N59083, cancelled Aug 15, 2013
Service difficulty reports · 29
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 = 'N59083' AND deregistration_id = 'N59083-2013-08-15' 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.
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 = 'N59083' AND deregistration_id = 'N59083-2013-08-15' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CNMA20060023Seal · cutABOUT 1.5 HRS INTO FLIGHT NR3 ENG OIL PRESSURE WENT TO 10 PSI, NR3 ENG OIL QUANTITY WENT TO ZERO. PERFORMED PRECAUTIONARY ENG SHUTDOWN NR3 ENG. UPON INSPECTION OF ENGINE FOUND HYDRAULIC PUMP LOCKOUT KIT LEAKING. REF DMI NR 8739. REMOVED LOCKOUT KIT AND FOUNDSDR CNMA20060015Oven · odorWHEN FORWARD OVENS 307 & 308 WHERE TURNED ON A STRONG ODOR CAME FROM THEM. WHEN TURNED OFF ODOR DISSIPATED. CLEANED TRAYS BOTH OVENS 307 & 308, OPS CHECK, NO ODOR NOTED, GOOD FOR SERVICE. OMNI AIR IS CURRENTLY ADDING AN INTERVAL FOR CLEANING OVENS AND OVEN SDR CNMA20060007Push-Pull Cable · brokenDURING TAKEOFF ROLL NR 3 ENGINE WOULD NOT SPOOL UP. INDICATIONS DID NOT CHANGE NO MATTER THROTTLE POSITION. ENGINE REMAINED IN IDLE THRUST. ABORTED TAKEOFF AT 65KTS. FOUND THROTTLE PUSH-PULL CABLE BROKEN AT PYLON REMOVED AND REPLACED PUSH-PULL CABLE IAW MMSDR CNMA200600002Charger · malfunctionedDURING CLIMBOUT BATTERY VOLTAGE READ 0 WITH NO CLOCKS. BATTERY CHARGER RELAY RESET 2 TIMES IN-FLIGHT WITH BATTERY VOLTAGE NORMAL AND CLOCKS RETURNED. CHARGER FAILED AGAIN, BATTERY VOLTAGE 0 FOR REMAINDER OF FLIGHT WITH NO CLOCKS. ALL OTHER INDICATIONS NORMASDR CNMA2006002Charger · inoperativeDURING CLIMBOUT BATTERY VOLTAGE READ 0 WITH NO CLOCKS. BATTERY CHARGER RELAY RESET 2 TIMES IN-FLIGHT WITH BATTERY VOLTAGE NORMAL AND CLOCKS RETURNED. CHARGER FAILED AGAIN, BATTERY VOLTAGE 0 FOR REMAINDER OF FLIGHT WITH NO CLOCKS. ALL OTHER INDICATIONS NORMASDR CNMA200500015Check Valve · leakingFUEL VENTING OUT OF THE LEFT WING VENT BOX AREA. RIGHT SIDE OK. NO TANK OVERFILLED LT ON. APPROX 1600 LBS VENTED. AFTER BLOCK IN FUEL LEAKING OUT OF LEFT FUEL VENT BOX DRAIN. REMOVED AND REPLACED CLIMB VENT FLOAT VALVE IAW DC10 M/M 28-12. ALSO REMOVED ANSDR 2005000015Valve · malfunctionedFUEL VENTING OUT OF THE LEFT WING VENT BOX AREA. RIGHT SIDE OK. NO TANK OVERFILLED LIGHT ON. APPROX 1600 LBS VENTED. AFTER BLOCK IN FUEL LEAKING OUT OF LEFT FUEL VENT BOX DRAIN. REMOVED AND REPLACED CLIMB VENT FLOAT VLV IAW DC10 M/M 28-12. ALSO REMOVED ANSDR CNMA200500014Check Valve · leakingAFTER T/O, GOT THE TANK OVERFILLED LT ON. VISUAL CHECK CONFIRMED FUEL VENTING OUT OF THE LEFT WING