# N585P: 1954 Convair 340/580, registration cancelled 2020-10-31

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 31, 2020
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Convair 340/580](https://openairdocs.org/model/convair-340-580) (registry code 3790228)
- Engine: [Allison 501-D13 series](https://openairdocs.org/engine/allison-501-d13-series) (registry code 03004)
- Data sheets: [TCDS E-282](https://openairdocs.org/tcds/E-282) (OpenAirDocs)
- Serial number: 163
- Year built: 1954
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: July 31, 2003
- Certificate issued: June 10, 2003
- Last registry action: July 20, 2017
- Mode S code: A789C0
- 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/N585P
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=585P
- Page: https://openairdocs.org/deregistered/N585P-2020-10-31

From the FAA registry file of October 31, 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 340/580: https://openairdocs.org/model/convair-340-580.md

## Service difficulty reports (6)

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

- [SDR I5HA041108001](https://openairdocs.org/sdr/I5HA041108001), Apr 11, 2008: VOLT REGULATOR. OUT OF ADJUST. AFTER CLIMB OUT, THE CREW LOST THE NR1 DC GENERATOR. AS A PRECAUTIONARY MEASURE THEY RETURNED TO DEPARTURE FOR MAINT TO CORRECT THE PROBLEM. MAINT RERACKED THE 
- [SDR I5HA0758012](https://openairdocs.org/sdr/I5HA0758012), Sep 12, 2007: PUMP. CRACKED. DURING DEPARTURE, ENROUTE, THE CREW LOST HYDRAULIC PRESSURE AND RETURNED TO DEPARTURE. THE AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWED TO A PARKING SPACE. MAINTE
- [SDR I5HA058005](https://openairdocs.org/sdr/I5HA058005), Jul 13, 2006: REGULATOR. FLUCTUATES. DURING TAKEOFF ROLL, CREW OBSERVED WHAT THEY BELIEVED TO BE A LOSS OF POWER FROM THE LT ENGINE. TAKEOFF WAS ABORTED AND AC RETURNED FOR MAINT. AFTER PERFORMING 
- [SDR I5HA058004](https://openairdocs.org/sdr/I5HA058004), Apr 19, 2006: UPLOCK. OUT OF RIG. CREW OBSERVED LANDING GEAR UNSAFE LIGHT AND FELT THE NOSE LANDING GEAR EXTEND DURING THE CLIMB OUT, AFTER THE HYDRAULIC BYPASS WAS SELECTED TO BYPASS. CREW SHIF
- [SDR I5HA0558002](https://openairdocs.org/sdr/I5HA0558002), Mar 6, 2005: TIE. CRACKED. DURING A ROUTINE INSP, A CRACK WAS DISCOVERED AT THE POWER SECTION END ON THE IB TIE STRUT ON THE RT ENGINE. CRACK WAS LOCATED IN THE WELD AREA ON THE END CLOSE
- [SDR 15HA03580005](https://openairdocs.org/sdr/15HA03580005), Sep 18, 2003: LEVER. CRACKED. AFTER TAKEOFF FROM PIT, EN ROUTE TO MIDDLETOWN, THE PILOT OBSERVED A LANDING GEAR 'UNSAFE' LIGHT AFTER GEAR RETRACTION. THE PILOT LOWERED THE GEAR AND PROCEEDED

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