N467LX
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.
6 reports on file, 2006-02-20 – 2007-09-16.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 1,385 hrs · 1,216 cycles
DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, BOTH THE RT AND LT IB ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. MAINTENANCE REPLACED BOTH RIBS WITH THE UPGRADED ASSEMBLIES.
Part: ANNUNCIATOR — INOPERATIVE (MLG) · airframe 982 hrs · 842 cycles
TRIP NR 1154624 - CREW REPORTED NO GREEN GEAR DOWN AND LOCKED LIGHTS. CREW ACCOMPLISHED EMERGENCY GEAR EXTENSION AND DECLARED EMERGENCY. MAINTENANCE DISCOVERED THE LANDING GEAR INDICATOR CAPSULE INOPERATIVE. THE CAPSULE WAS REPLACED.
Part: VALVE — INOPERATIVE (AFT FUSELAGE) · airframe 279 hrs · 229 cycles
THE CREW REPORTED LOUD CLUNKING SOUNDS WHILE IN CLIMB, CRUISE AND DESCENT. THE CABIN TEMPERATURE WAS REPORTED AS BEING HIGH AND A BURNING PAINT SMELL WAS NOTED WHEN THE WING ANTI-ICE HEAT WAS OPERATING. MAINTENANCE REPLACED THE FLOW INCREASING VALVE. SATISFACTORY OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: HOUSING — LEAKING (LT ENGINE) · airframe 269 hrs · 220 cycles
THE CREW REPORTED A BURNING SMELL IN THE AIRCRAFT WHEN INITIATING HIGH POWER SETTINGS. THE BURNING WOOD SMELL WOULD DISSIPATE AFTER APPROXIMATELY 30 SECONDS. MAINTENANCE FOUND THE NR 4 BEARING HOUSING ON THE LEFT ENGINE LEAKING WHICH WAS CAUSING THE BURNING SMELL AT HIGH POWER SETTINGS. THE NR 4 BEARING HOUSING WAS REPAIRED, THE LEFT OIL PUMP WAS REPLACED AND THE WATER SEPARATOR SOCK WAS CLEANED. NO BURNING SMELLS WERE NOTED WHEN THE ENVIRONMENTAL AND ENGINE SYSTEMS WERE CHECKED WHILE THE AIRCRAFT WAS RUN AT HIGH POWER SETTINGS. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: ODOR — DETECTED (CABIN/COCKPIT) · airframe 262 hrs · 212 cycles
THE CREW REPORTED A BURNING OR HOT WOOD SMELL IN THE CABIN. THE ODOR LASTED FOR 30 SEC TO 1 MINUTE THEN DISSIPATED. MAINTENANCE COMPLIED WITH RAYTHEON CUSTOMER SERVICE LETTER BJ-CSL-1011 WHICH REPLACES THE WRAPPING MATERIAL ON THE WING ANTI-ICE DUCTING AND COCKPIT AND CABIN CONDITIONED AIR DUCTING. SATISFACTORY OPERATIONAL CHECKS WERE PERFORMED, AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: SERVO — INTERMITTENT (RUDDER SERVO)
INVESTIGATED PILOT REPORT OF INTERMITTENT RUDDER BOOST FAILURE ALONG WITH SIMULATANEOUS AUTOPILOT AND YAW DAMPER DISEGAGEMENT. FOUND RUDDER SERVO INTERMITTENTLY FAILING. REPLACED RUDDER SERVO WITH OVERHAULED UNIT, RUDDER BOOST AND AUTOPILOT FUNCTIONAL TESTS SATISFACTORY. (K)