VENT. FUEL VENTED FOR APPROX 20 MIN. FUEL LOSS CONFIRMED OUT OF NR 3 MAIN AT 2000 LBS. TRIED TAKING TANKS DOWN TO 3000 LBS BELOW FULL AND REFILLING THEM USINSDR CNMA2005014Check Valve · malfunctionedAFTER T/O, GOT THE TANK OVERFILLED LEFT ON. VISUAL CHECK CONFIRMED FUEL VENTING OUT OF THE LEFT WING VENT. FUEL VENTED FOR APPROX 20 MIN. FUEL LOSS CONFIRMED OUT OF NR 3 MAIN AT 2000 LBS. TRIED TAKING TANKS DOWN TO 3000 LBS BELOW FULL AND REFILLING THEM USSDR 2005000014Check Valve · malfunctionedAFTER T/O, RECEIVED TANK OVERFILLED LIGHT ON. VISUAL CHECK CONFIRMED FUEL VENTING OUT OF THE LEFT WING VENT. FUEL VENTED FOR APPROX 20 MIN. FUEL LOSS CONFIRMED OUT OF NR 3 MAIN AT 2000 LBS. TRIED TAKING TANKS DOWN TO 3000 LBS BELOW FULL AND REFILLING THEM SDR 2004000015Cowling · departedAT CLIMB-OUT, NR 3 ENG LOST ENGINE COWLING DUMPED FUEL RETURNED TO EDDF.SDR 2004000007Engine · failedON T/O ROLL, NR 1 ENGINE MADE LOUD BANG, ENGINE FAIL LIGHT ILLUMINATED AND EGT PEGGED. N1 WAS 130 PERCENT AND SPEED WAS 125 KIAS. T/O ABORTED. TOWER NOTED FIRE FROM INTAKE.SDR 2004000001Seal · leakingNR 2 ENGINE OIL QUANITY STEADILY DECREASED DURING CRUISE. LOST 2.5 QTS IN 50 MINUTES. SHUTDOWN ENGINE TO PRESERVE OIL QTY. RESTARTED ENGINE AT ALT. FL 240, QTY HELD OK FOR APPROACH AND LANDING. FROM PREVIOUS ENGINE DRIVEN HYD PUMP REMOVAL AND BLOCKOUT FOUND SSDR CNMA200300011Rudder · stuckON SHORT FINAL AND FLARE RUDDER PEDALS COULD NOT BE MOVED. RUDDER PEDALS COULD NOT BE MOVED ON TAXI IN. TILLER OPERATION NORMAL. CAPTAINS AND CO-PILOTS SAME. LIMITED TRAVEL AT GATE. TAXI CHECK OF RUDDER PEDALS NORMAL. F/O DID NOTICE ALOT OF RUDDER FORCE ON TAKSDR CNMA200300008Engine · overtempON INITIAL CLIMBOUT NR 1 ENGINE OIL TEMP CLIMBED TO AND EXCEEDED LIMITS. (PEGGED OUT) SHUT DOWN ENGINE.SDR CNMA200300001Slide · dislodgedWHILE AT GATE FLIGHT ATTENDANT OPENED R-1 DOOR WITHOUT DISARMING DOOR. SLIDE CAME OUT OF ITS CONTAINER AND LANDED ON TOP OF CATERING TRUCK AWAITING TO DELIVER. APPARENTLY SLIDE DID NOT FALL FAR ENOUGH TO ACTIVATE DEPLOYMENT MECHANISM. SLIDE WAS REMOVED AND SDR CNMA200200007Electrical BoxOverspeed warning sounded at 270 knots - slats confirmed retracted. Removed and replaced Proximity Electronic Unit. Bite test normal.SDR CALA0100762Spar · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 3 PYLON LOWER SPAR WEB AT FAN DUCT CUTOUT. A REPAIR ANGLE AND STIFFENER WERE INSTALLED IAW SRM 54-20-00, FIGURE 19A.SDR 20000810SH021Harness · chafedD-CHECK, FQI SYSTEM WIRING CHAFING AND ARCING INSIDE FUEL TANK NR 3, PROBE NR 6, HARNESS FOUND CHAFING ON MOUNT