N491SH, cancelled Jan 10, 2008

Service difficulty reports · 20

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 = 'N491SH' AND deregistration_id = 'N491SH-2008-01-10'
  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 ASMF200408006Proximity Switch · damagedDURING TRANSIT CHECK, CAPTAIN REPORTED SLAT DISAGREE LIGHT TURNED ON. PSEU WAS TESTED SHOWING FAIL CODES 510 AND 580. PSEU WAS REPLACED IAW 34-19-01, BUT FAIL CONTINUED. LT SLAT SENSORS WERE CHECKED DETECTING FAIL IN SENSOR "C", SENSOR "C" AND ITS SPRING WEREAug 7, 2004 · N491SH · Doug DC982 · Leading Edge Slat Control SystemSDR ASMF200406016Damper · jammedAIRCRAFT RETURNED TO PLATFORM, DURING TAXING AND ELEVATOR CONTROL TEST, CAPTAIN REPORTED ELEVATOR JAMMED. ELEVATOR CONTROL SYSTEM WAS CHECKED AND DAMAGE WAS DETECTED IN CONTROL COLUMN DURING MOVEMENT OF NOSE DOWN. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVJun 17, 2004 · N491SH · Doug DC982 · Elevator Control SystemSDR ASMF200406010Warning Light · illuminatedAIRCRAFT REJECTED TAKE OFF AT 110 KNOTS AND RETURNED TO PLATFORM, (RT STRAINER CLOGGING) LIGHT TURNED ON. RT FILTER WAS REMOVED, CHECKED, CLEANED AND ENGINE OIL WAS REPLACED IAW MM 79-20-06, WHEELS WERE CHECKED BY REJECTED TAKE OFF, ALL CORRECT. DURING TRANSJun 12, 2004 · N491SH · Doug DC982 · Engine Oil Indicating SystemSDR ASMF200405022Switch · out of adjustAIRCRAFT RETURNED TO PLATFORM, (TAKE OFF) WARNING FLAG SHOWS, DURING TAKE OFF CONFIGURATION. DURING MAINTENANCE REVISION, FLAPS WERE OPERATED AND FAIL CONTINUE. VISUAL INSPECTION WAS PERFORMED AND WAS DETECTED THAT THE FLAP LEVER DOES NOT ACTUATE THE TAKE OFF May 19, 2004 · N491SH · Doug DC982 · Trailing Flap Position Indicating SystemSDR ASMF200403003Proximity Switch · failedDURING TRANSIT CHECK THE RIGHT AIR CONDITIONING TEMPERATURE CONTROL WAS OUT OF SERVICE. ADDITIONALLY, DURING TAKEOFF THE NOSE LANDING GEAR RED LIGHT WAS NOT TURNED OFF. THE PROXIMITY SWITCH ELECTRONIC UNIT (PSEU) WAS TESTED AND FAIL CODES 510 AND 580 APPEARMar 7, 2004 · N491SH · Doug DC982 · Landing Gear Position and WarningSDR MEX2004007Indicator · malfunctionedAIRCRAFT RETURNED TO PLATFORM AFTER ENGINES STARTING THE PO ALTIMETER FLAG CAME ON. CADC NR 2 WAS RESEATED AND TESTED IAW MM, ALL TESTED CORRECT. THE FLAG DISAPPEARED BUT IT HAD 130 FEET INDICATION BETWEEN ALTIMETERS. PNEUMATIC CONNECTIONS OF CADC NR 2 AND Jan 5, 2004 · N491SH · Doug MD83 · Altimeter, Barometric/EncoderSDR MEX2003488Door · damagedAFTER AIRCRAFT LANDED THRUST REVERSERS WERE EXTENDED BEFORE NOSE LANDING GEAR HAD BEEN CONTACT ON THE GROUND, SCRATCHING THE THRUST REVERSES LOWER DOORS OF BOTH ENGINES (LARGE: 12 INCH, WIDE 1.5 INCHES APPROX). PERSONNEL WAS SENT TO REPAIR THE DAMAGES. BOTH Oct 14, 2003 · N491SH · Doug DC982 · Engine Thrust ReverserSDR MEX2003288Switch · malfunctionedFLT 215 - HMO-GDL - AIRCRAFT ARRIVED WITH CAPTAIN REPORT 'L ICE PROTECT TEMP HI' LIGHTS TURN ON. DURING TRANSIT CHECK THE THERMOSTAT AND ANTICIPATOR WERE REPLACED IAW MM 36-10-00. AIRCRAFT WAS DISPATCHED AND AIR TURN BACK AS A CONSEQUENCE OF 'L ICE PROTECT TEJul 14, 2003 · N491SH · Doug DC982 · Airfoil Anti/De-ice SystemSDR MEX2003247Pulley · failedDURNG SLATS CABLE ADJUSTMENT WAS FOUND RUBBING BETWEEN CABLE PULLEYS OF SLAT NR '0', LOCATED IN THE RT OF THE SLAT DRIVE MECHANISM. BOTH PULLEYS WERE REPLACED AND GAINED ENOUGH SEPARATION. CABLE DEFLECTION WAS MEASURED, FOUNDED 25/34 INCHES, WITHIN LIMITS IAJun 17, 2003 · N491SH · Doug DC982 · Leading Edge Slat Control SystemSDR MEX2003154Valve · failedDURING COCKPIT CHECK THE CAPTIAN FOUND PROBLEMS WITH (AUTO LAND) BUTTON AND LEFT PRESSURE REGULATOR VALVE. THE BUTTON WAS DEFERRED BY