N193BH
Registered owner: BLACK MOUNTAIN AVIATION LLC, NV (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Hawaii Helicopters, LLC (I2WA) | Certificate holder | — | Matched by certificate designator |
| Helicopter Consultants of Maui, LLC. (HCMA) | 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.
8 reports on file, 1996-08-16 – 2006-04-26.
Part: CONNECTOR — DIRTY (OIL PRES IND SYS)
AC MADE PRECAUTIONARY LANDING OFF AIRPORT DUE TO LOSS OF OIL PRESSURE INDICATION. LANDING WAS UNEVENTFUL. NO INJURIES, NO AIRCRAFT OR PROPERTY DAMAGE. MAINT DETERMINED THAT THE OIL PRESSURE TRANSMITTER HAD A POOR ELECTRICAL CONNECTION. CONNECTOR WAS CLEANED AND REINSTALLED. OIL PRESSURE INDICATING SYS WAS CHECKED BY GROUND RUNNING ENGINE. GROUND RUN CHECKS PROVED GOOD. AIRCRAFT RETURNED TO MAINTENANCE BASE EMPTY AND RETURNED TO SERVICE. NORMAL LIGHT ENVIRONMENTAL CORROSION ON ELECTRICAL PIN CONTACT POINTS. REMOVED AND REPLACED CONNECTOR ITSELF, REESTABLISHED A GOOD ELECTRICAL CONNECTION PATHWAY. PLUG WAS REMOVED AND REPLACED SEVERAL TIMES TO ASSURE POSITIVE CONNECTION POINTS. (K)
Part: WIRE HARNESS — INTERMITTENT (CHIP DETECTOR)
PILOT EXPERIENCED AN ENGINE CHIP LIGHT INDICATION. HE CHOSE TO MAKE LANDING. UPON INVESTIGATION BY THE MECHANIC, A SMALL SILVER OF METAL WAS FOUND. THE PLUG WAS CLEANED. THE SYSTEM WAS FLUSHED AND THE OIL FILTER WAS INSPECTED WITH NO EVIDENCE OF METAL AND REPLACED. FOLLOWING GROUND RUN AFTER MAINTENANCE PRESENTED AN ADDITIONAL ENGINE CHIP LIGHT INDICATION WITH NO EVIDENCE OF METAL. ENGINE CHIP PLUG WIRING HARNESS WAS REPLACED. THE AIRCRAFT WAS GROUND RUN AND FLIGHT CHECKED WITH NO FURTHER INCIDENCE. (K)
Part: ROD — WORN (PITCH CONTROL) · airframe 8,358 hrs
PART IS WORN BEYOND LIMITS.
Part: BEARING — WORN (PITCH ROD)
PITCH CONTROL WORN BEYOND LIMITS. TIME ON PART IS UNKNOWN.
Part: ROD — WORN (PITCH CONTROL) · airframe 5,031 hrs
PART IS WORN BEYOND LIMITS. TIME ON PARTS IS UNKNOWN. PLEASE OVERHAUL PC LINKS.
Part: HINGE LAMINATE — CRACKED (TAIL ROTOR)
RUBBER IS CRACKED BEYOND LIMITS. (X)
Part: HINGE — DELAMINATED (TAIL ROTOR)
RUBBER IS TORN BEYOND LIMITS AND THERE IS NO J-GAP. (X)
Part: GYRO — DEFECTIVE (COCKPIT DG)
INOP. SEE JUDY SMITH FOR REPLACEMENT PART DATA.