N584AS
Service difficulty reports · 569
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 = 'N584AS' 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 = 'N584AS' 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 ASAA2020121233687Heat Exchanger · damagedWHILE REPLACING NR 1 ENGINE FUEL PUMP PACKAGE FUEL/OIL HEAT EXCHANGER FAILED BOLT TORQUE LOCKING CHECK. GROUNDED-YES. REMOVED AND REPLACED MAIN OIL/FUEL HEAT EXCHANGER, IAW B-737-800 AMM 79-21-02-000-801-F00 AND AMM 79-21-02-400-801-F00. ACCOMPLISHED TESTS SDR ASAA2020121133688Hmu · leakingPILOT OBSERVED OIL DRIPS UNDER NR 1 ENGINE COWL. GROUNDED-YES. RUN NR 1 ENGINE AT IDLE, DID NOT OBSERVE LEAK FROM ANY DRAIN LINES, BUT LEFT SIDE OF ENGINE COWL WAS WET FROM ENGINE OIL POSSIBLE LEAK FROM HEAT EXCHANGER. FOUND HMU LEAKING ON NR 1 ENGINE. REMSDR ASAA2020121033668Modulating Valve · faultedON RECALL CONT CAB ZONE TEMP LIGHT COMES ON. GROUNDED-YES. REPLACED ZONE TRIM AIR MODULATING VALVE, REF B737-800 AMM 21-61-21-400-801. OPERATIONS NORMAL. CLEARED FAULT, REF AMM 21-61-00-700-806-002.SDR ASAA2020111933574Warning Light · false activationRIGHT PACK ILLUMINATES ON MASTER CAUTION CAUTION RECALL. RIGHT PACK EXTINGUISHES WHEN RESET. GROUNDED-YES. VERIFIED FAULT, ACCOMPLISHED ZONE TEMP CONT BITE. NR 2 CONT SHOW ACT FAULT. NR 1 SHOWS NO FAULTS. ACCOMPLISHED BITE RESET. REACCOMPLISHED ZONE TEMSDR ASAA2020102933452Processor · faultedINTERMITTENT VERIFY GW AND FUEL SWITCH PAD MESSAGE WHEN MESSAGE APPEARS FUEL ON PERF INT PAGE IS DASHES. GROUNDED-YES. MULTIPLE FUEL QTY PROCESS UNIT FAULTS LAST LEG AND MULTIPLE FLIGHTS. REMOVED AND REPLACED PROCESSOR, REF B737-800 AMM 28-41-81/401. OPERASDR ASAA2020102533415Autothrottle Sys · malfunctionedAUTOTHROTTLE WILL NOT ENGAGE. GROUNDED-YES. PERFORMED A/T OPERATIONS TEST, IAW B737-800 AMM 22-31-00-710-801 AND SYSTEM TEST IAW AMM 22-31-00710-802. NO FAULTS NOTED. ALL TESTS PASS. PERFORMED LAND VERIFY TEST, IAW AMM 22-11-00-710-801. NO FAULTS FOUND.SDR ASAA2020102133400Fmc · failedRT FMC FAIL. GROUNDED-YES. REFERENCE B737-800 FIM 34-61 TASK 836 CYCLED CB TO RT HAND FMC. RT HAND FMC RECOVERED.SDR ASAA2020101633362Autothrottle Sys · malfunctionedAUTOTHROTTLE WON'T ENGAGE. GROUNDED-YES. PERFORMED AUTOTHROTTLE BITE, PER B737-800 FIM 22-31 TASK 801. NO CURRENT FAULTS. FOUND FAULT CODE 22-31543. PERFORMED FIM 22-31 TASK 830 WITH NO FAULTS. PERFORMED AUTOTHROTTLE SYSTEM TEST, PER B737-800 AMM 22-31-0SDR ASAA2020072433926Control Panel · malfunctionedFO'S COURSE MCP WINDOW INOPERATIVE. GROUNDED - YES. F/O MCP CRS WINDOW INOPERATIVE. ACCOMPLISHED MCP TEST