N167H
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
4 reports on file, 2000-03-22 – 2004-08-19.
Part: RELAY — OVERHEATED (BATTERY)
IN FLIGHT CREW AND PASSENGERS SMELLED SMOKE, LANDED AT FIRST AVAILABLE PLATFORM (WC 620) AND AFTER LANDING AIRCRAFT EXPERIENCED TOTAL ELECTRICAL FAILURE. REMOVED AND REPLACED AIRCRAFT BATTERY AND BATTERY RELAY, SET GENERATOR VOLTAGE AND INSPECTED WIRES IN AIRCRAFT NO DEFECTS NOTED. BATTERY RELAY GOT HOT. AIRCRAFT GROUND RAN NO DEFECTS NOTED ALL WORK DONE IAW MM.
Part: BLADE — FLAKING (MAIN ROTOR) · airframe 12,682 hrs
M/R BLADE T/E EXTRUSION EXFOLIATED AT APPROX. STA. 120.00. REMOVED BLADE FROM SERVICE AND INSTALLED A SERVICABLE UNIT.
Part: CLAMP — BROKEN (ENGINE)
DURING LANDING THE PILOT SMELLED A DISTINCT ODOR, UPON LANDING FOUND ONE OF THE EXHAUST STACKS ON THE SIDE OF THE ENGINE COWLING. THE MECHANIC REMOVED AND REPLACED THE BROKEN CLAMP AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: SUPPORT BRACKET — CORRODED (M/R CYCLIC)
DURING THE ANNUAL INSPECTION, THE PIVOT SUPPORT ASSEMBLY WAS FOUND CORRODED. REPLACED SUPPORT ASSEMBLY WITH NEW PART. SUBMITTER RECOMMENDED SPRAYING A CORROSION PREVENTATIVE COMPOUND IN THE AREA OF THE SUPPORT ASSEMBLY. (X)