MEL CATEGORY C AD THE VALVE WAS REPLACED IAW MM.May 3, 2003 · N491SH · Doug MD83 · Autopilot SystemSDR MEX2003054Transmitter · failedDURING CREW CABIN REVISION, CAPTAIN REPORTED LEFT ENGINE HYDRAULIC PUMP OUT OF SERVICE WITH 3000 PRESSURE INDICATION. LT TRANSMITTER HYDRAULIC PRESSURE WAS REPLACED AND IT WAS PERFORMED OPERATIONAL TEST WITH ZERO PRESSURE INDICATION, IAW MM, TESTS CORRECT.Mar 2, 2003 · N491SH · Doug DC982 · Hydraulic Pressure SensorSDR MEX2003024Socket · burnedAIRCRAFT ACCOMPLISHED AN UNSCHEDULED LANDING, SMOKE IN FORWARD GALLEY. DURING CRUISE WAS DETECTED SMOKE IN PASSENGERS CABIN FROM THE UPPER PART OF THE FORWARD GALLEY OVENS A SMOKE WAS INCREASED WHEN THE SYSTEM WAS SHUTOFF. OVEN NR 2 WAS CHECKED BY CONDITION Feb 4, 2003 · N491SH · Doug DC982 · Buffet/GalleysSDR MEX2003003Indicator · failedAIRCRAFT RETURNED TO PLATFORM DUE TO FIRST OFFICER ALTIMETER OFF FLAG. ALTIMETER WAS RESET BUT FLAG CONTINUES. BOTH CADCS WERE INTERCHANGED, TESTS WERE PERFORMED IAW MM. AFTER TESTS, 130 FT DIFFERENCE BETWEEN ALTIMETERS APPEARS. PNEUMATIC CONNECTIONS WERJan 5, 2003 · N491SH · Doug DC982 · Altimeter, Barometric/EncoderSDR MEX2002274Fcu · failedFLT 252 - MEX-GDL - AIRCRAFT RETURNED TO GATE DUE TO ACCELERATION FAILURE OF LEFT ENGINE. THE ACCELERATION CHAMBER WAS REVISED AND IT WAS PERFORMED A TRIM IAW MM 73-20-03 AND 73-11-00, TESTS OK. THE FCU OF LEFT ENGINE WAS REPLACED, TRIM WAS PERFORMED, TESTS Aug 23, 2002 · N491SH · Doug DC982 · Fuel Control/Turbine EnginesSDR MEX2002245Flow Valve · failedPILOT REPORTED A DIFFERENCE OF 6 DEGREES BETWEEN COMPASS AND RADAR WITH AN INDICATION FAILURE AND FLIGHT DIRECTORS OUT OF SERVICE IN TAKE OFF. DUE TO SUCH A FAILURE, A CHANGE OF EQUIPMENT WAS REQUESTED. THE FLOW VALVE OF THE COMPASS SYSTEM WAS REPLACED, IAWJul 29, 2002 · N491SH · Doug DC982 · Inertial Guidance SystemSDR MEX2002256Switch · failedAIRCRAFT RETURNED TO PLATFORM AS DUE TO AUTO SLAT FAIL LIGHT, THE STALL COMPUTER WAS REPLACED AND FAILURE CONTINUED, THE CONNECTORS OF STALL COMPUTER WERE CLEANED AND BOTH ACTUATOR CONNECTORS WERE RESEATED, TESTS WERE PERFORMED OK. DURING TAXI THE SAME LIGHTMay 8, 2002 · N491SH · Doug DC982 · Stall Warning SystemSDR MEX2002116Duct · leakingFLT 489 - SJD-ACA - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCES OF HIGH TEMPERATURE IN ENGINE NR 2 (470 GRADES), ENGINE WAS STARTED WITH A PNEUMATIC POWER GETTING 380 GRADES. DURING OVERNIGHT SERVICE WERE REPAIRED TWO PNEUMATIC LINES WITH LEAKS, TESTS WERE Apr 18, 2002 · N491SH · Doug DC982 · Pneumatic Distribution SystemSDR MEX2002082Filter · dirtyFLT 430 - PVR-LAX - CAPTAIN REPORTED HIGH TEMPERATURE AT ENGINE STARTING, THE ENGINE STARTING WAS PERFORMED THREE TIMES, AT THIS LAST TIME THE STARTING WAS INSIDE THE PARAMETERS. AIRCRAFT STARTED THE TAXI, HOWEVER IT RETURNED TO PLATFORM AS CONSEQUENCE OF AN Mar 24, 2002 · N491SH · Doug DC982 · Fuel Control/Turbine EnginesSDR MEX2002045Warning System · malfunctionedFLT 180 - MLM-HMO - DURING TAXI, CAPTAIN INFORMED THAT DC BUS OFF LIGHT IS ON. RESET THE CIRCUIT BREAKER, LIGHT WAS NOT OFF. AIRCRAFT RETURNED TO PLATFORM. BOTH BATTERIES WERE DISCONNECTED AND CONNECTED, RESET THE RELAYS R2-21 AND R2-326, TEST OK, IAW MM 24Feb 20, 2002 · N491SH · Doug DC982 · DC Indicating SystemSDR RG22002F00000Module · failedRECEIVED AT REPAIR STATION WITH UNCONTAINED TURBINE FAILURE. OPERATOR REPORTED THAT FAILURE OCCURED DURING AN APPROACH TO AIRPORT. AIRCRAFT ENCOUNTERED WINDSHERE WHEN AN ENGINE OVERBOOSTED. FAILURE OCCURE TO ENGINE 2 WHEN CUT BACK IN POWER. UNDER INVESTIGATJul 16, 2001 · N491SH · Doug DC982 · Turbine Section
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