IAW 22-11-34, NO FAULTS.SDR ASAA2020072722941Connector · corrodedNR 2 ENGINE B SIDE FIRE LOOP WILL NOT TEST. GROUNDED - YES. PERFORMED FIM 26-10, TASK 810. BITE CHECK SHOWS FAULTED ENGINE 2 LOOP B LOW DETECTOR RESISTANCE. CLEANED CONNECTIONS. PERFORMED RESISTANCE CHECK ON ALL FIRE LOOPS ALL RESISTANCE WITHIN LIMITS. FSDR ASAA2020072082908Sensor · failedR2 WINDOW OVERHEAT LIGHT, EXTINGUISHED FOR MOST OF THE FLIGHT THEN ILLUMINATED AGAIN ON DESCENT THROUGH 8,000. SAT WAS 13'C AT 8000'. GROUNDED - YES. ACCOMPLISHED WHCU BITE IAW FIM 30-41 TASK 801. BITE SHOWS R2 WINDOW SENSOR FAULT LIGHT. ACCOMPLISHED RT WINDSDR ASAA2020072082906Director · faultedCAPT FLIGHT DIRECTOR FAILED. AFTER ABOUT AN HOUR, IT WAS INTERMITTENT, ALONG W/ MACH TRIM FAIL LIGHT. GROUNDED - YES. FCC 'A' LOGGED SEVERAL INTERNAL FAULTS LAST LEG, R & R SAME PER B737-800 AMM 22-11-33. SYS OPS CKS NML PER SAME, LAND VERIFY PASS AND FLT DIR SDR ASAA2020071632901Module · faultyRT SIDE WINDOW OVERHEAT LIGHT CAME ON DESCENDING THRU 10,000 FT INTO ANC. COMPLETED CHECKLIST, LIGHT STAYED OUT/ OPERATED NORMALLY FOR REMAINDER OF FLIGHT. GROUNDED - YES. RT SIDE WINDOW CONTROLLER SHOWS P5-9 CONTROL FAULT. REPLACED OVERHEAD P5-9 MODULE PESDR ASAA2020071232894Warning System · false activationR2 WINDOW OVERHEAT ILLUMINATED DURING DESCENT GROUNDED - YES. APPLIED QRH PROCEDURE RESET SUCCESSFUL.SDR ASAA2020031332417Unknown · malfunctionedHF2 COMM PANEL SHOWS "FAIL" IN FREQ SELECTOR WINDOWS. GROUNDED - YES. PERFORMED B737-800 FIM 23-11 TASK 803. OP CK NORMAL.SDR ASAA2020031232407Warning System · false activationCONT CAB ZONE TEMP LIGHT ILLUMINATED WITH RECALL. GROUNDED - YES. ACCOMPLISHED OPS CK OF FLT DECK (CONT) TRIM VALVE PER B737-800 AMM 21-51-00. NO DEFECTS NOTED. ACCOMPLISHED BITE CK OF BOTH CONTROLLERS PER AMM 21-61-00. NO FAULTS. ALL CK OK.SDR ASAA2020030332335Turbine Nozzle · crackedWHILE ACCOMPISHING T/C 78472022 (SDI BORESCOPE ENGINE HPT BLADE) FOUND 1 LPT NOZZLE WITH 1 FULL CRACK, 1 RADIAL CRACK THAT INTERSECTS WITH THE F00000NOPARTULL CRACK, A HOLE IN HTE LPT NOZZLE WHERE THE CRACKS INTERSECT, AND AIRFOIL MATERIAL LIFTING OFF FWD OF TSDR ASAA2020030232338Actuator · leakingON WALKAROUND NOTICED FUEL DRIPPING FROM #1 ENG COWL. GROUNDED - YES. OPENED #1 ENG FAN COWL. RAN #1 ENG FOR FIVE MINUTES. NOTICED LEFT VSV DRAIN LEAKING AT 3 DROPS/MIN AND HPTCCV AT 4 DROPS/MIN REF B737-800 AMM 71-71-00-200-801 F00. REMOVED LEFT VSV ACTR AND SDR ASAA2020020522080Control Valve · inoperativeLEFT PACK LIGHT ILLUMINATES OM MC RECALL. RESETS W/MC RESET. GROUNDED - YES. BITE OF M1442 ZONE TEMP