N586AS
Service difficulty reports · 485
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 = 'N586AS' AND registry_match = 'registration' 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 = 'N586AS' AND registry_match = 'registration' 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 ASAA2016020115291Channel · crackedAFT CARGO COMPARTMENT RT ZEE CHANNEL SIDEPLATE CRACKED AT SEVERAL FRAME LOCATIONS FROM BS 727G-BS767, RBL 21.0, BS 727G - BS 767, RBL 21.0 - RBL 21.0, STR 25R-STR 25R. ACFT GROUNDED. ACCOMPLISHED AFT CARGO COMPARTMENT RT ZEE CHANNEL SIDEPLATE REPAIR FROM BS 7SDR ASAA2016020115290Floor Panel · corrodedFWD CARGO COMPARTMENT FLOOR PANEL 120DF HAS CORROSION AROUND EDGE. ACFT GROUNDED. REMOVED CORROSION PANEL 120DF FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. FABRICATED NEW FLOOR PANEL 120F IAW 453A2610, REV B APPLIED ALODINE AND PRIMER TO PANEL 120DF IAW SRM SDR ASAA2016020115275Floorbeam · corrodedFWD CARGO COMPARTMENT AFT BULKHEAD LOWER FLOOR SUPPORT ANGLE CORRODED BS 500I, RBL 21 - LBL 21. ACFT GROUNDED. REMOVED CORROSION FWD CARGO BULKHEAD LOWER FLOOR SUPPORT ANGLE BS500 ORIGINAL MATERIAL THICKNESS WAS .071 LOST .016 REMAINING IS .055 FOUND TO BE OSDR ASAA2016012414983Warning Message · false activationFMC DISAGREE ANNUNCIATED AFTER PUSH BACK. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMCS RESTORED NORMAL.SDR ASAA2016012014935Warning Message · false activationDATALINK FULL ALERT MESSAGE ON CDU. COMPLETED QRH PROCEDURE IAW FLIGHT HANDBOOK. ACFT GROUNDED. ACCOMPLISHED FIM 34-61, TASK 839. OPS NORMAL.SDR ASAA2016011414829Warning Message · false activationON GROUND, FMC DISAGREE LIGHT. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMCS RESTORED NORMAL.SDR ASAA2016010814703Engine · faultedIAW T/C 78273000, FOUND NR 1 ENGINE WITH ECONOMIC FAULT 73-31371. UPPER EGT SECTORS READING HIGH. ACFT GROUNDED. ON DEFERRAL.SDR ASAA2016010614643Exciter · failedAPU HAS HISTORY OF NO STARTS. ACFT GROUNDED. R & R IGNITER PLUG, IGNITER PLUG LEAD AND EXCITER IGNITER UNIT IAW AMM 49-41-15, 49-41-52, 49-41-31.SDR ASAA2015122914552Apu · faultedFAULT LIGHT ON APU ATTEMPTED START IAW QRH FAULT LIGHT EXITING. LESS THAN 5 MINUTES ATTEMPTED ANOTHER START, ANOTHER NO START, WITH FAULT LIGHT. ACFT GROUNDED. PERFORMED FIM APU BITE CHECK, IAW MM 49-60-801. FAULT CODE 49-41011 DISPLAYED NO FLAME SHUTDOWN, SDR ASAA2015122214358Fuel Nozzle · failedFOUND NR 2 ENGINE W/ ECONOMIC FAULT 73-31372, UPPER EGT SECTORS READ HIGH. ACFT GROUNDED. ACCOMPLISHED T/C POWER REPLACED-73 COMPARTMENT-07267-2. REPLACED MAIN ENGINE FUEL NOZZLES. ECONOMIC FAULT 73-31372, CLEARED.SDR ASAA2015122114378Wire Harness · damagedNR 2 ENGINE RT UPPER FIRE WARNING HARNESS TERMINAL END AT FIRE LOOP IS BROKEN. ACFT GROUNDED. R & R NR 2 ENGINE CORE FIRE DETECTION HARNESS MW0326, REF AMM 26-11-02. OPS NORMAL REF AMM 26-11-00.SDR ASAA2015120114065Satcom · lockedSATCOM LOCKUP. