N583AS
Service difficulty reports · 465
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 = 'N583AS' 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 = 'N583AS' 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 ASAA2017072921506Housing · detachedR2 EXIT SIGN ABOVE DOOR LENS BROKEN OFF. ACFT GROUNDED. REMOVED AND REPLACED THE R2 DOOR EMERGENCY EXIT SIGN IAW AMM 33-51-01. OPS CHECKED NORMAL.SDR ASAA2017072921495Panel · looseWHILE ACCOMPLISHING TC 78472000, THE NR 1 ENGINE FOUND FAN DUCT PANELS LOOSE AT THE 1:00 & 7:00 POSITIONS. ACFT GROUNDED. TORQUED THE NR 1 ENGINE DUCT PANELS AT 1:00 AND 7:00 POSITIONS IAW AMM 72-23-07.SDR ASAA2017071021346Pressure Switch · failedNR 2 FUEL FILTER BYPASS LIGHT ILLUMINATED AT FL 370, JUST AFTER CENTER PUMPS TURNED OFF. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE FUEL DIFFERENTIAL PRESSURE SWITCH IAW AMM 73-34-01. OPS CHECKED GOOD.SDR ASAA2017070221250Pressure Switch · malfunctionedPERFORMED TASK CAR 78273000, #2 ENGINE HAD LONG TIME FAULT - 73-31072 - "THE FUEL FILTER SIGNALS DISAGREE". GROUNDED - YES. REFERENCE LOGPAGE 11803593, FUEL FILTER & DRAIN PLUG WERE REPLACED. LOG 11803589 THE FUEL DIFFERENTIAL PRESSURE SWITCH WAS REPLACED. A/CSDR ASAA2017062921249Pressure Switch · malfunctionedNR 2 ENGINE FILTER BYPASS LIGHT ON DURING TAXI, AFTER LANDING. ACFT GROUNDED. REPLACED THE NR 2 ENGINE EEC IAW AMM 73-21-60-00-801-F00, & 73-21-60-400-801. FUEL BYPASS STILL ON AND OFF PRIOR TO STARTING. PERFORMED INDENT/CONFIG IAW 73-21-00-700-808-F00, TSDR ASAA2017062421183Pressure Switch · failedAT ROTATION NR 2 ENGINE FUEL FILTER BYPASS ILLUMINATED. STAYED ON FOR ABOUT 15 MINUTES. ACFT GROUNDED. ON ARRIVAL, THE NR 2 ENGINE FUEL BYPASS LIGHT NOT ILLUMINATED. REMOVED AND REPLACED THE FILTER, NO CONTAMINATION NOTED ON FILTER AND LEAK CHECKED GOOD IAWSDR ASAA2017062021149Warning Light · false activationAFTER TAKEOFF, THE RIGHT NR 2 ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED. FOLLOWED CHECKLIST. LIGHT WENT OUT APPROXIMATELY 8 MINUTES AFTER TAKEOFF. ACFT GROUNDED. PERFORMED EEC TEST IAW AMM 73-21-00, NO FAULTS FOUND. PERFORMED EEC BITE, NO FAULTS FOUND.SDR ASAA2017061921136Transceiver · failedDURING PREFLIGHT, FOUND THE NR 2 HF CIRCUIT BREAKER OPEN. ACFT GROUNDED. REMOVED, REPLACED, AND TESTED THE NR 2 HF TRANSCEIVER IAW AMM 23-11-21-400-801, TEST PASSED. ACCOMPLISHED HF COMMUNICATION SYSTEM TEST IAW AMM 23-11-00-730-801, TEST PASSED. ETOPS SIGNISDR ASAA2017060820985Warning Message · false indicationON LANDING, BOTH FMC BLANKED ALONG WITH A VTK FLAG ON BOTH DISPLAYS. BOTH FMC RESUMED AND VTK FLAG CLEARED AFTER APPROXIMATELY 45-60 SECONDS. ACFT GROUNDED. PERFORMED FIM 34-61, TASK 801, AMM 34-61-00-860-801. NUISANCE ERROR, NO FAULT NOTED. OPS NORMAL.SDR ASAA2017060720977Shroud · crackedAPU DRAIN SHROUD APPEARS CRACKED ON TOP RADIUS/ FILLET. GROUNDED - YES. CONFIRMED CRACK , REMOVED AND REPLACED APU FUEL, HYD DRAIN MAST, REF B737-800 AMM 28-25-07-401SDR ASAA2017060320952Rod End · wornNR 2 ENGINE LOWER STARTER DUCT FWD ROD END WORN. