NTSB investigations · 1
Matched to this aircraft by N376J and the event date: up to this one’s cancellation.
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N376J and the event date: up to this one’s cancellation.
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2000ZZZX61Stack · mismanufacturedTHIS NEW FAA-PMA PART WAS NOT FORMED PROPERLY AND COULD NOT BE INSTALLED WITHOUT CAUSING UNDUE STRESS ON MATING PARTS. THE PART WAS TAGGED AND RETURNED TO DISTRIBUTOR AND ANOTHER NEW PART ORDERED FOR THE AIRCRAFT. (THE ANGLE OF THE BEND IN THE PIPE WAS NOT COSDR 2000ZZZX60Slip Joint · crackedPART WAS FOUND CRACKED 330 DEGREES AROUND WELD AND WAS VISIBLE BY OPENING THE OUTBOARD COWLING DOOR.SDR 2000ZZZX59Stack · misinstalledCOUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK. AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQUENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT. THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATERIAL AND IS LOCATED SDR 2000ZZZX58Stack · misinstalledCOUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK. AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQUENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT. THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATERIAL AND IS LOCATED SDR 2000ZZZX57Header · damagedCOUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK. AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQUENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT. THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATERIAL AND IS LOCATED USDR 2000ZZZX56Stack · damagedCOUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK. AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQUENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT. THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATERIAL AND IS LOCATED SDR 2000ZZZX55Engine Beam · corrodedENGINE BEAM FOUND SEVERELY CORRODED FROM EXPOSURE TO HOT EXHAUST GASSES DUE TO LEAKING EXHAUST PIPE FLANGES AND CLAMPS. OTHER DAMAGE FOUND INVOLVED THE FIREWALL ACCESS PANEL WHICH COVERS THE FUEL CROSSFEED LINE IN WHICH MOSTLY ALL OF THE ATTACHING SCREW HEADSSDR 2000ZZZX54Header · damagedCOUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK. AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQUENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT. THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATERIAL, AND IS LOCATED