Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6D20210909001Frame · chafedAS350 S/N 7102 WAS FOUND TO HAVE RH X-FRAME CHAFING DAMAGE. THE DAMAGE IS WITHIN THE REPAIRABLE LIMITS OF REF /A/, BUT THE P/N 350A21-1058-20 DOUBLER NOTED IN THE AMM WAS NOT AVAILABLE IN TIME TO MEET RTS REQUIREMENTS. EA 33-5300-EA-3656 PROVIDES AUTHORIZATIONSDR 2A6D20210824004Deck Plate · damagedDAMAGE WAS NOTED TO THE ENGINE DECK (PN: 350A21-1239.21) IN THE FORM OF A CHAFE AND DENT.THE DAMAGE AREAS WERE DISCOVERED TO BE NEAR THE SCUPPER DRAIN HOLE WITH THE FIRST CHAFE MEASURING APPROXIMATELY 0.50” WIDE AND 0.020” DEEP AT THE DEEPEST POINT, AND THE SESDR 2A6D20210824002Structure · corrodedCORROSION WAS NOTED ON THE RH SIDE OF THE CABIN FLOOR EDGE.SDR 2A6D20210824001Skin · damagedDAMAGE WAS NOTED TO THE TAIL BOOM UPPER SKIN PANEL (PN: 350A23-0020.21) AS WELL AS THE YAW COMPENSATOR CHANNEL REINFORCEMENT (PN: 355A23-2000.20) IN THE FORM OF CHAFE DAMAGE. THE CHAFE DAMAGE TO THE TAIL BOOM UPPER SKIN WAS MEASURED TO BE 1.70” X 0.40” AND 0.0SDR 2A6D20210824003Crossbeam · crackedDAMAGE WAS NOTED TO THE X1790 CROSS BEAM (PN: 350A21-1368.20) IN THE FORM OF A CRACK. THE CRACK WAS MEASURED TO BE APPROXIMATELY 2.0” LONG. THERE WAS ALSO DAMAGE TO THE AFT BULKHEAD WEB (PN: 350A21-1036.22) IN THE FORM OF NUMEROUS CHAFES. THE CHAFES WERE MEASU