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE LOWER STARTER DUCT FWD ROD END IAW AMM 36-11-01-000-802(2)(E)(9), AND AMM 36-11-01-400-302(3)(F)(6).SDR ASAA2017060320947Duct · gougedNR 2 ENGINE TAI VALVE DUCT AND BRACKETS HAD GOUGES FROM LINK ROD ENDS. GROUNDED - YES. REMOVED AND REPLACED #2 ENG TAI VALVE DUCT AND BRACKETS REF AMM CH. 30-21-11. LEAK CHECK GOOD.SDR ASAA2017052920897Fmc · false indicationAFTER LANDING, CAPTAIN'S DISPLAY SHOWED A VTK FLAG. WENT AWAY AFTER A MINUTE. ACFT GROUNDED. PERFORMED FIM 34-61, TASK 836. FMC RESET & GROUND FUNCTIONAL CHECKED GOOD. NO RECENT HISTORY OF FAULT.SDR ASAA2017050620659Warning Message · illuminatedALL VNAV FUNCTIONS FAILED EN ROUTE. TIME ESTIMATES, FUEL ESTIMATES, EN ROUTE WIND, AND DESCENT PLANNING ALL DISAPPEARED. THE COST INDEX ENTRY DISPLAYED EMPTY BOXES. ATTEMPTS TO REENTER THE CI GAVE REPEATED MESSAGES OF VNAV INVALID, PERF OR INVALID MOD PLAN. ASDR ASAA2017040820396Extinguisher · faultedDURING CLIMBOUT, DISCHARGED LIGHT ILLUMINATED ON FIRE PANEL. TESTED NORMAL. LIGHT EVENTUALLY WENT OUT. ACFT GROUNDED. REPLACED THE NR 1 CARGO FIRE BOTTLE.SDR ASAA2017040420365Warning Light · false activationDURING CLIMBOUT, CARGO FIRE DISCHARGE LIGHT ILLUMINATED WITH NO PILOT INPUT. ACFT GROUNDED. CARGO FIRE TESTED GOOD. ALL INDICATIONS NORMAL IAW AMM 26-23-00.SDR ASAA2017040320347Warning Light · false activationDURING PREFLIGHT, OBSERVED DISCHARGE LIGHT ILLUMINATED ON CARGO FIRE PANEL. ACFT GROUNDED. PERFORMED FIM 26-23 TASK 802. AFTER DISCONNECTING CONNECTOR FROM NR 1 BOTTLE PRESSURE SWITCH, LIGHT EXTINGUISHED. INSPECTED CONNECTOR WITH NO FAULTS FOUND. INSTALLED TSDR ASAA2017033120313Pump · failedBEING AWARE OF PREVIOUS FUEL IMBALANCE WRITE UP, WE MONITORED FUEL TANK LEVEL. AT 4 HOURS AND 10 MINUTES INTO FLIGHT AT 38,000 FEET NR 2 FUEL TANK WAS 800 LBS. LOWER THAN NR 1 TANK (LEFT SIDE). TO PREVENT A LIMIT FUEL IMBALANCE OF 1,000 LBS. WE CROSSFEED THE TSDR ASAA2017033120312Unknown · malfunctionedAT CRUISE 360 ALL FUEL PUMPS ON CENTER TANK FUEL DEVELOPED 1000 IMBALANCE ON THE RIGHT TANK. SHUT OFF RT PUMPS, BURNED OFF LEFT TO BALANCE 1 & 2 AND HAD NO FURTHER PROBLEMS. GROUNDED - YES. ACCOMPLISHED GVI AROUND EXTERNAL A/C LOOKING FOR FUEL LEAKS, NONE FOUNSDR ASAA2017021719847Warning Light · false activationAIR CONDITIONING LIGHT & RT PACK LIGHT ILLUMINATED DURING RECALL, LIGHTS GO OUT WITH RESET. ACFT GROUNDED. RAN RT PACK ON AUTO & HIGH SETTINGS. NO FAULTS