# N584E: 1952 Convair 340, registration cancelled 2011-03-14

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 14, 2011
- Exported to: Mexico
- Status when cancelled: Triennial form not returned
- Airframe: [Convair 340](https://openairdocs.org/model/convair-340) (registry code 242270A)
- Engine: [Allison 501 series](https://openairdocs.org/engine/allison-501-series) (registry code 03000)
- Data sheets: [TCDS 6A6](https://openairdocs.org/tcds/6A6), [TCDS E-282](https://openairdocs.org/tcds/E-282) (OpenAirDocs)
- Serial number: 24
- Year built: 1952
- Type of aircraft: Fixed wing multi engine
- Engine type: 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](https://openairdocs.org/faa-owner/AIR%20TAHOMA%20INC)
- Location: [Spanaway, WA](https://openairdocs.org/faa-place/WA/Spanaway)
- Owner type: Corporation
- Owner's area on the map: 47.0609° N, 122.3889° W: Placed by OpenAirDocs at the center of ZIP code 98387, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N584E
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=584E
- Page: https://openairdocs.org/deregistered/N584E-2011-03-14

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.

ADs and bulletins for the Convair 340: https://openairdocs.org/model/convair-340.md

## Service difficulty reports (13)

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

- [SDR 15HA0858011A](https://openairdocs.org/sdr/15HA0858011A), Oct 15, 2008: OIL COOLER. LEAKING. WHILE 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 EN
- [SDR I5H2008F00003](https://openairdocs.org/sdr/I5H2008F00003), Aug 15, 2008: OIL COOLER. LEAKING. WHILE 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 ENG
- [SDR I5HA0658016](https://openairdocs.org/sdr/I5HA0658016), Feb 7, 2007: SKIN. DAMAGED. ON 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 DETERMINE
- [SDR 15HA0758001](https://openairdocs.org/sdr/15HA0758001), Jan 10, 2007: AMPLIFIER. DAMAGED. ON TAKEOFF ROLL THE RT ENGINE FAILED TO MAKE TAKEOFF POWER. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO BLOCKS. MAINTENANCE FOUND THAT THE TEMPERATURE DATU
- [SDR I5HA0658012](https://openairdocs.org/sdr/I5HA0658012), Dec 12, 2006: O-RING. DAMAGED. AFTER TAKEOFF, THE CREW OBSERVED FLUCTUATING REDUCTION GEARBOX OIL PRESSURE ON THE LT ENGINE WITH A CORRESPONDING LOSS OF OIL QUANTITY. THE CREW PERFORMED AND E
- [SDR I5HA058003](https://openairdocs.org/sdr/I5HA058003), Jan 30, 2006: CLAMP. LOOSE. WHILE 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 S
- [SDR I5HA058009](https://openairdocs.org/sdr/I5HA058009), Nov 25, 2005: ENGINE. SHUTDOWN. WHILE ENROUTE, THE CREW OBSERVED THE LT OIL QUANTITY GO TO ZERO. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN AND DIVERTED. INSPECTION REVEALED OIL LEAKIN
- [SDR I5HA0558005](https://openairdocs.org/sdr/I5HA0558005), Sep 3, 2005: ENGINE. FAILED. WHILE 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
- [SDR I5HA0558004](https://openairdocs.org/sdr/I5HA0558004), Jun 8, 2005: GENERATOR. FAILED. WHILE ON TRAINING FLIGHT, RT AC GENERATOR (MECHANICAL FAIL) LIGHT ILLUMINATED. THE CAPTAIN PERFORMED AN IN-FLIGHT PRECAUTIONARY SHUTDOWN OF THE RT ENGINE IAW PR
- [SDR I5HA03580009](https://openairdocs.org/sdr/I5HA03580009), Dec 9, 2004: BUSHING. BACKED OUT. ENROUTE, CREW OBSERVED LANDING GEAR (UNSAFE LIGHT) REMAINED ON AFTER LANDING GEAR WAS RAISED AND AFTER HYDRAULIC BYPASS HANDLE WAS PUT IN (BYPASS) POSITION. MEC
- [SDR I5HA0358AAA](https://openairdocs.org/sdr/I5HA0358AAA), Mar 25, 2004: RELAY. INOPERATIVE. AFTER 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 
- [SDR 15HA0358008](https://openairdocs.org/sdr/15HA0358008), Jan 7, 2004: ENGINE. MALFUNCTIONED. DURING 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 GALLON
- [SDR 15HA0358001](https://openairdocs.org/sdr/15HA0358001), Feb 16, 2003: BRAKE. INOPERATIVE. A/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 DI

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