N581P1952 Convair 340-31
This N-number isn't registered right now. Below is its last known registration, canceled Sep 10, 2024.
Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply16 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 21, 2026- Last registered owner
- Air Tahoma INC
- Owner type
- Corporation
- City, state
- Groveport, OH
- Certificate issued
- Dec 16, 2022
- Canceled
- Sep 10, 2024
- Airworthiness
- Standard · Transport
- Airworthiness date
- Feb 20, 1995
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
- 340-31
- Year
- 1952
- Serial number
- 29
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 46
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- A77AE4
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- 2022 – 2024Air Tahoma INCGroveport, OH
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 (16)
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.
- Propellers · o-ring · leakingDec 19, 2008
DURING THE TAKEOFF ROLL DEPARTING, ENROUTE, THE NR ONE ENG AUTO-FEATHERED. THE CREW ABORTED THE TAKEOFF AND RETURNED TO BASE. MX PERSONNEL OBSERVED A LARGE AMOUNT OF OIL AROUND THE FRONT OF THE PROPELLER. FURTHER INSP REVEALED A FAILED O’RING BENEATH THE FEATHER RESERVOIR CAUSING A MASSIVE OIL…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · channel · damagedJul 17, 2008
DURING A STORM ON APRIL 6, 2008 A CARGO CAN (ULB) WAS THROWN INTO THE RT SIDE OF ACFT. THE RT PROPELLER WAS ALSO STRUCK A GLANCING BLOW. THERE WAS SIGNIFICANT DAMAGE TO THE SKIN AND SUPPORT STRUCTURE BENEATH THE SKIN. THERE WAS DAMAGE TO WIRING IN THE AREA. THE NOSE STEERING ACTUATOR WAS ALSO…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · channel · damagedJul 17, 2008
DURING A STORM A CARGO CAN (ULB) WAS THROWN INTO THE RT SIDE OF ACFT. THE RT PROPELLER WAS ALSO STRUCK A GLANCING BLOW. THERE WAS SIGNIFICANT DAMAGE TO THE SKIN AND SUPPORT STRUCTURE BENEATH THE SKIN. THERE WAS DAMAGE TO WIRING IN THE AREA. THE NOSE STEERING ACTUATOR WAS ALSO DAMAGED. DAMAGE AREA…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Landing gear · actuator · damagedApr 5, 2008
DURING A STORM, ON APR 6,2008, A CARGO CAN (ULB) WAS THROWN INTO THE RT SIDE. THE RT PROP WAS ALSO STRUCK A GLANCING BLOW. THERE WAS SIGNIFICANT DAMAGE TO THE SKIN AND SUPPORT STRUCTURE BENEATH THE SKIN. THERE WAS DAMAGE TO WIRING IN THE AREA. THE NOSE STEERING ACTUATOR WAS ALSO DAMAGED. DAMAGE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · actuator · damagedApr 5, 2008
DURING A STORM IN MIA ON APRIL 6, 2008 A CARGO CAN (ULB) WAS THROWN INTO THE RT SIDE OF N581P. THE RT PROPELLER WAS ALSO STRUCK A GLANCING BLOW. THERE WAS SIGNIFICANT DAMAGE TO THE SKIN AND SUPPORT STRUCTURE BENEATH THE SKIN. THERE WAS DAMAGE TO WIRING IN THE AREA. THE NOSE STEERING ACTUATOR WAS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Structures (general) · angle · damagedApr 5, 2008
DURING A STORM (MIA) A CARGO CAN (ULB) WAS THROWN INTO THE RT SIDE OF N581P. THE RT PROPELLER WAS ALSO STRUCK A GLANCING BLOW. THERE WAS SIGNIFICANT DAMAGE TO THE SKIN AND SUPPORT STRUCTURE BENEATH THE SKIN. THERE WAS DAMAGE TO WIRING IN THE AREA. THE NOSE STEERING ACTUATOR WAS ALSO DAMAGED.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Structures (general) · angle · damagedApr 5, 2008
DURING A STORM (MIA) A CARGO CAN (ULB) WAS THROWN INTO THE RT SIDE OF N581P. THE RT PROPELLER WAS ALSO STRUCK A GLANCING BLOW. THERE WAS SIGNIFICANT DAMAGE TO THE SKIN AND SUPPORT STRUCTURE BENEATH THE SKIN. THERE WAS DAMAGE TO WIRING IN THE AREA. THE NOSE STEERING ACTUATOR WAS ALSO DAMAGED.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Structures (general) · angle · damagedApr 5, 2008
DURING A STORM (MIA) A CARGO CAN (ULB) WAS THROWN INTO THE RT SIDE OF N581P. THE RT PROPELLER WAS ALSO STRUCK A GLANCING BLOW. THERE WAS SIGNIFICANT DAMAGE TO THE SKIN AND SUPPORT STRUCTURE BENEATH THE SKIN. THERE WAS DAMAGE TO WIRING IN THE AREA. THE NOSE STEERING ACTUATOR WAS ALSO DAMAGED.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Structures (general) · channel · damagedApr 5, 2008
DURING A STORM (MIA) A CARGO CAN (ULB) WAS THROWN INTO THE RT SIDE OF N581P. THE RT PROPELLER WAS ALSO STRUCK A GLANCING BLOW. THERE WAS SIGNIFICANT DAMAGE TO THE SKIN AND SUPPORT STRUCTURE BENEATH THE SKIN. THERE WAS DAMAGE TO WIRING IN THE AREA. THE NOSE STEERING ACTUATOR WAS ALSO DAMAGED.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine fuel and control · relay · failedJan 15, 2007
ON TAKEOFF ROLL, RT ENGINE TURBINE INLET TEMPERATURE (TIT) REACHED 880 DEGREES AND BEGAN TO DETERIORATE. CREW NOTED A LOUD BANG (COMPRESSOR STALL) AND THE ENGINE SPOOLED DOWN. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO BASE. SUBSEQUENT ATTEMPT TO RESTART THE ENGINE FAILED. THE ENGINE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 16 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 21, 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