N143CF

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

Accident · 2003-09-03 Unresolved
Agusta A109E Minor injuryoperator not yet resolved
Source: NTSB case FTW03FA211

Maintenance disclosures

O · 2013-04-23 Unresolved
ATA 6320

DURING THE ACCOMPLISHMENT OF AN TECHNICAL BULLETIN BT109EP-128 ON A MAIN GEARBOX; A CROWN GEAR, WAS FOUND TO HAVE A CRACK. THE CROWN GEAR WILL BE REPLACED BY A NEW SUPPORT ASSY.

Source: SDR DT1R20130425003 · FAA SDRS
O · 2003-03-26 Unresolved
ATA 5302

A CRACK WAS FOUND IN THE INTERIOR OF THE LEFT SIDE OF THE VERTICAL FIN. THE CRACKS WERE LOCATED ON HORIZONTAL RIBS AT WL 235.2 AT STATION 9725.0 MM. LOWER CRACK IS APPROXIMATELY 4 INCHES LONG. SECOND CRACK IS APPROX. 1.25 INCH LONG. MFG WAS CONTACTED FOR SERVICEABILITY INSTRUCTIONS. A LETTER WAS INSSUED PERMITTING OPERATION FOR 100 HOURS PROVIDED DAILY AND 25 HOUR INSPECTIONS WERE COMPLIED WITH INSTRUCTIONS.

Source: SDR NXT2003F00001 · FAA SDRS
R J · 1999-07-27 Unresolved
ATA 7320

THIS PY AIR LINE CRACKED AND CAUSED SUDDEN DECELERATION. PILOT MADE NORMAL SINGLE ENGINE LANDING WITHIN PUBLISHED OEI LIMITATIONS. VIBRATIONS WERE RECORDED ON MAIN DRIVESHAFT. THE ENGINE ASSY AND MAIN DRIVE SHAFT WERE REPLACED.

Source: SDR 99ZZZX3021 · FAA SDRS
O · 1997-08-22 Unresolved
ATA 7310

TUBE OR WELD CRACKED WHERE TUBE ENTERS FUEL NOZZLE FITTING. THIS IS THE SIXTH OCCURRENCE SINCE MAY, 1997. THREE WERE P/N 4-401-376-01 MANIFOLDS AND 3 WERE P/N 4-301-236-04 MANIFOLDS. THIS IS BEING ADDRESSED BY ALLIED SIGNAL.

Source: SDR 97ZZZX4093 · FAA SDRS
R · 1997-03-05 Matched by certificate designator
ATA 7310

FOUR MINUTES AFTER TAKEOFF, NR 2 ENGINE WENT TO FLT IDLE. A SINGLE ENGINE LANDING WAS INITIATED. MAINTENANCE PERSONNEL FOUND A T-FITTING ON THE PC FILTER HOUSING BROKEN OFF. THE FILTER ASSY WAS REPLACED, THE ENGINE WAS OPERATIONAL CHECKED AND RETURNED TO SERVICE. (M)

Source: SDR 97ZZZM652 · FAA SDRS
M · 1996-06-10 Matched by certificate designator
ATA 6322

DURING FLIGHT, THE PILOT NOTED THE NR 2 ENGINE OIL PRESSURE DROPPING AND THE OIL TEMPRATURE RISING. HE SHUT DOWN THE ENGINE AS A RESULT, AND PERFORMED A SINGLE ENGINE LANDING. WHILE INVESTIGATING THE CAUSE, THE MECHANIC DISCOVERED THE SHAFT OF THE OIL COOLER BLOWER TO HAVE SHEARED NEXT TO THE SPINE ADAPTER. THE IMPELLERS APPEAR TO HAVE SEIZED INSIDE THE HOUSING.

Source: SDR 96ZZZX3843 · FAA SDRS
M · 1996-06-10 Matched by certificate designator
ATA 6322

DURING FLIGHT, PILOT NOTED NR 2 ENGINE OIL PRESSURE DROPPING AND THE OIL TEMPERATURE RISING. HE SHUT DOWN THE ENGINE AS A RESULT AND PERFORMED A SINGLE ENGINE LANDING. WHILE INVESTIGATING THE CAUSE, MECHANIC DISCOVERED THE SHAFT OF THE OIL COOLER BLOWER TO HAVE SHEARED NEXT TO THE SPLINE ADAPTER. THE IMPELLERS APPEAR TO HAVE SEIZED INSIDE THE HOUSING.

Source: SDR 96ZZZX3968 · FAA SDRS