N752WJ
Registered owner: CX 34 LLC, FL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Charter Airlines, LLC (AJXA) | Certificate holder | — | Matched by certificate designator |
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.
7 reports on file, 2020-01-09 – 2024-01-12.
Part: PROXIMITY SENSOR — OUT OF TOLERANCE (ZONE 800) · airframe 14,924 hrs · 8,498 cycles
AFTER TAKEOFF PILOT REPORTED THAT THEY RECEIVED 3 WARNINGS. 1. CABIN DOOR OPEN, 2. CABIN VENT DOOR OPEN AND A CABIN ALTITUDE WARNING. AFTER TROUBLESHOOTING FOUND THAT THE DOOR PROXIMITY SWITCH FAILED. THE SWITCH CONTROLS THE VENT DOOR WARNING AND THE CABIN DOOR WARNING INDICATIONS. FOUND CABIN VENT DOOR SEAL LOOSE CAUSING CABIN ALTITUDE NOT TO RISE
Part: PRESSURE SWITCH — FAILED (ZONE 400) · airframe 14,922 hrs · 8,496 cycles
HYDRAULIC SYSTEM A FAILED ON WHILE DESCENDING ON APPROACH TO KOPF
Part: OVERHEAT SENSOR — INTERMITTENT (TAILCONE) · airframe 14,247 hrs · 8,208 cycles
DURING TAKEOFF PILOT RECEIVED A TAIL CONE BLEED LEAK INDICATION. HE REPORTED THAT THE INDICATION WAS INTERMITTENT. WE REMOVED AND REPLACED A FAILING RTD SENSOR, PERFORMED FUNCTIONAL CHECK WITH NO FURTHER DEFECTS
Part: TRIM SYSTEM — MALFUNCTIONED · airframe 14,247 hrs · 8,208 cycles
ON TAKEOFF THE PILOT REPORTED THAT THEY HAD A PRIMARY TRIM FAILURE AND A MACH TRIM OFF INDICATION. THE PRIMARY TRIM FAILURE WAS DUE TO THE FACT THAT THE PILOT IN COMMAND DID NOT TURN ON THE MACH TRIM. WE PERFORMED A FUNCTIONAL CHECK OF THE SYSTEM AND FOUND THAT SYSTEM HAD NO FAULTS.
Part: PUMP — LOW PRESSURE (ZONE 400) · airframe 14,156 hrs · 8,169 cycles
DURING CRUISE THE PILOT RECEIEVED A CAS MESSAGE NOTING A FUEL IMBALANCE BETWEEN THE LH AND RH WING. THE FUEL FLOW FROM THE RIGHT HAND TRANSFER SYSTEM WAS NOT KEEPING UP WITH THE FUEL FLOW FROM THE LH FUEL TRANSFER SYSTEM INDICATING LOW PRESSURE FROM THE MOTIVE FLOW FROM THE RIGHT HAND ENGINE DRIVEN FUEL PUMP. THE RIGHT HAND ENGINE DRIVEN FUEL PUMP WAS REPLACED WITH A OVERHAULED UNIT AND THIS RESOLVED THE ISSUE WITH THE FUEL IMBALANCE. THE PLANE WAS RETURNED TO SERVICE AND COMPLETED SEVERAL FLIGHTS WITH NO FURTHER ISSUES.
Part: YAW DAMPER — NONE (ZONE 300) · airframe 13,911 hrs · 8,067 cycles
DURING TAKOFF THE LOWER YAW DAMPER B AMBER CAS ILLUMINATED AND THE PILOT ABORTED TAKEOFF AND RETURNED TO THE FBO AT KOPF. MECHANICS WERE SENT TO THE PLANE AND PERFORMED A CHECK OF THE YAW DAMPER SYSTEM AND WERE UNABLE TO DUPLICATE THE FAULT. PILOT ALSO REPORTED NOSEWHEEL SHIMMY DURING TAKEOFF ROLL. MECHANICS REMOVED AND REPLACED BOTH NOSE WHEEL TIRE ASSEMBLIES. AIRCRAFT HAS BEEN RETURNED TO SERVICE
Part: STRUT — LOW PRESSURE (NLG) · airframe 12,610 hrs · 9,535 cycles
DURING DEPARTURE, THE CREW WAS UNABLE TO RETRACT THE LANDING GEAR AFTER TAKEOFF. THE AIRCRAFT RETURNED SAFELY TO TETERBORO AIRPORT TO INVESTIGATE THE PROBLEM. THE AIRCRAFT WAS PUT INTO MAINTENANCE AND IT WAS FOUND THAT THE PRESSURE OF THE NOSE GEAR STRUT WAS TOO LOW. THE NOSE GEAR WAS SERVICED AND GEAR SWINGS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED BACK TO SERVICE.