CONTROLLER #1 FAULTS "TCV THIS PACK" REF B737-800 FIM 21-62 TASK 830. REPLACED TCV V139. INSTALLATION TEST PASSES, NO LEAKS NOTED REF B737-800 AMM 21-51-10-400SDR ASAA202002032062Lens · detachedFA REPORTS THAT CEILING EXIT SIGN AT WING EXITS FELL OFF. GROUNDED - YES. INSPECTED LIGHT FIXTURE AND LIGHT LENS ASSEMBLY. FOUND NO DEFECTS. REINSTALLED LIGHT LENS ASSY AS REQUIRED. OPS NORMAL.SDR ASAA2020012733962Motor · inoperativeLEFT MAIN FWD FUEL PUMP "LOW PRESSURE" LIGHT ON. GROUNDED - YES. REMOVED AND REPLACED L/H FWD FUEL BOOST PUMP REF B737-800 AMM 28-22-41. OPS AND LEAK CHECK NORMAL. GROUND VERIFICATION COMPLETE.SDR ASAA2020012171914Lens · detachedEXIT LENS MISSING AT AFT DIVIDER BY GALLEY (LEFT SIDE). GROUNDED - YES. INSTALLED EXIT LENS MISSING. REF B737-800 AMM 33-51-01. GRD CHECK OK.SDR ASAA2020010631790Engine · damaged#2 ENGINE SN-892792 AFT SIDE OF THE J-HOOK STAGE 3 VSV T/E @ 12 O'CLOCK HAS MISSING MATERIAL REF T/C CMPT-72EO-02015-3 GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE PER SHOP WO 1038123SDR ASAA20191231734Lens · detachedCENTER AISLE EXIT SIGN AT 16 ROW FELL OFF. GROUNDED - YES. REINSTALLED PLASTIC EMERGENCY EXIT SIGN COVER - NO OTHER DEFECTS NOTED. LIGHT OPS NORMAL.SDR ASAA2019123061718Heater · inoperativeR ELEV PITOT LIGHT CAME ON DURING TAXI TO THE RUNWAY. GROUNDED - YES. REF B737-800 FIM 30-31-TASK 809, DISCONNECTED D638 CONNECTOR & INSPECTED PINS NO DEFECTS NOTED, REINSTALLED CONNECTOR R ELEV PITOT LIGHT REMAINS ON. REPLACED RH ELEV PITOT PROBE REF B737-800SDR ASAA2019121953623Window · overheatedWINDOW HEAT LEFT SIDE OVERHEAT. GROUNDED - YES. ON DEFERRAL.SDR ASAA2019121633609Warning Light · false activationCLIMBING THROUGH FL210, LEFT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. GROUNDED - YES. FOLLOWED QRH 3.5 PROCEDURES. LIGHT EXTINGUISHED AND REMAINED OFF.SDR ASAA2019121633608Warning Message · false activationLEFT SIDE WINDOW HEAT OVERHEAT LIGHT ILLUMINATED ON GROUND. CYCLED SWITCH PER QRH 3.5 SYSTEM RESET GOOD. GROUNDED - YES. CONFIRMED FAULT, WHC SHOWS SENSOR FAULTS. ACCOMPLISHED "RESISTANCE CHECK WINDOW TEMPERATURE SENSORS" REF B737-800 AMM 30-41-21-760-801, BOTSDR ASAA201912131591Blade · damagedDURING ACCOMP #1 ENG S/N 894857 T/C 78472010 FAN LUBE FOUND MISSING CU NI COATING ON BLADES #7, #9, #12. GROUNDED - YES. REMOVED AND REPLACED #7, #9, AND #12 FAN BLADES ON #1 ENGINE AND PAIR BLADES #24, #19, AND #21 REF T//C #78472010SDR ASAA2019120423500Lens · detachedEXIT SIGN AT ROW 17 AISLE OVERHEAD -LENS FELL OFF. GROUNDED - YES. REATTACHED LENS COVER PER B737-800 AMM 33-51-01.SDR