N818PH
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.
17 reports on file, 1996-06-20 – 1998-10-03.
Part: OIL COOLER — CRACKED (RT ENGINE)
GNV - FLT 5069 - RIGHT ENGINE OIL PRESSURE BELOW 55 PSI FEATHERED PROP AND OIL PRESSURE HELD AT 40 PSI 10 MIN LATER IT FELL TO 30 PSI INFLIGHT SHUTDOWN OF RIGHT ENGINE. INFLIGHT EMERGENCY DECLARED. AIRCRAFT LANDED NO INCIDENTS. FOUND ENGINE OIL COOLER LEAKING. REPLACED OIL COOLER IAW DHC-8 MM ATA 72-10. OPERATIONAL LEAK CHECKED OK. (M)
Part: SELECTOR VALVE — MALFUNCTION (COCKPIT)
LEFT LANDING GEAR AMBER LIGHT ILLUMINATED, EXTENDED GEAR AND THE LEFT RED MAIN GEAR LIGHT ILLUMINATED. VISUAL INSPECTION NOTED THE LEFT MAIN GEAR FORWARD DOOR FULLY OPEN, AND THE REMAINING LEFT GEAR DOORS OPEN PARTLY. REPLACED THE MAIN LANDING GEAR SELECTOR VALVE, OPERATIONAL CHECKS GOOD.
Part: AUTOFEATHER SYST — FAILED TEST (E/E COMPT)
EUG- AUTOFEATHER WILL NOT TEST PROPERLY. CYCLED POWER LEVERS AND PERFORMED AUTOFEATHER TEST AGAIN. TESTED GOOD, AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Earlier reports · 1996–1997 · 14 reports
1997
Part: SELECTOR VALVE — MALFUNCTION (RT MLG WW)
ON APPROACH, LANDING GEAR WOULD NOT COME DOWN USING THE GEAR HANDLE. USED ALTERNATE LANDING GEAR EXTENSION METHOD 1, NORMAL EXTENSION WAS TRIED SEVERAL TIMES, BUT GEAR HANDLE WAS INEFFECTIVE. INSPECTED AIRCRAFT AND FOUND SAFE FOR FERRY FLIGHT FROM GEG TO PDX. IN PDX, REPLACED RESISTOR AT TERMINAL BLOCK 7 BETWEEN 8C AND 9G, AND REPLACED LANDING GEAR SELECTOR VALVE. OPERATIONAL AND FUNCTIONAL CHECK OF GEAR IS GOOD.
Part: PLUG — INSTALLED (NR 1 ENGINE)
NR 1 ENGINE TORQUE DROPPED FROM 90 PERCENT TO 60 PERCENT AT 600 FT AGL ON CLIMBOUT FROM PUW. FUEL FLOW DROPPED TO 620 PPH, THE NH RPM'S WERE MATCHED. MANUAL SELECTOR CYCLED WITH NO EFFECT. NO CAUTION LIGHTS AND THE OIL PRESSURE WAS NORMAL. INFLIGHT ENGINE SHUTDOWN ACCOMPLISHED. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER PROBLEM. ENGINE INTAKE PLUG FOUND IN THE INTAKE. THE REMAINDER OF THE INTAKE PLUG WAS REMOVED. HP AND LP BORESCOPE PERFORMED. FOUND IN LP COMPRESSOR REQUIRING ENGINE REPLACEMENT WITHIN 10 FLIGHT HOURS. ENGINE GROUND RUN PERFORMED. ALL ENGINE INDICATIONS WERE WITHIN MAINTENANCE MANUAL REQUIREMENTS.
1996
Part: WIRE — BROKEN (NR 2 SMOKE DET)
CARGO SMOKE WARNING LIGHT ILLUMINATED DURING CLIMB. LIGHT REMAINED ON FOR 5 SECONDS THEN WENT OUT. LIGHT ILLUMINATED AGAIN THEN WENT OUT. AIRCRAFT RETURNED TO SEA AND LANDED WITHOUT FURTHER PROBLEMS. NO SIGNS OF SMOKE OR HEAT NOTED. BROKEN WIRE AT NUMBER TWO SMOKE DETECTOR. CANNON PLUG REPAIRED, NUMBER ONE SMOKE DETECTOR REPLACED AS A PRECAUTIONARY MEASURE, UNIT WAS SLOW TO TEST. SYSTEM OPS CHECKED GOOD.
Part: SEAT TRACK — CORROSION (CABIN)
SEAT TRACK (P/N 85330507-107) FOUND CORRODED BEYOND LIMITS. CORROSION NOTED DURING C-CHECK (NR200-83). TRACK REPLACED IAW SRM 51-40-00.
Part: SEAT TRACK — CORROSION (CABIN)
SEAT TRACK (P/N 85331040-109) FOUND CORRODED BEYOND LIMITS. CORROSION NOTED DURING C-CHECK (NR200-90). TRACK REPLACED IAW SRM 51-40-11.
Part: SEAT TRACK — CORROSION (CABIN)
SEAT TRACK (P/N 85320701-125) FOUND CORRODED BEYOND LIMITS. CORROSION NOTED DURING C-CHECK (NR200-84). TRACK REPLACED IAW SRM 51-40-00.
Part: SEAT TRACK — CORROSION (CABIN)
SEAT TRACK (P/N 85320490-135) FOUND CORRODED BEYOND LIMITS. CORROSION NOTED DURING C-CHECK (NR200-85,133-23). TRACK REPLACED IAW SRM 51-40-11.
Part: SEAT TRACK — CORROSION (CABIN)
SEAT TRACK (P/N 85320490-133) FOUND CORRODED BEYOND LIMITS. CORROSION NOTED DURING C-CHECK (NR200-88). TRACK REPLACED IAW SRM 51-40-00.
Part: SEAT TRACK — CORROSION (CABIN)
SEAT TRACK (P/N 85330164-119) FOUND CORRODED BEYOND LIMITS. CORROSION FOUND DURING C-CHECK (NR200-87). TRACK REPLACED IAW SRM 51-40-11.
Part: SEAT TRACK — CORROSION (CABIN)
SEAT TRACK (P/N 85320701-123) FOUND CORRODED BEYOND LIMITS. CORROSION NOTED DURING C-CHECK (NR200-80-82). TRACK REPLACED IAW SRM 51-40-00.
Part: SEAT TRACK — CORROSION (CABIN)
SEAT TRACK (P/N 85330164-117) FOUND CORRODED BEYOND LIMITS. CORROSION NOTED DURING C-CHECK (NR200-86). TRACK REPLACED IAW SRM 51-40-11.
Part: SEAT TRACK — CORROSION (CABIN)
SEAT TRACK (P/N 85330507-104) FOUND CORRODED BEYOND LIMITS. CORROSION NOTED DURING C-CHECK (NR200-81). TRACK REPLACED I/A/W SRM 51-40-11.
Part: CONTORL BOX — INOPERATIVE (CABIN)
EMERGENCY LIGHTS WILL NOT RESET. EMERGENCY LIGHT CONTROL BOX REPLACED AND LIGHTS OPS CHECKED GOOD.
Part: CONTROL BOX — MALFUNCTIONED (CABIN)
UNABLE TO RESET EMERGENCY LIGHTING. EMERGENCY LIGHTING CONTROL BOX REPLACED AND EMERGENCY LIGHTS OPS CHECKED GOOD.