INDICATED. COULD NOT DUPLICATE DISCREPANCY. OK FOR SERVICE.SDR ASAA2017011719465Engine · malfunctionedDURING ENGINE START OF THE NR 1 ENGINE. THE ENGINE N2 ROSE VERY SLOWLY AND HUNG AT 19% AT ABOUT 40 SECONDS INTO THE START. ACFT GROUNDED. PERFORMED FIM 80-05, TASK 806, ENGINE STARTED SLOW N2 ACCELERATION TO IDLE OR HUNG START WITH NO DEFECTS NOTED. VERIFSDR ASAA2017011419391Warning System · false activationAPPROXIMATELY 1 MINUTE AFTER LANDING THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED (WITH POWER AT IDLE THRUST) ENGINE WAS THEN SHUTDOWN. GROUNDED - YES. ACCOMPLISHED FIM 79-05 TASK 817 UP TO E(2)(C)1). ACCOMPLISHED REPAIR CONFIRMATION PART POWER LEAK CHESDR ASAA2017011419356Unknown · unknownENGINE START IN SJC NR 1 ENGINE N2 WAS VERY SLOW IN SPOOLING UP MAX ROTATION WAS 21.2 % AFTER APPROXIMATELY 35 SECONDS WITH START LEVER STILL IN CUTOFF. AFTER LEVER RAISED TO IDLE N2 AND N1 CONTINUED TO RISE SLOWLY BUT CONSISTENTLY ACHIEVING CUTOUT W/ NORMAL PSDR ASAA2017011319354Unknown · malfunctionedON STARTING ENGINE NR 2 IN LAS, ENG START INDICATIONS WERE VERY SLOW TO INCREASE. START PSI WAS BELOW 30 AND AT REACHING 20% N2, MOVED START LEVER TO RUN. ENGINE CONTINUED TO START BUT VERY SLOWLY. EXHAUST FUMES ENTERED AIRCRAFT DURING START. START COMPLETED WSDR ASAA2017011119326Fmc · malfunctionedLEFT FMC FAILED IN CRUISE FL 380, CHECKLIST FOLLOWED CONTINUED WITH SINGLE FMC OPS. ACFT GROUNDED. PULLED AND RESET THE NR 1 FMCS COMPUTER CIRCUIT BREAKER. TEST SUCCESSFUL IAW AMM 34-61-00-710-801. FMC OPS CHECKED NORMAL.SDR ASAA2017010919287Relay · failedAUTOPILOT NR 1 & 2 WOULD NOT ENGAGE. ACFT GROUNDED. PERFORMED DFCS BITE, IAW FIM 22-11 TASK 801, FOUND MAINTENANCE MESSAGE 22-11176. STAB TRIM RELAY ISSUE. REPLACED THE STAB TRIM RELAY R64, IAW FIM 22-13 TASK 818. ALL TESTED GOOD.SDR ASAA2016122819182Pump · failedNR 2 FUEL TANK, AFT PUMP, LOW PRESSURE LIGHT ILLUMINATED WITH SWITCH ON AND QUANTITY IN TANK READING 8.56. GROUNDED - YES. REMOVED AND REPLACED NR 2 FUEL TANK AFT PUMP WITH SERVICEABLE UNIT, REF AMM 28-22-41. OPS CHECKS GOOD, REF AMM 28-22-41.SDR ASAA2016122719173Compensator · no testWHILE ACCOMPLISHING T/C NG-28FCD-18090-1, FOUND #2 MAIN TANK FUEL TANK TOTAL TANK CAPACITANCE AND COMPENSATOR CAPACITANCE OUT OF LIMITS. GROUNDED. MIG-2C INITIATED. REMOVED AND REPLACED #2 TANK COMPENSATOR PROBE AND TANK UNITS F1,F3,F8 AND F9 IAW B737-800 AMM SDR ASAA2016122719172Compensator · no testDURING ACCOMPLISHMENT OF FUEL QUANTITY INDICATION SYSTEM, NR 1 TANK AND COMPENSATOR UNITS TESTING IAW TASK CARD NG-28FCD-18088-1, FOUND COMPENSATORS, F1, F7 AND F8 BAD. ACFT GROUNDED. REPLACED THE PROBES IAW AMM 28-41-21-000/400-801. ALL PROBES CHECKED GOOD.SDR ASAA2016122619159Control Unit · faultedWARNING LIGHT