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. SATCOM RESTORED NORMAL.SDR ASAA2015112413969Warning Light · false indicationELECTRIC ANNUNCIATOR LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED FIM 24-31, TASK 801, ELECTRIC FAULT CLEARED.SDR ASAA2015100513343Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. RAN QRH. OPS NORMAL.SDR ASAA2015093013287Warning Light · false activationELEC WARNING LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED ELECTRONIC LIGHT BITE PROC REF FIM 24-31, TASK 801. LOGGED SPCU INOPERATIVE MSG. PERFORMED FIM 24-34, TASK 802 & FAULT CLEARED. DRD FUNCTIONAL TEST PASSED. NO HISTORY OF FAULT LAST 30 DAYS.SDR ASAA2015090912989Sign · detachedFRONT HALF OF MID CABIN EXIT SIGN FELL OFF. ACFT GROUNDED. REINSTALLED MID CABIN SIGN, EXIT.SDR ASAA2015090612960Fault Code · activatedWHILE ACCOMPLISHING TASK CARD 78273000, INTEROGATE THE FMC CDU FOR ENGINE FAULTS, FOUND ECONOMIC FAULTS: 73-31371, UPPER EGT SECTORS READING HIGH, 73-31372, UPPER EGT SECTORS READING HIGH. ACFT GROUNDED. RE-ACCOMPLISHED T/C 78273000 FMC CDU ENGINE INTERROGATSDR ASAA2015080812764Warning Light · false activationON RECALL, LEFT PACK LIGHT ILLUMINATED. LIGHT OUT WHEN MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED BITE CHECK ON BOTH TEMP CONTROLLERS. LEFT TEMP CONTROLLER LOGGED TCV FAULT. FAULT REST, ON TEMP CONTROLLER LEFT TEMP CONTROLL GROUND VERIFICATION CHECKSDR ASAA2015080212682Display · failedWHILE TAXIING TO THE GATE THE CAPTAIN'S CDU WENT BLANK. ACFT GROUNDED. R & R LT CDU REF MM 34-61-01, OPS CHECK NORMAL.SDR ASAA2015080212677Control Valve · failedLEFT PACK LIGHT ILLUMINATED, DOES NOT GO OUT WITH TRIP RESET. ACFT GROUNDED. R & R NR 1 PACK TCV IAW AMM 21-51-10, OPS AND LEAK CHECK GOOD.SDR ASAA2015073112661Display · malfunctionedCA CDU SCREEN FAILED. ACFT GROUNDED. CYCLED NR 1 MCDU CIRCUIT BREAKER. NR 1 FMC AND CDU OPS CHECKED GOOD IAW MM 20-60-01 AND 34-61, TASK 835.SDR ASAA2015072812614Controller · malfunctionedLT PACK LIGHT ILLUMINATED ON MASTER CAUTION RECALL, GOES DARK ON RESET. ACFT GROUNDED. PERFORMED BITE TEST NR 1 TEMP CONTROLLER, RESET CONTROLLER. OPS CHECKED NORMAL, REF TASK 21-61-00-700-806-002. NO HISTORY LAST 30 DAYS.SDR ASAA2015072612607Engine · sparksWHILE POWERING UP TO TAKE RUNWAY FOR TAKEOFF, ANOTHER ACFT OBSERVED SPARKS AND/OR FLAMES COMING FROM NR 1 TAILPIPE. ALL ENGINE INDICATIONS WERE NORMAL WITH NO FIRE INDICATIONS. ACCOMPLISHED ENGINE TAILPIPE FIRE CHECKLIST. NO FURTHER SPARKS OF FLAMES OBSERVSDR ASAA2015072612598Start Valve · failedSTART VALVE FAILED TO CLOSE ON NR 1 ENGINE START. ACFT GROUNDED.SDR ASAA2015072112508Probe · out of limitsNR 1 ENGINE TREND DATA SHOWS INCREASE IN EGT AND A DECREASE IN EGT HOT DAY MARGIN. ACFT GROUNDED. ACCOMPLISHED NR 1 ENGINE EGT SYSTEM INSPECTION, REF 77-21-01. FOUND S1 AND S4 OUT OF LIMITS IAW TABLE C. REPLACED EGT PROBES S1 AND S4 IAW 77-21-01. PERFORMESDR ASAA2015071912507Actuator · damagedDURING REMOVAL OF CONNECTOR DP1002, FOUND RUBBER ISOLATOR FOR PINS DAMAGED ON VSV ACTUATOR, NR 1 ENGINE. ACFT