N414AN
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
3 reports on file, 2001-09-11 – 2008-10-17.
Part: CYLINDER — CRACKED (ENGINE) · airframe 6,220 hrs
UPON INSPECTION FOUND THAT NR 1 AND NR 5 CYLINDERS WERE CRACKED AND LEAKING FUEL ORIGINATING JUST INBOARD OF THE FUEL NOZZLE BETWEEN THE 16TH AND 18TH COOLING FINS. CYLINDERS WERE NEW WHEN INSTALLED AT ENGINE OVERHAUL.
Part: WASHER — SHEARED (ZONE 700) · airframe 5,870 hrs
ON LANDING AIRCRAFT VEERED TO THE RT, INSPECTION SHOWED WASHER PN 5045018-1 HAD SHEARED ALLOWING BOTTOM TORQUE LINK AND WHEEL ASSY TO TURN 180 DEGREES ROTATION. ADDITIONAL ROTATION WAS STOPPED WHEN BRAKE ASSY CONTACTED UPPER TORQUE LINK. CONSIDERING TORQUE LOADING UPON LANDING THE SPECIAL WASHERS PN 5045018-1 NEED TO BE CLOSELY INSPECTED AND CORRECT TOW OUT NEEDS TO BE MAINTAINED. THIS IS CENTER PIVOT TORQUE LINK BOLT WASHER. NOTE: WASHERS IN QUESTION MEASURE .045 - .032.
Part: LINE — CHAFED (BRAKE ASSY)
BRAKE LINE ROUTED UNDER THE CO-PILOTS SEAT PEDESTAL AREA IS CHAFFING ON HEAT DUCT TUBING. SLIDING A 193-6 LOW PRESSURE HOSE OVER THE BRAKE LINE WILL KEEP THE BRAKE LINE FROM DEVELOPING A HOLE.