ASAA201912031492Starter · making metal#2 ENGINE N1 ROTATION STOPPED AT 20% AND THEN ROLLED BACK. START VALVE REMAINED OPEN AFTER SECOND ATTEMPT (N1 DIDN'T MAKE IT PAST 17% ON 2ND ATTEMPT). GROUNDED - YES. OPENED FAN COWLS #2 ENG REF B737-800 AMM 71-11-02-410-806-F00 USING ALT DEACTIVATION TABLE 3,SDR ASAA201912031491Start Valve · inoperativeWHEN PERFORMING IDLE POWER TEST ON #2 ENGINE START VALVE LIGHT REMAINED ON AND BLINKED. GROUNDED - YES. REMOVED AND REPLACED #2 ENG STARTER VLV REF B737-800 AMM TASK 80-11-03/401. START VALVE TEST AND TEST #1 (PNEUMATIC LEAK CHECK) FROM POWER PLANT TEST REFERESDR ASAA2019111841347Autoland Sys · malfunctionedAUTOLAND APPROACH SURVEY NOT SUCCESSFUL APPROACH MODE DISCONNECTED APPX 500 FT AGL. GROUNDED - YES. NO FAULTS LOGGED LAST FLIGHT DFCS CHANNEL A & B DFCS LAND VERIFY CHANNEL A & B GRP 49 BITE CKS NORMAL. FCC REPLACEMENT TEST GRP 35 BITE CKS NORMAL HGS NO FAULT SDR ASAA201911131317Lens · detachedEXIT SALIDA DIRECTIONAL SIGN FELL OFF IN MID CABIN. GROUNDED - YES. REATTACHED EXIT ROW SIGN PER B737-800 AMM 33-51-01.SDR ASAA2019102173064Sign · detachedMID CABIN CEILING EMERGENCY EXIT SIGN HAS HAD A PIECE FALL OFF. GROUNDED - YES. RESECURED EMERGENCY EXIT SIGN LENS.SDR ASAA2019102153128Warning Light · false activationZONE TEMP LIGHT ILLUMINATED ON RECALL FOR CONT CAB ON AIR CONDITIONING PANEL OVERHEAD. GROUNDED - YES. PERFORMED BITE TEST OF ZONE TEMP CONTROLLER #1, CURRENT FAULT SHOWS FLT DECK TRIM VALVE REF B737-800 AMM 21-61-00. RESET CONTROLLER, NO CURRENT FAULTS SHOWN,SDR ASAA2019101753126Lens · detachedFRONT PART OF EXIT SIGN MISSING ABOVE ROW 16-17. GROUNDED - YES. REPLACED MISSING FRONT PART OF EXIT SIGN ABOVE ROW 16-17 WITH NEW EXIT SIGN LENS REF. AMM 33-51-01.SDR ASAA2019092630838Idg · failedRIGHT TRANSFER BUS OFF LIGHT ILLUMINATED TWICE IN FLIGHT, ACCOMPANIED BY M/C LIGHT. ILLIMUNATION WAS A HALF SECOND BOTH TIMES, NOT ACCOMPANIED BY ANY OTHER INSTRUMENT INDICATION. FIRST TIME WAS AT CRUISE. SECOND TIME WAS DURING DESCENT. GROUNDED - YES. REMOVEDSDR ASAA2019092530823Warning System · false activationTRANSFER BUS OFF LIGHT #2 BEGAN TO FLICKER JUST AFTER TOP OF DESCENT TO JFK, IT WAS ALWAYS A VERY QUICK FLASH AND CAUSED THE MASTER CAUTION TO FLASH AS WELL. NO OTHER SYSTEMS SEEMED TO BE AFFECTED AND THE BUS SEEMED TO REMAINED POWERED CONTINUOUSLY. THE INTERMSDR ASAA2019091330699Trim Motor · failedAFTER DEPARTURE ELECTRIC TRIM INOP ON BOTH CONTROL COLUMNS. ENGAGED AUTOPILOT PER QRH & STAB OUT OF TRIM LIGHT ILLUMINATED. GROUNDED - YES. AIR TURNBACK. DIVERSION TIME 51 MINUTES - VERIFIED