GROUNDED. REMOVED LT VSV ACTUATOR IAW AMM 75-31-01-000-801-F00, INSTALLED SERVICABLE LT VSV ACTUATOR IAW AMM 75-31-01-400-801-F00.SDR ASAA2015071912506Circuit Breaker · trippedENGINE 1 ALTN POWER CHANNEL A CIRCUIT BREAKER FOUND POPPED ON PREFLIGHT. ACFT GROUNDED. CHECKED C/B PANEL, RESET C/B, PREFORMED FIM 73-00, TASK 801, NO FURTHER PROBLEMS, OPS GOOD, REF MM 20-60-01. PERFORMED GROUND VERIFICATION TEST IAW MM 73-21-00-700-804-FSDR ASAA2015071812489Wire Harness · damagedNR 1 ENGINE EGT SHOWED HIGH TEMPERATURE EXCEEDANCE. ON TAKEOFF, APPROXIMATELY 1000 DEGREES FOR A FEW SECONDS. AUTO THROTTLES WERE ON ENGINE OPERATED NORMALLY AFTER THAT EVENT. AT CRUISE NR 1 ENGINE TEMPERATURE SHOWED 30 DEGREES HIGHER THAN NR 2 ENGINE. ACFSDR ASAA2015071412442Warning Light · false activationPRIOR TO TAKEOFF IN FMC DISAGREE LIGHT BOTH SIDES. ACFT GROUNDED. QRH PROCEDURE UTILIZED. LIGHT EXTINGUISHED. CONTINUE NORMAL OPS.SDR ASAA2015061112076Light · inoperativeFWD LEFT EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. R & R THE EMERGENCY LIGHT. OPS CHECKED GOOD IAW AMM 33-51-04.SDR ASAA2015060511990Circuit Breaker · trippedGENERATOR NR 1 DISC CIRCUIT BREAKER TRIPPED. ACFT GROUNDED. CHECKED HISTORY. NO HISTORY 90 DAYS. RESET CIRCUIT BREAKER ON P6-4 GENERATOR DISC 1, IAW WDM 24-11-11 AND MM 20-60-01. RAN NR 1 ENGINE AND OPS TESTED DISCONNECT FOR NR 1 IDG. OPS NORMAL. RESET ISDR ASAA2015060311956Warning Light · false activationRIGHT PACK LT ILLUMINATED DURING CLIMB IAW QRH RESET. ACFT GROUNDED. PERFORMED PACK ZONE TEMP CONTROLLER BITE TEST. NO FAULT FOUND. GROUND VERIFICATION COMPLETE REF AMM 21-61-00. NO HISTORY LAST 30 DAYS.SDR ASAA2015042411488Warning Message · false activationFMC DISAGREE ON GROUND. GROUNDED - YES. COMPLETED QRH CHECKLIST. FMC DISAGREE MSG NO LONGER DISPLAYED.SDR ASAA2015042211467Engine · fault messageWHILE ACCOMP T/C 78273000, FOUND NR 2 ENG WITH ECONOMIC FAULT 73-31372, UPPER EGT SECTORS READ HIGH. ACFT GROUNDED. ACCOMPLISHED T/C 78273000. NO FAULTS LOGGED.SDR ASAA2015041611390Engine · malfunctionedDURING START OF NR 2 ENGINE, NO FUEL FLOW AND EGT WHEN START LEVER PLACED TO IDLE. NR 2 ENGINE RT IGNITION C/B DISCOVERED OPEN. ACFT GROUNDED. INSPECT NR 2 CB FOR DEFECTS NO DEFECTS NOTE. RESET CC IAW AMM 20-60-01-860-801. PERFORMED AMM TASK 74-00-00-750-8SDR ASAA2015041511363Transceiver · failedNR 1 HF INCOMING COMMS GARBLED AND UNREADABLE. OUTGOING TRANSMISSIONS WORK FINE. TRIED TUNING & DETUNING SEVERAL FREQUENCIES WITH NO CHANGE. PREFLIGHT HF NR 1 CHECK HAD ALL COMMS NORMAL. HF NR 2 WORKS PERFECTLY. ACFT GROUNDED. REMOVED AND INSTALLED NR 1 HF SDR ASAA2015040911304Probe · faultedDIAGNOSTIC REPORTS NR 1 ENGINE TREND DATA SHOWS A SHIFT IN CRUISE AND TAKEOFF MARGIN INDICATIVE OF EGT INDICATION ERRORS. ACFT GROUNDED. WHILE COMPLYING WITH TC 78273000 FOUND ECONOMIC FAULT 77-20861 ON ENGINE 1ESN894921. READINGS OF ENGINE NR 1 T49.5 PROBESDR ASAA2015040111203Satcom · lockedSATCOM APPEARS TO BE LOCKED UP. ACFT GROUNDED. REBOOTED