N584E

Cancelled 2011

Deregistered aircraft · 1952 Convair 340 · Allison 501 series

Cancelled
March 14, 2011
Exported to
Mexico
Status when cancelled
Triennial form not returned
Serial number
24
Year built
1952
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, transport
Airworthiness date
May 20, 2000
Certificate issued
May 29, 2002
Last registry action
May 20, 2008
Mode S code
A78528
Owner when cancelled
Air Tahoma Inc
Location
Spanaway, WA
Owner type
Corporation

From the FAA registry file of October 29, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

Service difficulty reports · 13

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 15HA0858011AOil Cooler · leakingWHILE IN FLIGHT, THE CREW OBSERVED THE OIL QUANTITY ON THE RT ENGINE DECREASING. AS THE OIL QUANTITY CONTINUED TO DECREASE, THE CREW ELECTED TO SHUT DOWN THE ENGINE AS A PRECAUTIONARY MEASURE. THE CREW DIVERTED TO ST MARTIN SMX AND MADE AN UNEVENTFUL LANDINGOct 15, 2008 · N584E · Cvac 340CVAC · Engine Oil CoolerSDR I5H2008F00003Oil Cooler · leakingWHILE IN FLIGHT, THE CREW OBSERVED THE OIL QUANTITY ON THE RT ENGINE DECREASING. AS THE OIL QUANTITY CONTINUED TO DECREASE, THE CREW ELECTED TO SHUTDOWN THE ENGINE AS A PRECAUTIONARY MEASURE. THE CREW MADE AN UNEVENTFUL LANDING. MAINTENANCE INSP REVEALED A LAug 15, 2008 · N584E · Cvac 340CVAC · Engine Oil CoolerSDR I5HA0658016Skin · damagedON APPROACH, THE CREW FELT A VIBRATION AND A SEVERE PULL TO THE LT. THEY DECLARED AND EMERGENCY. AFTER LANDING AND GOING TO THE PARKING SPOT, THE CREW DETERMINED THAT THEY HAD A BIRD STRIKE ON THE LT IB WING (LEADING EDGE). MAINTENANCE WAS CALLED AND THEY MAFeb 7, 2007 · N584E · Cvac 340CVAC · Leading Edge DevicesSDR 15HA0758001Amplifier · damagedON TAKEOFF ROLL THE RT ENGINE FAILED TO MAKE TAKEOFF POWER. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO BLOCKS. MAINTENANCE FOUND THAT THE TEMPERATURE DATUM (TD) FUEL CONTROL SYSTEM HAD DRIVEN TO THE FULL (TAKE) POSITION RESULTING IN LOW POWER DURING THJan 10, 2007 · N584E · Cvac 340CVAC · Fuel Control/Turbine EnginesSDR I5HA0658012O-Ring · damagedAFTER TAKEOFF, THE CREW OBSERVED FLUCTUATING REDUCTION GEARBOX OIL PRESSURE ON THE LT ENGINE WITH A CORRESPONDING LOSS OF OIL QUANTITY. THE CREW PERFORMED AND ENGINE SHUTDOWN AND RETURNED, WHERE THEY LANDED UNEVENTFULLY. MAINTENANCE DETERMINED THAT AN O-RINGDec 12, 2006 · N584E · Cvac 340CVAC · Turbine Engine Oil SystemSDR I5HA058003Clamp · looseWHILE IN ROUTE, THE CREW OBSERVED RT OIL QUANTITY LOW LIGHT ILLUMINATED WITH NO SECONDARY INDICATIONS. AT THE SAME TIME THE ZONE 1 FIRE WARNING SOUNDED ON THE SAME ENGINE. THECREW PERFORMED AN EMERGENCY ENGINE SHUTDOWN AND RETURNED TO DEPARTURE. INSPECTION Jan 30, 2006 · N584E · Cvac 340CVAC · Engine Indicating System WiringSDR I5HA058009Engine · shutdownWHILE ENROUTE, THE CREW OBSERVED THE LT OIL QUANTITY GO TO ZERO. