Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 4DSR20141102Duct · crackedDURING SCHEDULED INSPECTION FOUND THE INLET ANTI-ICE HOT AIR DISTRIBUTION DUCT CRACKED FORWARD WHERE THE BLEED AIR TAP IS WELDED INTO THE DUCT. THIS AREA IS DIFFICULT TO DETECT AND REQUIRES CAREFUL EXAMINATION. ON THIS ACFT THE LEAK HAD BLOWN BACK SOME OF THESDR 2005FA0001354Drive Assy · stiffTHE PILOT REPORTED THAT THE CONTROLS WERE STIFF IN THE ROLL AXIS. THE AUTOPILOT WAS TURNED OFF AND THE CB WAS CYCLED WITH NO CHANGE IN THE CONDITION. AFTER LANDING, WITHOUT INCIDENT, TECHNICIANS ARRIVED AND TROUBLESHOOT THE A/P SYSTEM. THEY DISCOVERED THE ASDR 2005FA0001129Drive Assy · inoperativeTHE PILOT REPORTED THAT THE CONTROLS WHERE STIFF IN THE ROLL AXIS. THE AUTOPILOT WAS TURNED OFF AND THE C/B WAS CYCLED WITH NO CHANGE IN THE CONDITION. AFTER LANDING WITHOUT INCIDENT, TECHS ARRIVED AND TROUBLESHOT THE A/P SYSTEM. THEY DISCOVERED THE AILERONSDR B3OR20010007Harness · deterioratedDUR HI-PWR ENG RUN, NOTICED LT ENG ITT AT 690 DEG. ITT CLIMBED, REDUCED PWR IN ORDER NOT TO EXCEED 700 DEG RED LINE OF ITT. A 5 PT PERFORMANCE RUN PERF AT P&W REQUEST. ITT AT 695 DEG. CHECKED T1 HARNESS & T6 THERMOCOUPLES. RESISTANCE OF BOTH OF THE HARNESSDR B3OR200000008Skin · damagedINSPECTED THIS AC FOR LING LEADING EDGE SKIN CONTACT DAMAGE FROM HEATED LEADING EDGE RETAINING SCREWS DUE TO CONTACT DAMAGE BEING FOUND IN SISTER SHIP. DAMAGE WAS FOUND TO WING LEADING EDGE UNDER HEATED LEADING EDGE ASSY EVEN THOUGH PROPER SCREWS WERE USED .