N192PH
Registered owner: PHI AVIATION LLC, LA (owner ≠ operator)
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
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.
10 reports on file, 2005-08-21 – 2012-08-08.
Part: WIRE HARNESS — DAMAGED (FIRE DETECTION) · airframe 7,863 hrs
NR 2 ENGINE FIRE WARNING LIGHT AND AURAL WARNING CAME ON IN CUISE FLIGHT. LANDING UNEVENTFUL. INSTALLED NEW FLAME DETECTOR AND HARNESS AND COMPLIED WITH SHRINK WRAP MODIFICATION.
Part: FIRE DETECTOR — FALSE ACTIVATION (NR 2 NACELLE) · airframe 7,819 hrs
NR 2 ENGINE INTERMITTENT FIRE WARNING LIGHT WITH AURAL WARNING CAME ON 5 TIMES. LIGHT WENT OUT IMMEDIATELY EACH TIME. MAINTENANCE REPLACED THE NR 2 ENGINE AFT FLAME DETECTOR AND AFT FIRE DETECTION HARNESS, PN 925582-04112-042.
Part: WIRE HARNESS — SHORTED (FIRE DETECTOR) · airframe 6,417 hrs
NR 2 ENGINE FIRE LIGHT CAME ON INTERMITTENTLY, NO SECONDARY INDICATIONS. INSPECTED FIRE DETECTION SYS AND FOUND SHORT IN NR 2 ENG AFT FLAME DETECTOR HARNESS.
Part: FRAME — CRACKED (ENGINE) · airframe 6,097 hrs
FOUND CRACKED FRONT FRAME AT 6 O'CLOCK POSITION INSIDE INLET AREA. OIL LEAKAGE SEEMED TO BE CARRIED THROUGH TO THE PARTICLE SEPARATOR BLOWER AND DEPOSITED ON THE TAILBOOM, RATHER THAN INTO THE COMPRESSOR. SENT ENGINE FOR REPAIR.
Part: COMPRESSOR — FAILED (ACM) · airframe 5,914 hrs
DURING IFR CRUISE FLIGHT, PASSENGERS REPORTED FUMES IN CABIN. DECLARED "EMERGENCY". PROCEEDED TO DESTINATION. LANDED WITHOUT INCIDENT. MX FOUND THE AIR CONDITIONING COMPRESSOR MOTOR TO HAVE FAILED. REPLACED THE COMPRESSOR PALLET ASSY, PN 92309-04851-108, SN 1001.
Part: FIRE WARNING — FALSE ACTIVATION (NR 2) · airframe 5,672 hrs
DURING TAKEOFF THE NR 2 ENGINE FIRE LIGHT ILLUMINATED. ABORTED TAKEOFF AND LANDED ON THE FLYWAY. TAXIED TO THE PARKING AREA AND NOTIFIED MAINTENANCE. CLEANED CONNECTORS AND INSPECTED SYSTEM. FOUND NO DEFECTS. RAN AIRCRAFT, TESTED SYSTEM AND PERFORMED CHECK FLIGHT. ALL CHECKED GOOD. NOTE: PREVIOUSLY SUBMITTED ON 10/15/09.
Part: SPAR CAP — CRACKED (FUSELAGE) · airframe 3,211 hrs
FORWARD SPAR CAP ANGLE AT TOP OF THE DRIVESHAFT TUNNEL IS CRACKED AT TOP OF THE LAST LARGE HL64-8 PIN. CONTACTED MFG FOR 8110 REPAIR.
Part: ANGLE — CRACKED (TAILCONE) · airframe 3,211 hrs
FWD LT CAP ANGLE CRACKED. REPORTED PROBLEM TO MFG.
Part: SEAL — LEAKING (ENGINE OIL) · airframe 1,722 hrs
OIL PRESSURE WAS NORMAL AFTER TAKEOFF, ABOUT 35 MIN IN CRUISE FLIGHT, NR 2 ENGINE OIL PRESSURE HAD DROPPED TO 55 PSI, THEN ON ARRIVAL, NR 2 ENGINE OIL PRESSURE WAS BETWEEN 47 AND 50 PSI. REPLACED G AXIS SEAL.
Part: LINE — RUPTURED (NR 2 HYD SYSTEM) · airframe 646 hrs
NR 2 HYDRAULIC SYSTEM FAILED IN FLIGHT. MAINTENANCE FOUND NR 2 HYDRAULIC PUMP DISCHARGE HOSE HAD RUPTURED. REPLACED HOSE.