BRACKET OF THE FILL ALOT VALVE IN BAY R07 (XORS- -298-500). WIRES 3E900E22GR X 3E901E22WH DAMAGED THROUGH OUTER SLEEVE INSULATION CAUSING ARCING ONSDR 20000829SH007Harness · chafedD-CHECK, FQI SYSTEM WIRING CHAFING AND ARCING INSIDE FUEL TANK NR 3, PROBE NR 6. HARNESS FOUND CHAFING ON MOUNT BRACKET OF THE FILL PILOT VALVE IN BAY R07 (XORS: -298-500). WIRES 3E900E22GR X 3E901E22WH DAMAGED THROUGH OUTER SLEEVE INSULATION CAUSING ARCINGSDR CALA0001384Harness · frayedINSPECTION FOUND RT WING FUEL TANK WIRING OUTER AND INNER INSULATION CHAFING AND ARCING DAMAGE ON FLOAT SWITCH BRACKET ZONE R07-11, LOCATION T2-104, PROBE XORS = 298.500. ALSO FOUND RT WING FUEL TANK WIRING FRAYED AND INNER FERRULE AT TANK PROBE T2-105, ZONE SDR CALA9901355Floorbeam · corrodedFLOORBEAM J SECTION AT STN 1887 AT 27R - 33R CORRODED. REMOVED CORRODED AREA. FABRICATED AND INSTALLED NEW SECTION PER SRM 51-21-00 AND GMM 10-900-01.SDR CALA9901354Floorbeam · corrodedFLOORBEAM J SECTION AT STA 1887 AT 60L - 90L CORRODED. REMOVED CORRODED AREA. FABRICATED AND INSTALLED NEW SECTION PER SRM 51-21-00 AND GMM 10-900-01.SDR CALA9901353Floorbeam · corrodedFLOORBEAM J SECTION CORRODED AT ST 1887 AT 60R - 90R. REMOVED CORROSION. FABRICATED AND INSTALLED NEW SECTION PER SRM 51-21-00 AND GMM 10-900-01.SDR CALA9901352Floorbeam · corrodedFLOOR BEAM J SECTION CORRODED AT ST 1887 AT 39L TO 58 L. REMOVED CORROSION AND INSTALLED NEW SECTION PER SRM 51-21-00 AND GMM 10-900-01.SDR CALA9900878Decoder · shortedSMOKE APPEARED IN THE AIRCRAFT CABIN NEAR THE VICINITY OF SEATS 37 AND 38KL WHILE ON FINAL APPROACH TO DUS. THE FLIGHT ATTENDANT'S PULLED OVERHEAD PANEL IN THE AREA AND USED HALON TO COOL THE AREA. NO FIRE WAS OBSERVED. THE AIRCRAFT LANDED AT DUS WITHOUT INSDR CALA9801129Battery Charger · inoperativeINSPECTION FOUND THE EMERGENCY AISLE LIGHTING INOPERATIVE AT ROWS 9 AND 10 (LEFT AND RIGHT). THE BATTERY CHARGER AT DOOR 2R AND 2L GALLEY OVERHEAD PANEL WAS REPLACED AND THE EMERGENCY LIGHT BATTERY PACK WAS CHARGED. OPERATIONAL CHECKS WERE GOOD IAW MM 33-50-SDR CALA9800537Slide · inoperativeINSPECTION FOUND THE R-3 DOOR SLIDE BOTTLE PRESSURE LIGHT ILLUMINATED. THE R-3 DOOR SLIDE WAS REMOVED AND REPLACED AND THE LIGHT TESTED NORMAL.SDR CALA9800206Fire Detector · chafedTHE NR 2 ENGINE A FIRE LOOP DETECTOR LIGHT BEGAN TO FLICKER WHILE IN CRUISE FLIGHT FROM LGW TO EWR. WHEN THE NR 2 ENGINE THRUST WAS REDUCED THE FLICKERING STOPPED. WHEN THRUST WAS ADDED THE FLICKERING RESUMED. THE NR 2 ENGINE WAS OPERATED WITH PARTIAL THRUS
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