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EFTA01326217_sub_006 - EFTA01326217_600
) Wire 2SX21A22 and Were 2SX7seso were spliced together new TCAS control pad P2; (e) Wee ISX23A22 had be pmiously removed horn muisponda count pad Palo E and rapped and stowed. and (4 Wire 2SX23A22 had hem previously removed from 52 transponder cord panel Pia E and capped and stowed. Dusan Avant (FAA
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