DEFECT, ACCOMPLISHED FIM 27-41 TASK 804 VERIFIED 115VAC ON D700 PINS SDR ASAA2019083130582Unknown · malfunctionedHF 2 SHOWS FAIL IN BOTH ACTIVE AND STANDBY FREQUENCY. GROUNDED - YES. PERFORMED FIM TASK 23-11 TASK 801, FOR HF #2 RADIO, NO DEFECTS NOTED.SDR ASAA2019081423385Warning Light · false activationON MASTER CAUTION RECALL AFTER START CHECKLIST GOT A MACH TRIM FAIL LIGHT. AS PER QRH IT DID RESET ON SUBSEQUENT RECALL. GROUNDED - YES. CYCLED SHIPS POWER. ACCOMPLISHED DFCS BITE REF B737-800 FIM TASK 22-11 TASK 801. CURRENT STATUS PASSED MACH TRIM A AND B PASDR ASAA2019072930245Unknown · malfunctionedFMC FAIL AND VTK FLAG UPON LANDING OF F/O SIDE. GROUNDED - YES. PERFORMED FIM 22-11 TASK 812. NO FAULTS FAULTS AFTER TEST,BITE CK. PER STEP D SUB TASK [B] AN INTERMITTENT FAULT OCCURRED & CLEARED. NO FAULTS /FLAGS AFTER FIM 22-11 TASK 812. AIRCRAFT OK FOR SERVSDR ASAA2019072230136Unknown · malfunctionedAUTOLAND FAILED. APPCH WARN AND R/O CTN AT 80' RA. GROUNDED - YES. A/P CURRENT STATUS IS OK REF FIM TASK 22-11 TASK 801.SDR ASAA2019061629737Computer · failedFOUND FAULT CODE 22-11235 A SYSTEM FAULT, THIS AFFECTS THE A SYSTEM AUTOPILOT. GROUNDED - YES. ATTEMPTED TO APPLY 22-1F, FOUND ALTITUDE ALERT TO BE AFFECTED. NO ER OPS ALLOWED FOR THAT MEL. FCC A HAS FAILED AND REQUIRES REPLACEMENT. REMOVED AND REPLACED FCCA RSDR ASAA2019051929406Lens · unsecureEXIT SIGN FELL OFF AT ROW 16 CENTER AISLE. GROUNDED - YES. REINSTALLED COVER ASSY OK FOR SERVICE.SDR ASAA2019051229290Unknown · malfunctionedR1 WINDOW OVERHEAT LIGHT ILLUMINATED ON GROUND. DOES NOT RESET PER QRH. GROUNDED - YES. RESET A/C WINDOW HEAT C/B ON P18 PANEL. IAW SWPM 20-60-00. R1 WINDOW HEAT OPS CHECK GOOD.SDR ASAA2019042489113Floor Support · corrodedFWD PASS COMPT FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 294.5 AND STA 312 AT LB 12 HAS CORR ON UPPER SURFACE. GROUNDED - YES. REMOVED,DRILLED, LOCATED AND INSTALLED NEW INTERCOSTAL IAW BDWG #141A5600 W 1" O .080" R 0.0" L 6" D .080".SDR ASAA2019040988934Floor Support · crackedPASSENGER COMPARTMENT FLOOR STA 312 - STA 328 RBL 31 INTERCOSTAL CRACKED ON UPPER SURFACE GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL AT PASSENGER FLOOR STA 312 - STA 328 RBL 31 IAW B737-800 SRM 51-40-02-0G-0SDR ASAA201904290152Floorbeam · corrodedPASSENGER COMPARTMENT FLOOR 986.5 FLOOR BEAM UPPER SURFACE CORRODED AT FASTENER HOLE GIRT BAR FITTING. GROUNDED - YES. REPAIRED 986.5 FLOOR BEAM UPPER SURFACE HOLE GIRT BAR FITTING IAW ALASKA EA: 800-53-EA-21508W=1.5" O=.150 R=.110 L=2.0" D= .040.
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