N585P1954 Convair 340/580
This N-number isn't registered right now. Below is its last known registration, canceled Oct 31, 2020.
Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply6 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Air Tahoma INC
- Owner type
- Corporation
- City, state
- Spanaway, WA
- Certificate issued
- Jun 10, 2003
- Canceled
- Oct 31, 2020
- Airworthiness
- Standard · Transport
- Airworthiness date
- Jul 31, 2003
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Convair
- Model
- 340/580
- Year
- 1954
- Serial number
- 163
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 46
- Engines
- 2
- Max takeoff weight
- 12,500 - 19,999 lb
- Mode S code
- A789C0
Engine
- Make and model
- Allison 501-D13 Ser
- Type
- Turbo-prop
- Power
- 3750 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2003 – 2020Air Tahoma INCSpanaway, WA
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
ADs published since 1998 that may apply (1)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2006-25-12 | Rolls-Royce Corporation 501-D Series Turboprop Engines | Jan 23, 2007 | Engine (501-D13 SER) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (6)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Electrical power · volt regulator · out of adjustApr 11, 2008
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 NR1 DC GEN CONTROL PANEL AND PARALLEL THE DC GENERATORS IAW THE MM. THE AC WAS RETURNED TO SERVICE AND RETURNED WITHOUT FURTHER PROBLEMS.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · pump · crackedSep 12, 2007
DURING DEPARTURE, ENROUTE, THE CREW LOST HYDRAULIC PRESSURE AND RETURNED TO DEPARTURE. THE AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWED TO A PARKING SPACE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE ENGINE DRIVEN HYDRAULIC PUMP HAD FAILED AND PUMPED ALL THE HYDRAULIC FLUID OVERBOARD.…
From FAA Service Difficulty Reports; matched by N-number. - Propellers · regulator · fluctuatesJul 13, 2006
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 INSP FOR FOD, WATER IN THE FUEL FILTERS, BLEED AIR LEAKS AND A HIGH POWER PENALTY RUN, THE AC WAS RETURNED TO SERVICE WITH GOOD POWER. AC…
From FAA Service Difficulty Reports; matched by N-number.
Show all 6 reportsShow fewer reports
- Landing gear · uplock · out of rigApr 19, 2006
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 SHIFTED THE HYDRAULIC BYPASS HANDLE BACK TO THE PRESSURE POSITION AD THE LANDING GEAR CAME UP AND LOCKED AND REMAINED SO, FOR THE REST OF THE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Power plant · tie · crackedMar 6, 2005
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 CLOSEST TO THE POWER SECTION. A THROUGH INSPECTION WAS DONE ON THE REST OF THE ENGINE FOR EVIDENCE OF OTHER CRACKS. NONE WERE FOUND AND THERE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · lever · crackedSep 18, 2003
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, GEAR DOWN, TO THE COLUMBUS MAINTENANCE FACILITY. THE LANDING GEAR 'UNSAFE' LIGHT WAS EXTINGUISHED WITH THE GEAR DOWN. DURING AN…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026