N581P, cancelled Sep 10, 2024

Service difficulty reports · 17

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

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N581P' AND deregistration_id = 'N581P-2024-09-10'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 15HA0858014O-Ring · leakingDURING 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 FEDec 19, 2008 · N581P · Cvac 580 · Propeller Feathering/ReversingSDR I5HA0858005GChannel · damagedDURING 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 AJul 17, 2008 · N581P · Cvac 34031 · Fuselage Miscellaneous StructureSDR I5HA0858005FChannel · damagedDURING 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. THJul 17, 2008 · N581P · Cvac 34031 · Fuselage Miscellaneous StructureSDR I5HA0858005EChannel · damagedDURING 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 NOSEApr 5, 2008 · N581P · Cvac 580 · Standard Practices/StructuresSDR I5HA0858005DAngle · damagedDURING 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 NOSEApr 5, 2008 · N581P · Cvac 580 · Standard Practices/StructuresSDR I5HA0858005CAngle · damagedDURING 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 NOSEApr 5, 2008 · N581P · Cvac 580 · Standard Practices/StructuresSDR I5HA0858005AAngle · damagedDURING 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 NOSEApr 5, 2008 · N581P · Cvac 580 · Standard Practices/StructuresSDR I5HA0858005Actuator · damagedDURING 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 TApr 5, 2008 · N581P · Cvac 580 · Landing Gear Steering SystemSDR I5H2008F00000Actuator · damagedDURING 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 STEEApr 5, 2008 · N581P · Cvac 34031 · Landing Gear Steering SystemSDR I5HA0758003Relay · failedON 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 Jan 15, 2007 · N581P · Cvac 580 · Fuel Controlling SystemSDR 15HA0658011Structure · damagedON NOVEMBER 8, 2006 WHILE EN-ROUTE, THE CREW OBSERVED A BIRD PASS CLOSE BY THE RT FUSELAGE. THE CREW NOTICED NO ABNORMAL FLIGHT CHARACTERISTICS OR ENGINE INDICATIONS AND ELECTED TO CONTINUE, WHERE THEY LANDED UNEVENTFULLY. MAINTENANCE PERSONNEL INSPECTED THENov 8, 2006 · N581P · Cvac 580 · Leading Edge DevicesSDR I5HA0258001Wing · gougedA BAGGAGE CART DISCONNECTED FROM ITS TOW VEHICLE AND IMPACTED THE AIRCRAFT IN THE AREA OF THE LOWER LT WING LEAVING GOUGES AT WING STATIONS 51.5 AND 52.5 RANGING FROM .078 TO .380 WIDE AND .016 TO .038 DEEP. THE DAMAGE WAS ACCESSED. THE DAMAGED AREA DOES NOTJan 18, 2006 · N581P · Cvac 34031 · Wing, Plate/SkinSDR I5HA0258010Access Panel · crackedDURING A RECENT SCHEDULED INSPECTION, A FUEL LEAK WAS DISCOVERED ON THE LOWER RT WING NEAR THE IB FUEL TANK ACCESS PANEL. A CRACK LOCATED AT WS 8. A NEW ACCESS PANEL DOUBLER WAS INSTALLED IAW DWG. THE AIRCRAFT WAS RETURNED TO SERVICE. (K)Oct 30, 2005 · N581P · Cvac 580 · Wing, Plate/SkinSDR I5HA0558008Arm · brokenENROUTE, CREW OBSERVED A (LANDING GEAR UNSAFE UP) INDICATION ON THE ANNUNCIATOR PANEL. THE LANDING GEAR WAS PLACED DOWN WITH ALL 3 LANDING GEAR INDICATING DOWN AND LOCKED. AC LANDED SAFELY. INSP OF RT LANDING GEAR BY THE OB MECHANIC REVEALED A BROKEN MLG AROct 1, 2005 · N581P · Cvac 34031 · Landing Gear Retraction/Extension SystemSDR I5HA0258007Tire · departedMFD - DURING PILOT TRAINING, AIRPORT MX CREWS NOTICED ONE OF THE TIRES MISSING OFF THE AIRCRAFT AS IT TAXIED BY WHILE ON THE TAXI-WAY. THE MX CREW NOTIFIED THE TOWER WHO IN TURN NOTIFIED CRW. THE AIRCRAFT TAXIED TO THE TARMAC AREA AND SHUTDOWN. THE MX AND IJun 24, 2004 · N581P · Cvac 580 · TireSDR 15HA0258007Actuator · separatedAFTER TAKEOFF, ENROUTE, THE PILOT HEAR A POP OR SNAP AFTER RAISING THE LANDING GEAR. THERE WERE NO OTHER ABNORMAL INDICATIONS IN THE COCKPIT AND THE FLIGHT WAS CONTINUED AND TERMINATED. THE LANDING WAS LOWERED UNEVENTFULLY. DURING THE POSTFLIGHT INSPECTION,Nov 2, 2002 · N581P · Cvac 34031 · Landing Gear ActuatorSDR I5HA0258008Wire · looseWHILE EN ROUTE FROM CVG-PIT, THE CAPTAIN NOTICED A MOMENTARY PUFF OF SMOKE COMING FROM THE FLIGHT DIRECTOR. THE FLIGHT DIRECTOR FUSELAGE WAS REMOVED AND THE FLIGHT WAS CONTINUED UNEVENTFULLY AND TERMINATED IN PIT. A LOOSE POWER WIRE ON THE FLIGHT DIRECTOR CONov 1, 2002 · N581P · Cvac 580 · Navigation System Wiring
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