N330MX
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.
10 reports on file, 1996-12-27 – 2012-11-02.
Part: SKIN PANEL — CRACKED (RT WING) · airframe 19,856 hrs · 23,786 cycles
RIGHT LEADING EDGE OUTBOARD (WING RT) LEAKING FUEL. A CRACK IN THE LOWER WING PANEL HAS BEEN FOUND WITH AN APPROX LENGTH OF 30 MM, LOCATED INBOARD RIB 12 AT THE RUN-OUT OF STRINGER 14. REPAIRED CRACK IN RIGHT LEADING EDGE OUTBOARD IAW 328-100-SPR A000104718 AND RAS-328-57-4489. NOTE: WING TOTAL TIME AND TOTAL CYCLES ARE THE SAME AS AIRCRAFT TOTAL TIME AND TOTAL CYCLES.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 16,956 hrs · 20,189 cycles
LT REAR EMERGENCY EXTERNAL EXIT LIGHT INOP.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 16,747 hrs · 19,883 cycles
LEFT SIDE EXTERNAL EMERGENCY LIGHTS DO NOT WORK (BOTH EXTERNAL LIGHTS ON THE LEFT SIDE).
Part: DAU — MALFUNCTIONED (E/E BAY)
ENGINE MISCOMPARE MESSAGE ON TAKEOFF WITH NO OBVIOUS ENGINE PROBLEMS. ABORTED TAKEOFF. MAINTENANCE RERACKED DAU NR 1 AND NR 2, CREW PERFORMED ENGINE RUN UP. OPS CHECK GOOD, NO MESSAGE NOTED. (M)
Part: SMOKE — DETECTED (CABIN)
LAVATORY SMOKE CAS MESSAGE, VISIBLE SMOKE, RETURNED TO GATE. MAINTENANCE RAN ENGINES WITH PAX ON FOR 15 MINUTES, NO SMOKE NOTED. (M)
Part: WIPER — MALFUNCTIONED (WINDSHIELD)
CAPTAIN PULLED OUT ON RUNWAY, TURNED OFF WIPER AND WIPER WOULD NOT PARK. CAPTAIN TURNED OFF RUNWAY AND RETURNED TO GATE. C/W OPERATIONAL TEST IAW DO-328 ITC 30-41-02. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X)
Part: TEMP SENSOR — DEFECTIVE (RT ENGINE)
EN ROUTE, THE FLIGHT CREW NOTICED THE OIL TEMPERATURE INDICATION FOR THE RIGHT ENGINE WAS VERY ERRATIC. CREW CONTACTED MAINTENANCE CONTROL AND WERE ADVISED TO DIVERT TO COS WHERE REPAIRS COULD BE MADE. AIRCRAFT LANDED IN COS WITHOUT FURTHER INCIDENT. COS MX REPLACED THE RT ENGINE OIL TEMPERATURE SENSOR IAW AMM 79-32-01, ENGINE GROUND RUNS WERE SATISFACTORY.
Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT)
EN ROUTE, CREW ENCOUNTERED A PROBLEM WITH THE AUTO PRESSURIZATION CONTROL SYSTEM. CREW ELECTED TO RETURN TO COS. MX INSPECTED AIRCRAFT UPON ARRIVAL IN COS. MX THEN DEFERRED AUTO PRESSURIZATION FUNCTION PER MEL 21-9-1. ON 28 JUNE, 1997 MX CLEARED MEL DEFERRAL BY REPLACING THE CABIN PRESSURIZATION CONTROL PANEL IAW AMM 21-30-00.
Part: UPLOCK — LACK OF LUBE (MLG)
FLT NR 3003 - A/C RETURNED TO FIELD WHEN CREW WAS ALERTED TO AN UNSAFE GEAR CONDITION, BOTH LT AND RT MLG. A/C LANDED COS WITHOUT FURTHER INCIDENT. COS MAINTENANCE CLEANED AND LUBRICATED BOTH LT AND RT MLG UPLOCK ROLLER ASSEMBLIES AND RELEASED AIRCRAFT FOR A FUNCTION TEST FLIGHT. RESULTS OF FUNCTION TEST FLIGHT WERE UNSATISFACTORY. AIRCRAFT WAS RETURNED TO MAX HANGAR WHERE ICE ACCUMULATION WAS ALLOWED TO THAW. ROLLERS WERE CLEANED AND LUBRICATED. GROUND OPERATIONAL CHECK OF THE LANDING GEAR WAS CONDUCTED WITH SATISFACTORY RESULTS. (M)
Part: FLOW CNTRL VALVE — DEFECTIVE (LT ENGINE)
FLT 3005 - AIRCRAFT RETURNED FROM FLIGHT WHEN CREW WAS ALERTED TO LT ENGINE INLET DEICE FAILURE INDICATION. AIRCRAFT LANDED COS WITHOUT FURTHER INCIDENT. COS - MX REPLACED LT ENGINE INLET EJECTOR FLOW CONTROL VALVE IAW AMM 30-22-03. GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X)