052 EASA AD2010.0076 - BR700-710 Effectivity: All BR700- Engines High-Pressure (HP) Turbine 710C4.11 with Discs Stage 1 and 2 Assembly Life hardware Limits - Modification configurations as implied on the AD and equipped with HP Turbine Dics listed in Table 1 or Table 2 of the AD!!
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