N212CE
Registered owner: CAL ENTERPRISES LLC, MT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Jet Linx Aviation, LLC (9JLA) | 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.
5 reports on file, 2015-02-18 – 2021-11-02.
Part: SOLENOID — FAILED · airframe 4,632 hrs · 2,997 cycles
THE MAINTENANCE TEAM FOUND THAT THE LEFT THRUST REVIEWER INTERMITTENTLY WILL NOT ALLOW THRUST LEVER TO ADVANCE ENGINE POWER AFTER THRUST REVERSER IS DEPLOYED. TROUBLESHOOTING FOUND LEFT THRUST REVERSER INTERLOCK SOLENOID NOT ACTIVATING . REMOVED THRUST REVERSER INTERLOCK SOLENOID AND INSTALLED NEW UNIT. OPS CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: TORQUE MOTOR — INOPERATIVE (RT ENGINE) · airframe 4,418 hrs · 2,850 cycles
THE FLIGHT CREW REPORTED OF AN INTERMITTENT RIGHT ELECTRONIC ENGINE CONTROL ANNUNCIATOR WHILE IN FLIGHT. THE FLIGHT CREW RAN THE APPROPRIATE CHECKLIST. LANDING WAS UNEVENTFUL. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THE TORQUE MOTOR WAS INOP. P/N 30J3491-01 S/N TR6337CPWAZ129. A NEW TOQUE MOTOR WAS INSTALLED. OPS CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 3,159 hrs · 1,966 cycles
FLIGHT CREW REPORTED THAT THE RIGHT HAND FORWARD FACING WINDSHIELD OUTER PANEL CRACKED DURING FLIGHT. THE WINDSHIELD WAS REPLACED WITH A NEW UNIT AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: BUTTON — DISENGAGED (FLIGHT DIRECTOR) · airframe 3,146 hrs · 1,958 cycles
SHORTLY AFTER T/O FOR A REPOSITION FLT FROM SDL TO LAS, EXPERIENCED A FAULT WITH THE FLT DIR CONTROLLER IN THE VERTICAL MODE ON BOTH PILOTS A COPILOTS CONTROLLERS. CREW REPORTED, WERE UNABLE TO ENGAGE EITHER V/S OR F/C MODES ON EITHER SIDE. CREW INDICATED THE CHECKLIST DID NOT ADDRESS THE V/S, F/C AUTOPILOT FAULT. IT WAS DECIDED TO RETURN TO THE DEPARTURE AIRPORT FOR CORRECTIVE ACTIONS. NORMAL LANDING WAS ACCOMPLISHED. T/S FOUND THAT THE VS PUSHBUTTON ON THE COPILOTâS MODE SELECTOR WAS NOT PROPERLY ENGAGED. THE PUSHBUTTON WAS RESET AND FUNCTIONAL CHECKS OF THE BUTTON WERE FOUND TO BE SATISFACTORY. AC WAS RETURNED TO SERVICE. THE LAMPS FOR THE VS PUSHBUTTON ON THE COPILOTS AP MODE SELECTOR PANEL WERE REPLACED DURING A RECENT OUTSOURCED MX/INSP VISIT PRIOR TO THIS FLIGHT. MX VENDOR HAS BEEN MADE AWARE OF THEIR LAPSE IN QUALITY CONTROL.
Part: ADAPTER — BROKEN (APU) · airframe 2,727 hrs · 1,682 cycles
THE FLIGHT CREW REPORTED THAT THE APU FAILED TO START AFTER LANDING, INDICATING A FAULT ON THE CONTROL PANEL. TROUBLESHOOTING IDENTIFIED THAT THE STARTER GEN DRIVE ADAPTER PN 3861055-1 FAILED. THE BROKEN DRIVE ADAPTER WAS REMOVED & A NEW ADAPTER INSTALLED.