N892PH
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.
4 reports on file, 2007-02-13 – 2018-02-28.
Part: ARM — BROKEN · airframe 5,077 hrs
ENGINE REMOVED 6-2-12 DUE TO BROKEN LEVER ARM. REPLACED LEVER ARM AND RETURNED TO SERVICE.
Part: FIRE DETECTOR — INOPERATIVE (NR 2 NACELLE) · airframe 1,806 hrs
IFR FLIGHT, WHILE LEVEL AT 6000 FT, NR 2 ENGINE FIRE WARNING ACTIVATED. BEFORE EMERGENCY PROCEDURE STARTED, LIGHT AND AUDIO EXTINGUISHED. RETURNED TO DEPARTURE AND NR 2 ENGINE FIRE WARNING ACTIVATED BRIEFLY AGAIN. MX REPLACING RT NR 2 FIRE DETECTOR AND HARNESS.
Part: DETECTOR — MALFUNCTIONED (NR 2) · airframe 333 hrs
NR 2 ENGINE FIRE LIGHT ILLUMINATED FOR APPROX 2 SECONDS DURING IFR CLIMBOUT FIVE MINUTES AFTER TAKEOFF. REPLACED FLAME DETECTOR AND ALSO REPLACED HARNESS 92552-04112-041.
Part: CONTROL PANEL — FAILED (MLG)
UPON APPROACH TO GC902 DURING BEFORE LANDING CHECK, GEAR WOULD NOT EXTEND. RETURNED TO HUM AND USED EMERGENCY BLOW DOWN. TROUBLESHOOTING REVEALED CONTACTS BETWEEN PINS A AND B OF LANDING GEAR CONTROL PANEL MAINTAINING CONTINUITY WHEN GEAR LEVER IS PLACED IN THE DOWN POSITION. THEREFORE POWER IS CONTINUALLY SUPPLIED TO THE RETRACT SIDE OF THE CONTROL VLAVE.