# Service difficulty reports: N581P, cancelled Sep 10, 2024 A list on [N581P, cancelled Sep 10, 2024](https://openairdocs.org/deregistered/N581P-2024-09-10.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 15HA0858014](https://openairdocs.org/sdr/15HA0858014.md): O-Ring · leaking · Dec 19, 2008 · N581P · Cvac 580 · Propeller Feathering/Reversing > 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 FE - [SDR I5HA0858005G](https://openairdocs.org/sdr/I5HA0858005G.md): Channel · damaged · Jul 17, 2008 · N581P · Cvac 34031 · Fuselage Miscellaneous Structure > 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 A - [SDR I5HA0858005F](https://openairdocs.org/sdr/I5HA0858005F.md): Channel · damaged · Jul 17, 2008 · N581P · Cvac 34031 · Fuselage Miscellaneous Structure > 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. TH - [SDR I5HA0858005E](https://openairdocs.org/sdr/I5HA0858005E.md): Channel · damaged · Apr 5, 2008 · N581P · Cvac 580 · Standard Practices/Structures > 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 - [SDR I5HA0858005D](https://openairdocs.org/sdr/I5HA0858005D.md): Angle · damaged · Apr 5, 2008 · N581P · Cvac 580 · Standard Practices/Structures > 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 - [SDR I5HA0858005C](https://openairdocs.org/sdr/I5HA0858005C.md): Angle · damaged · Apr 5, 2008 · N581P · Cvac 580 · Standard Practices/Structures > 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 - [SDR I5HA0858005A](https://openairdocs.org/sdr/I5HA0858005A.md): Angle · damaged · Apr 5, 2008 · N581P · Cvac 580 · Standard Practices/Structures > 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 - [SDR I5HA0858005](https://openairdocs.org/sdr/I5HA0858005.md): Actuator · damaged · Apr 5, 2008 · N581P · Cvac 580 · Landing Gear Steering System > 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 T - [SDR I5H2008F00000](https://openairdocs.org/sdr/I5H2008F00000.md): Actuator · damaged · Apr 5, 2008 · N581P · Cvac 34031 · Landing Gear Steering System > 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 STEE - [SDR I5HA0758003](https://openairdocs.org/sdr/I5HA0758003.md): Relay · failed · Jan 15, 2007 · N581P · Cvac 580 · Fuel Controlling System > 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 - [SDR 15HA0658011](https://openairdocs.org/sdr/15HA0658011.md): Structure · damaged · Nov 8, 2006 · N581P · Cvac 580 · Leading Edge Devices > ON 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 THE - [SDR I5HA0258001](https://openairdocs.org/sdr/I5HA0258001.md): Wing · gouged · Jan 18, 2006 · N581P · Cvac 34031 · Wing, Plate/Skin > A 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 NOT - [SDR I5HA0258010](https://openairdocs.org/sdr/I5HA0258010.md): Access Panel · cracked · Oct 30, 2005 · N581P · Cvac 580 · Wing, Plate/Skin > DURING 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) - [SDR I5HA0558008](https://openairdocs.org/sdr/I5HA0558008.md): Arm · broken · Oct 1, 2005 · N581P · Cvac 34031 · Landing Gear Retraction/Extension System > ENROUTE, 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 AR - [SDR I5HA0258007](https://openairdocs.org/sdr/I5HA0258007.md): Tire · departed · Jun 24, 2004 · N581P · Cvac 580 · Tire > MFD - 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 I - [SDR 15HA0258007](https://openairdocs.org/sdr/15HA0258007.md): Actuator · separated · Nov 2, 2002 · N581P · Cvac 34031 · Landing Gear Actuator > AFTER 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, - [SDR I5HA0258008](https://openairdocs.org/sdr/I5HA0258008.md): Wire · loose · Nov 1, 2002 · N581P · Cvac 580 · Navigation System Wiring > WHILE 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 CO ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N581P-2024-09-10/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.