N958CP
Registered owner: JOSLYN LARRY J, NV (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Airwork LLC | Operator | on 2008-02-29 | Operator named in NTSB report |
| Silver State Helicopters LLC | Operator | on 2005-05-19 | Operator named in NTSB report |
Accident & incident history
Operated by Silver State Helicopters (per NTSB report)
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.
1 report on file, 2011-03-18.
Part: TAIL ROTOR — DAMAGED · airframe 5,534 hrs
ODOR OF BURNING LUBRICANT, EXCESSIVE VIBRATION, FORCED A SUCCESSFUL OFF AIRPORT LANDING. FOUND AFT "H" FRAME BEARING, PN 269A5050-56, SEIZED, OVERHEATED, DRIVESHAFT JAMMED FWD AGAINST BEARING, AFT BEARING SUPPORT BROKEN OFF FRAME, PN 269A5573-13, AND MISSING. THAT SEGMENT OF THE FRAME WAS NOT RECOVERED. TAIL ROTOR DRIVE COMPONENTS WHERE REMOVED AND DISASSEMBLED. FOUND NUT, PN 269A6029, HAD BACKED OUT OF TAIL ROTOR TRANSMISSION INPUT GEAR, PN 369A5425-3, AND HAD EXERTED FORCE AGAINST THE TAIL ROTOR DRIVESHAFT, PN 269A6040-7, REAR PLUG FORCING THE ENTIRE DRIVESHAFT ASSEMBLY FWD WITH SUFFICIENT FORCE TO PRESS THE DRIVESHAFT ATTACHING HARDWARE AGAINST THE AFT BEARING AND APPARENTLY LOCK THE BEARING INNER AND OUTER RACES TOGETHER. THE RESULTANT HEAT DESTROYED THE FRAME ASSY. THE DRIVESHAFT WAS BENT WELL BEYOND LIMITS. ALL OF THE FWD DRIVESHAFT ATTACHING COMPONENTS HAD EXCESSIVE HEAT DAMAGE AND REQUIRE REPLACEMENT. THE TAIL ROTOR TRANSMISSION HAS NOT BEEN INSPECTED AT THIS POINT, BUT IT IS POSSIBLE THAT THE NUT COMING LOOSE WOULD UNLOAD THE THRUST PROVISION OF THE TRANSMISSION FWD BEARING AND THE REARWARD FORCE GENERATED BY THE NUT LOOSENING AND ACTING AS A PRESS (EQUAL FORCE WOULD BE EXERTED FWD AND AFT) COULD HAVE CAUSED INTERNAL TRANSMISSION DAMAGE. SPECIFIC CAUSE OF FAILURE HAS NOT YET BEEN DETERMINED.