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN AND DIVERTED. INSPECTION REVEALED OIL LEAKING FROM THE STRATER O`RING. THE O`RING WAS REMOVED AND REPLACED AND THE AIRCRAFT RETURNED TO SERVINov 25, 2005 · N584E · Cvac 340CVAC · Engine (Turbine/Turboprop)SDR I5HA0558005Engine · failedWHILE ENROUTE, THE PILOT NOTICED A SIGNIFICANT DROP IN HORSEPOWER ON THE LT ENGINE. THE PILOT PERFORMED EMERGENCY SHUTDOWN OF THE LT ENGINE USING THE (E) HANDLE. AC LANDED UNEVENTFULLY AND TAXIED TO FACILITY. INSP OF LT ENGINE REVEALED A CATASTROPHIC FAILURSep 3, 2005 · N584E · Cvac 340CVAC · Engine (Turbine/Turboprop)SDR I5HA0558004Generator · failedWHILE ON TRAINING FLIGHT, RT AC GENERATOR (MECHANICAL FAIL) LIGHT ILLUMINATED. THE CAPTAIN PERFORMED AN IN-FLIGHT PRECAUTIONARY SHUTDOWN OF THE RT ENGINE IAW PROCEDURES IN THE EMERGENCY PROCEDURES CHECKLIST. THE AIRCRAFT RETURNED TO BASE AND MADE AN UNEVENTFJun 8, 2005 · N584E · Cvac 340CVAC · AC Generator-AlternatorSDR I5HA03580009Bushing · backed outENROUTE, CREW OBSERVED LANDING GEAR (UNSAFE LIGHT) REMAINED ON AFTER LANDING GEAR WAS RAISED AND AFTER HYDRAULIC BYPASS HANDLE WAS PUT IN (BYPASS) POSITION. MECHANICS WERE UNABLE TO DUPLICATE THIS DISCREPANCY WITH AC ON JACKS BUT DETERMINED THAT NLG ACTUATOR Dec 9, 2004 · N584E · Cvac 340CVAC · Landing Gear Position and WarningSDR I5HA0358AAARelay · inoperativeAFTER TAKEOFF FROM PIT EN ROUTE TO CVG, THE CREW WAS UNABLE TO RAISE THE LANDING GEAR HANDLE DUE TO THE 'UNLOCK SOLENOID' NOT RETRACTING. THE AIRCRAFT RETURNED TO PIT WHERE IT LANDED SAFELY. THE AIRCRAFT WAS FERRIED TO THE AIR TAHOMA, INC MAINTENANCE BASE INMar 25, 2004 · N584E · Cvac 340CVAC · Landing Gear Retraction/Extension SystemSDR 15HA0358008Engine · malfunctionedDURING THE DESCENT INTO MEM, THE PILOT OBSERVED THE 'LOW OIL PRESSLURE' LIGHT ILLUMINATE FOR THE LT ENGINE AND AN ASSOCIATED LOSS OF OIL QUANTITY TO ZERO GALLONS. THE CREW PERFORMED AN INFLIGHT EMERGENCY SHUTDOWN USING THE 'E' HANDLE. THE AIRCRAFT MADE AN UNJan 7, 2004 · N584E · Cvac 340CVAC · Engine (Turbine/Turboprop)SDR 15HA0358001Brake · inoperativeA/C TRANSITIONED FROM THE RUNWAY TO THE TAXIWAY, CREW WAS INFORMED THAT THE LT LANDING GEAR APPEARED TO BE ON FIRE. TAXIED A/C TO A SAFE AREA. FIRE TRUCK WAS DISPATCHED, BUT NO FIRE WAS OBSERVED. MAINT CREW FOUND THE PRESSURE LINE TO NR 1 BRAKE, VERY LOOSEFeb 16, 2003 · N584E · Cvac 340CVAC · Landing Gear Brake System