SATCOM SYS REF FIM 23-15-00-23-801. NO HISTORY 30 DAYS. GROUND VERIFICATION GOOD.SDR ASAA2015012610444Panel · looseNR 1 ENGINE, INLET FAN DUCT PANEL NR 8 HAS LOOSE FASTENERS. ACFT GROUNDED. RETIGHTENED FASTENERS REF AMM 72-23-07-000-801-F00.SDR ASAA2015012010327Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. QRH COMPLIED WITH OPS NORMAL.SDR ASAA2015012010326Fmc · malfunctionedAT TOP OF CLIMB, 34000, CAPTAIN'S FMC'S SCREEN WENT BLACK, AFTER A FEW SECONDS IT RETURNED TO NORMAL OPERATIONS AFTER A START UP TEST SCREEN. ACFT GROUNDED. PERFORMED FIM TASK 34-61 TASK 801 NO DEFECTS NOTED NO HISTORY LAST 30 DAYS. ACFT OK FOR SERVICE.SDR ASAA2014122510066Radio · malfunctionedNR 1 HF RADIO FREQUENCY DISPLAY READS "FAIL/FAIL". RADIO TUNES AND TRANSMIT, RECEIVES NORMAL. AFTER 10 SECONDS FAIL WARNING APPEARS. ACFT GROUNDED. RESET NR 1 HF AND NR 2 HF, PERFORMED BITE CHECK PROCEDURE. NO FAULTS NOTED, NO FAIL INDICATED, REF AMM FIMSDR ASAA2014121109934Bleed Valve · failedBLEED TRIP OFF LIGHT LT SIDE CAME ON CLIMBING THROUGH ABOUT 20,000'. RESET PROCEDURES IAW QRH UNSUCCESSFUL. DUCT PRESSURE 0 PSI LT SIDE. ACFT GROUNDED. ACCOMPLISHED FIM 36-10, TASK 801. REPLACED NR 1 PCCV IAW AMM 36-12-02. OPS CHECK NORMAL. R & R NR 1 PCCSDR ASAA2014121109921Autothrottle Sys · malfunctionedAUTOTHROTTLES ARMED FOR TAKEOFF, AUTOTHROTTLES DISCONNECTED AND BOTH FD MASTER LITES ILLUMINATED WHEN TOGA BUTTON WAS PUSHED. ACFT GROUNDED. ACCOMPLISHED DFCS BITE CHECK IAW FIM 22-11, TASK 801 FOUND IRU DATA INVALID IN HISTORY. NO CURRENT FAULTS. ACCOMPLISDR ASAA2014120109846Warning Message · false activation"DATALINK FULL" MESSAGE ON GROUND. ACFT GROUNDED. ACCOMPLISHED QRH. OPS NORMAL.SDR ASAA2014112809783Shim · wornR 2 ENGINE FOUND ALL FAN BLADE SHIMS EXHIBIT MORE THAN 25 PERCENT MOLYDAG COATING IAW MM 72-21-02-200-801, STEP 2. L, 1, B, 1. ACFT GROUNDED. REPLACED ALL SHIMS ON NR 2 ENG FAN BLADES, REF T/C 78472002.SDR ASAA2014112309731Controller · failedNOTICED RAPID EAR PRESSURE CHANGE, CABIN CLIMB GAUGE WAS PEGGED AT NO AUTO FAIL LIGHT LIGHT. OUTFLOW VALVE INDICATOR WAS SHOWING FULL CLOSED. DURING DESCENT BELOW ABOUT 18000 FT, CABIN ALTITUDE WAS GOING BELOW SEA LEVEL. AT THIS TIME WE MOVED PRESS CONTROLLSDR ASAA2014112209737Probe · failedDIAGNOSTICS REPORTED NR 1 ENGINE TREND DATA SHOWED A SHIFT IN DELTA CRUISE AND TAKEOFF MARGIN INDICATIVE OF EGT INDICATION ERRORS. ACFT GROUNDED. T49.5 S2 PROBE HIGH RESISTANCE. REPLACED S2 PROBE IAW MM 77-21-01, EEC TEST PASS. EGT SYS INSPECTION NORMAL REF SDR ASAA2014112209727Shim · wornNR 1 ENGINE, FAN BLADE SHIM WORN AND DAMAGED. ACFT GROUNDED. R & R FAN BLADE SHIM IAW TC 78472002.SDR ASAA2014112209726Blade · wornFOUND CU-NI-IN COATING MISSING, CHIPPED MORE THAN AREA Y ON NR 1 ENGINE FAN BLADES: NR 1 , 7 , 11, 12, 13, 19, 23, 24, REF MM 72-21-02-200-801-FOO AND T/C 78472003, AND FAN BLADE NR14 HAS WEAR FROM SHIM IN AREA G MEASURED AT .0095 WITH SMARTSCOPE. ACFT GROUN
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