ON OVERHEAD PANEL DURING TAXING OUT. ACFT GROUNDED. SPCU FAULT ON BITE, WILL NOT CLEAR. REMOVED & REPLACED SPCU IAW AMM 24-34-11. OPS NORMAL, AFTER FAULT CLEARED.SDR ASAA2016122219161Indicator · failedFUELER REPORTED NR 1 TANK INDICATION FLUCTUATING AT WING. ACFT GROUNDED. FOUND NR 1 REFUEL PANEL FUEL QUANTITY INDICATOR BLANK. REMOVED AND REPLACED IAW AMM 28-41-61-000/400-801, OPS NORMAL.SDR ASAA2016112618808Hf Comm · malfunctionedHF 1 RADIO RECEIVES ONLY, UNABLE TO TRANSMIT. HF 2 RADIO WORKS FINE. ACFT GROUNDED. PERFORMED FIM TASK 23-11 TASK 806. PERFORMED HF COMM SYSTEM TROUBLESHOOTING GROUND VERIFICATION CHECK SUCCESSFUL. NO HISTORY PAST 30 DAYS.SDR ASAA2016112618806Transceiver · failedNR 1 HF INAUDIBLE AND EXTREMELY GARBLED AND UNUSABLE FOR RECEPTION. SEEMS TO TRANSMIT FROM EITHER CAPT OR FO PANEL. MULTIPLE FREQUENCIES WERE ATTEMPTED WITH NO IMPROVEMENT IN RECEPTION. ACFT GROUNDED. ACCOMPLISHED T/S IAW FIM 23-11 TASK 806. REPLACED NR 1 HF TSDR ASAA2016112318826Blade · wornNR 2 ENGINE, PLATFORMS WORN WITH MISSING ELASTOMERS. FAN BLADE SPACERS WORN. GROUNDED - YES. REMOVED AND REPLACE ALL 24 PLATFORMS WITH P/N 340-001-816-0 AND ALL 24 SHIMS WITH P/N 340-252-307-0 ON NR 2 ENG.SDR ASAA2016100718229Module · failedOUTFLOW VALVE POSITION INDICATOR LED POSITION DISPLAY IS INOPERATIVE. ACFT GROUNDED. REMOVED & REPLACED CABIN PRESSURE CONTROL MODULE, IAW AMM 21-31-02. OPS NORMAL.SDR ASAA2016100518219Module · malfunctionedFLT ALT SELECTOR ON OVHD PANEL IS STUCK ON 37,000 FEET. ACFT GROUNDED. REMOVED AND REPLACED CPC MODULE IAW AMM 21-31-02, ALL TESTS PASSED.SDR ASAA2016092618257Fuel Nozzle · failedAFTER SHUTDOWN NR 1 ENGINE EGT RED BOX ILLUMINATED INDICATING EGT EXCEEDANCE ON NR 1 ENGINE ON TAKEOFF. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE UPPER SEGMENT FUEL NOZZLES PER T/C PWRPL-73CMPT-07267-2.SDR ASAA2016092418128Egt Indication · reads highNR 1 ENGINE ECONOMIC FAULT FOUND DURING LL-2 CHECK ON CDU T/C MSG 73-3171 UPPER EGT SECTORS READING HIGH. ACFT GROUNDED. BITE CHECK OF NR 1 ENGINE T49.5. INSPECTED AND CLEANED EGT TEMP PROBE CONNECTORS. RING OUT OF PROBES WAS WITHIN LIMITS. INSPECTED CJ10SDR ASAA2016091918078Actuator · leakingNR 1 ENGINE RT VSV DRAIN LEAKING > 30 DPM. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 VSV ACTUATOR IAW AMM 75-31-01-000-802, AND AMM 75-31-01-400-802.SDR ASAA2016091918077Heater · leakingWHILE ACCOMPLISHING TEST 3A-LEAK CHECK ON THE NR 1 ENGINE FOR HPTCC VAVE REPLACEMENT, FOUND LEAK COMING FROM SERVO FUEL HEATER. