Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR LY02011F00001Accumulator · crackedDURING FLIGHT, THE ACFT HAD HYD LEAK DUE TO A CRACKING ON THE ACCUMULATOR. THE ACFT RETURNED TO DEPARTURE AND PERFORMED EMERGENCY PROCEDURES WITHOUT ANY PROBLEMS. THE HYD ACCUMULATOR IS AN "ON CONDITION COMPONENT", THE CRACK FOUND IS UNKNOWN. WE ARE INVESTISDR LY02011F00000Packing · leakingACFT DURING ASCENT WITH ALTITUDE OF 6500 FT WAS EVIDENCE THE LOW OIL PRESSURE LIGHT ENG RT "TURN ON", AND THE OIL QTY INDICATOR TO ZERO. CABIN CREW AGREES TO SHUTDOWN THE RT ENGINE IAW THE PROVISIONS OF THE CHECKLIST " ENGINE FAILURE DURING FLIGHT". THE CONTSDR SWIA95752Strut · wornLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. INSPECTION OF AIRCRAFT DETECTED A FAULTY OUTBOARD GEAR SWITCH. REPLACED AND ADJUSTED PER 32-00-00, THE LEFT MAIN LANDING GEAR STRUT WAS IN NEED OF REBUILDING. REPLACED THE STRUT SEALS AND INSPECTED AIRCRAFT LANDSDR SWIA95692Potentiometer · dirtyAFTER TAKEOFF, GEAR HORN SOUNDED UPON RETRACTION. AT THIS POINT, IT WAS NOTICED THAT THE FLAP INDICATOR SHOWED FULL DOWN DEFLECTION, HOWEVER, FLAPS WERE RETRACTED. FLAPS INOP AFTER THIS. SUSPECT LOGIC BOX FAILURE. CLEANED FLAP TRANSMITTER POTENTIOMETER SEASDR SWIA95628Contl Cables · out of adjustDURING PREFLIGHT CONTROL CHECK, FOUND EXCESSIVE PLAY IN CONTROLS, COPILOT WOULD MOVE WHILE CAPT WOULD REMAIN STATIONARY. INSPECTED AILERON CABLES FROM CONTROL COLUMN TO BELL CRANK, FOUND NORMAL. FOUND CABLE TENSION TO BE BELOW, ADJUSTED CABLES TO CORRECT TENSDR SWIA95607Awi Syst · malfunctionedDURING TAKEOFF, AWI WAS TURNED ON, GOT BOTH LIGHTS BUT NO TORQUE RISE ON EITHER ENGINE. OPS CKS AWI SYSTEM ON GROUND, FOUND TO BE OPS NORMALLY AT THIS TIME.