N660JM

No registry detail on file · not in current registry

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

O · 2019-01-17 Matched by certificate designator
ATA 3260

THE AIRCRAFT WAS ON A MAINTENANCE CHECK FLIGHT DUE TO AN ENGINE CHANGE. AFTER TAKEOFF, THE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED, MAINTENANCE JACKED THE AIRCRAFT, PULLED UP THE FIM AND FOUND THE NOSE GEAR SAFETY PROX SWITCH TARGET LOOSE AND NOT ACTUATING THE PROX SWITCH. THE TARGET WAS SECURED, THE GEAR SWING WAS NORMAL AND THE AIRCRAFT TOOK OFF AND COMPLETED ITS MCF WITH NO FURTHER DIFFICULTIES.

Source: SDR 7SJA2019F00115 · FAA SDRS
B · 2018-05-21 Unresolved
ATA 3300

FLIGHT ATTENDANT REPORTED ELECTRICAL BURNING ODOR IN CABIN. FLIGHT CREW CONFIRMED NO SMOKE WAS PRESENT IN CABIN. LANDED AND WAS INSPECTED ON GROUND BY THE FIRE DEPARTMENT FOR EVIDENCE OF SMOKE OR BURNING. NONE DETECTED, MAINTENANCE SURVEYED AIRCRAFT AT BASE, FOUND THE NR 4 UP WASH LIGHT INVERTER TO BE FAILED, AND HAVE STRONG ELECTRICAL BURNING ODOR.

Source: SDR 201805220000160 · FAA SDRS
O · 2017-01-09 Matched by certificate designator
ATA 2133

JANUARY 9, AIRCRAFT WAS IN TEB AND UPON TAXI OUT, CREW FELT A PRESSURE BUMP AND REPORTED AN ASSOCIATED CAS MESSAGE OF PRESS AUTO FAIL. AIRCRAFT RETURNED TO THE FBO. A TECHNICIAN WAS DISPATCHED AND PERFORMED TROUBLESHOOTING PER FIM. NO FAULTS FOUND AND MESSAGE WAS NOT IN VIEW. PER THE FIM IT STATES THAT IT WAS TRANSITORY CONDITION. A/C WAS RELEASED. A/C TOOK OFF, CLIMBED TO FL 380 AND WAS THERE FOR 20 MINUTES AND CABIN PRESSURE BECAME UNCONTROLLABLE. A/C DESCENDED TO FL 100 AND DIVERTED TO MDW. IN MDW THE OUTFLOW VALVES WERE LOCKED OUT AND WE INSTALLED MEL 21-30-00C. JANUARY 10, THE A/C WAS DISPATCHED TO CLE WHERE QUALIFIED MAINTENANCE IS BUT DUE TO RUNWAY ICE, THE AIRCRAFT DIVERTED TO CMH. AN AOG TEAM FROM CLE WAS DISPATCHED TO CMH. THE TECHNICIAN DOWNLOADED THE CMC AND SENT TO TECH SUPPORT AND STARTED FOLLOWING THE FIM FOR THE STATED ISSUE. REPORTED THAT NO ASSOCIATED MESSAGES WERE LOCKED INTO THE CMC SYSTEM. TROUBLESHOOTING SHOWED 1 STEP TO BE OUT OF TOLERANCE REGARDING DELTA P WHEN AIRCRAFT CONFIGURED ON GROUND. IT WAS RECOMMENDED TO CHANGE THE ELECTROMECHANICAL OUTFLOW VALVE AND PRESSURE CONTROLLER. ABOVE PARTS ORDERED, RECEIVED, INSTALLED. PRESSURIZATION SYSTEM FUNCTIONAL CHECK PERFORMED. SYSTEM FUNCTIONAL CHECKS GOOD. JANUARY 12, THE AIRCRAFT WAS DISPATCHED CMH-TEB TO POSITION FOR A REVENUE FLIGHT. IN ROUTE AND AT FL 390 FOR 20 MINUTES, CABIN PRESSURE STARTED CLIMBING. CREW DESCENDED TO FL 100 AND DIVERTED TO CLE. CLE MAINTENANCE TEAM DOWNLOADED CMC AND SENT TO TECH SUPPORT, NO FAULTS NOTED. RAN SUGGESTED FIM AND FOUND PNEUMATIC OUTFLOW VALVE FAILED THE TIME TO CLOSE TEST. ORDERED AND INSTALL OF OUTFLOW VALVE AND PERFORMED GROUND FUNCTIONAL CHECKS GOOD. WE PERFORMED A LOCAL MAINTENANCE FUNCTIONAL CHECK FLIGHT AND THE AIRCRAFT AND PRESSURIZATION SYSTEM OPERATED NORMALLY.

Source: SDR 2017FA0000014 · FAA SDRS