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE SERVE FUEL HEATER IAW AMM 73-11-07-000-801-F00 & 73-11-07-400-801-F00. OPS & LESDR ASAA2016083017856Warning Light · false activationDURING AFTER START CHECKLIST ON "RECALL" LEFT PACK, ILLUMINATED - RESETS WITH MASTER CAUTION PRESSED. ACFT GROUNDED. PERFORMED PACK ZONE/TEMP CONTROLLER BITE TEST IAW AMM 21-51-00-700-803. PACK FAULT CLEARED AND DID NOT ILLUMINATE ON SECOND TESTING. CONSIDERSDR ASAA2016080517613Transceiver · failedNR 1 HF RADIO INOPERATIVE. ACFT GROUNDED. VERIFIED FAULT UNIT WOULD NOT BITE TEST. R & R HF TRANSCEIVER IAW AMM 23-11-21, GROUND VERIFICATION OK.SDR ASAA2016073117564Autoland Sys · malfunctionedDURING AUTOLAND AND HGS APPROACH SURVEY AIRCRAFT DRIFTED AND TOUCHED DOWN APPROXIMATELY 40 FEET LEFT OF CENTERLINE. CRITICAL AREA WAS CLEAR AND WINDS WERE REPORTED WITHIN LIMITS AND ND WIND DISPLAY SHOWED WINDS IN LIMIT. TOUCH DOWN OCCURRED SMOOTHLY BUT WAS NOSDR ASAA2016072117469Display · malfunctionedDURING TOUCHDOWN, FUEL READOUT IN FMC BLANKED OUT, FMC SHOWED "INSUFFICIENT FUEL" AND THE YELLOW FMC LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED BITE OF FMCS IAW FIM 34-61-00-810-801. NO FAULTS NOTED. PERFORMED OPS CHECK OF FQIS IAW AMM 28-41-00-710-801. SDR ASAA2016070917322Engine · unknownNR 1 ENGINE DID NOT LIGHT OFF DURING START. ACCOMPLISHED ABORT PROCEDURE. ACCOMPLISHED QRC. STRONG ODOR OF FUMES. ACFT GROUNDED. ACCOMPLISHED IGNITION SYSTEM AUDIBLE TEST FOR THE NR 1 ENGINE LT & RT IGNITION CHECK. BOTH LEFT AND RIGHT IGNITERS PASSED WITH NO FSDR ASAA2016052716875Keyboard · failedFLIGHT CREW REPORTS THAT THE F/O'S CDU KEYPAD IS MISSING THE O-KEY. ACFT GROUNDED. R & R F/O'S CDU KEYBOARD REF AMM 34-61-01. OPS NORMAL, GROUND VERIFCATION ACCOMPLISHED.SDR ASAA2016052516846Warning Light · false activationLEFT PACK ILLUMINATES ON MASTER CAUTION RECALL AFTER ENGINE START AND EXTINGUISHES AFTER MASTER CAUTION RESET. ACFT GROUNDED. COMPLIED WITH TEMPERATURE CONTROLLER BITE TEST IAW AMM 21-51-00-700-803, BITE CHECK RESET GOOD . OPS TEST IAW AMM TASK 21-51-00-700-8SDR ASAA2016052316834Packing · failedWHILE PERFORMING TASK CARD 78472040 FOUND FWD MAINTENANCE, AGT/TGB SPOOL VALVE INNER NOT FULLY SEALING. ACFT GROUNDED. ACCOMPLISHED TASK AMM 79-21-01-400-804-F00, OPS AND LEAK CHECKS GOOD. INNER, PN J221P019 AND OUTER PN 335-299-401-0SD, SPOOL SEALS REPLACEDSDR ASAA2016052216822Fault Code · activatedWHILE PERFORMING TASK CARD 78273000, FOUND FAULT CODE 73-31371, UPPER EGT SECTORS READING HIGH, FOR ENGINE NR 1 ECONOMIC FAULT. ACFT GROUNDED. RE-CHECKED FOR FAULT CODE 73-31371 ON NR 1 ENGINE. NO RECENT FAULTS FOUND.SDR ASAA2016041916470Fmc · malfunctionedON TAXI IN "VTK" DISPLAYED ON LEFT NAV DISPLAY, THEN CLEARED ITSELF. ACFT GROUNDED. CREW REPORTS THAT FAULT HAPPENED WHEN THEY SWITCHED POWER SOURCE FROM APU TO EXTERNAL POWER. BITE CHECK OF FMC'S REVEALS LEFT FMC FAULT ON GROUND LEG, PGM FAULT, REF FIM 34-6
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