Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR AC2A075817Gearshaft · wornEXCESSIVE SPLINE WEAR ON AFT END. REPLACED WITH NEW.SDR AC2A072789Altimeter · out of toleranceVIBRATOR INOP,AUTOPILOT CORRECTION POTENTIOMETER OUT OF TOLERANCE AND OFF FLAG STICKS. REPLACED INST.SDR AC2A072777Chip Detector · leakingPART LEAKS AT CONNECTOR. REPLACED CHIP DETECTORSDR AC2A0000087Fitting · crackedFOUND SMALL CRACK IN UNDERSIDE OF FITTING. VERIFIED CRACK WITH NDT. REPLACED FITTING. (X)SDR AC2A0000047Angle · crackedT-ANGLE FOUND CRACKED SIX INCHES FORWARD ON PILOTS AFT DOOR POST. REPAIRED PER SRM. (X)SDR AC2A0000043Bearing · bindingINTERMITTENT BINDING IN FLIGHT CONTROL WHEN ROLL INPUT IS APPLIED. REPLACED WORN BEARING. (X)SDR AC2A0000016Scroll · crackedSCROLL CRACKED AT NORMAL LOCATION. REPLACED SCROLL. (X)SDR 99ZZZX4116Potentiometer · failedFEEDBACK POTENTIOMETER PREMATURE FAILURE, SHOULD LAST UNTIL OVERHAUL TIME OF 3,000 HOURS. SUBMITTER STATED CAUSED ACTUATOR TO KICK IN-FLIGHT. COMP P/N 7690001802106.SDR 99ZZZX4202Potentiometer · failedFEEDBACK POTENTIOMETER PREMATURE FAILURE, SUBMITTER STATED SHOULD LAST UNTIL OVERHAUL TIME OF 3,000 HOURS. CAUSES ACTUATOR TO KICK IN-FLIGHT. COMPONENT P/N 769000180210L.SDR 98ZZZX2538Rescue Light · defectiveUPON COMPLETION OF LIFE VEST INSPECTION (12 EACH), EVERY RESCUE LIGHT WITH A MNAUFACTURE DATE OF JUNE, 1997, HAD FAILED DUE TO CASE SWELLING (9 EACH) AFTER ONLY 3 MONTHS IN SERVICE. OTHER LIGHTS WITH DIFFERENT MANUFACTURE DATES DID NOT FAIL DURING THE SAME 3 SDR 97ZZZX3454Blade · crackedBLADE HAS A COMPLETE CHORD-WISE CRACK IN THE NICKEL LEADING EDGE ABRASION STRIP LOCATED 170 INCHES FROM THE ROOT END OF BLADE. THE NICKEL STRIP IS SEPARATED OUTBOARD OF THE CRACK ON LOWER SIDE, 12 INCHES ALONG TRAILING EDGE OF STRIP AND INBOARD OF THE CRACK 2