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.

SDR ASAA1159612Unknown · malfunctionedA "FMC DISAGREE" WARNING IN BOTH CAPT'S AND F/O'S EHSI ON GRD WHILE TAXIING. TWO CIRCUIT BREAKERS WERE PULLED AND RESET (FMCS CMPTR 1 AND FMCS CMPTR 2 ) PER QRC CHECKLIST PROCEDURES. PULLING AND RESETTING CIRCUIT BREAKERS FIXED THE PROBLEM.May 3, 2011 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1159587Autothrottle Sys · malfunctionedAUTOTHROTTLES ADDED POWER WHEN THEY SHOULD HAVE BEEN AT IDLE . THIS OCCURRED IN A VERTICAL SPEED DESCENT AND IN VNAV PATH. PERFORMED AUTOTHROTTLE OPS TEST PER M/M 22 31 00 710 801. NO FAULTS FOUND. NO HISTORY LAST 30 DAYS. OK FOR SERVICE.May 2, 2011 · N584AS · Boeing 737890 · Auto Throttle SystemSDR ASAA1159278Computer · failedGOT "SINGLE FMC OPERATION" MESSAGE FOLLOWED BY MAP AND VTK MESSAGES ON F/O DISPLAY. FOUND RIGHT FMC INOP. ACCOMPLISHED FIM 34 61 00 FMC OPERATION RETURNED TO NORMAL. ON SWITCHING TO AIRCRAFT GENERATOR FROM APU ELECTRIC POWER GOT "SINGLE FMC OPERATION " MESSMar 19, 2011 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1159250Cdu · malfunctionedCAPTAIN'S CDU WENT BLANK DURING TAXI OUT. REMOVED AND REPLACED CAPTAIN'S MCDU PER B737 800 AMM 34 61 000 802/400 802. OPERATIONAL CHECK GOOD.Mar 16, 2011 · N584AS · Boeing 737890 · Central DisplaySDR ASAA1159235Unknown · malfunctionedRT FMC INOP. VTK SHOWS IN F/O'S DISPLAY. COULD NOT DUPLICATE. REF FIM: 34 61/801 RT FMC SENSOR CK OK AND INFLT FAULT BITE CK NML. ON RELATED FLT LEG FOUND RT FMC DATE FAULT & PGM FAULT AND NO ACTIVE FAULTS FOUND. RT FMC CK NML. NO VTX FLG. NO HISTORY 6Mar 12, 2011 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1159233Unknown · malfunctionedM CAUTION AIR COND ZONE TEMP LIGHTS (CONT CABIN) ON RECALL. ALL LIGHTS CLEAR WHEN RECALL IS RESET. COMPLIED WITH QRH. CONFIRMED NR 2 CTRLR SHOWS "FLT DECK TRIM VALVE" ON BIT & PREV FLT TESTS. VERIFY TEST PASS. RESET FAULT. FAULT DID NOT RETURN. INTERMITMar 10, 2011 · N584AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1159059Unknown · malfunctionedFUEL CROSS FEED VALVE FAILED CLOSED.PERFORMED CROSSFEED VALVE OPERATIONAL TEST COULD NOT REPLICATE DEFECT REF AMM 28 22 21 710 801. NOTE: NO HISTORY WITHIN 1 YEAR OF ANY PROBLEMS WITH CORSSFEED VALVE.Feb 19, 2011 · N584AS · Boeing 737890 · Fuel Transfer ValveSDR ASAA1158967Unknown · malfunctionedON GRD IN SAN FMC DISAGREE LIGHT CAME ON. RAN CHECKLIST LIGHT WENT OUT.Feb 4, 2011 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1058617Unknown · malfunctionedNR 2 ENGINE GENERATOR NO VOLTS NO FREQS. PERFORMED OPERATION TEST 24 11 00 IT PASSED. GROUND VERIFICATION OF NR 2 ENG GENERATOR OPS CHECK GOOD.Dec 10, 2010 · N584AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA1058469Circuit Breaker · openLEFT FORWARD OVERHEAT LIGHT (WINDOW HEAT) ILLUMINATED AT THE GATE. PERFORMED QRH PROCEDURE. OVERHEAT LIGHT RE-ILLUMINATED. FOUND C/B WINDOW HEAT PWR LEFT FRONT OPEN. CHECKED HISTORY. NO HISTORY. RESET C/B. REF CH 20 60 01. TESTED WINDOW HEAT REF MM 30 Nov 1, 2010 · N584AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA1058365Chip Detector · contaminatedWHILE ACCOMPLISHING T/C 78472040 CHIP DETECTOR INSPECTION FOUND REAR SUM MCD TO HAVE MAGNETIC PARTICLES. NR 2 ENG .163 INCH. UNABLE TO IDENTIFY MAGNETIC PARTICLES WITH THE LARGEST PARTICLE MEASURING .163 INCH. UNSATISFACTORY CONDITION PER AMM 79-00-00-200-8Oct 12, 2010 · N584AS · Boeing 737890 · Turbine Engine Accessory DriveSDR ASAA1058360Filter · defectiveFOUND LUBE FILTER HOUSING ON APU FILTER INDICATOR POPPED. ACCOMPLISHED T/C 78349013 DELTA P INSPECTION ON W/O 92909. LUBE FILTER HOUSING INDICATOR RESET FILTER CHANGED REF MM 49 91 13. FOUND NO METAL PARTICLES.Oct 12, 2010 · N584AS · Boeing 737890 · APU Oil SystemSDR ASAA1058300Pump · leakingFUEL PACKAGE LEAKING AT DRAIN NR 2 ENGINE. ACFT GROUNDED. REMOVED AND REPLACED FUEL PUMP IAW AMM 73-11-01 PERFORMED OPERTIONAL TEST NR 12-2-13-3A IAW AMM 71-00-00 TEST OKSep 22, 2010 · N584AS · Boeing 737890 · Engine Fuel PumpSDR ASAA1058200Magnetic Seal · leakingFOUND LEAKAGE FROM NR 1 ENG IDG MAGNETIC SEAL. REMOVED AND REPLACED NR 1 ENG IDG MAGNETIC SEAL PER AMM 72 60 00 400 801 F00 AND 72 60 00 000 801 F00. COMPLETED TEST 3B AMM 71 00 00 700 823 F00, LEAK CHECKS GOOD.Aug 17, 2010 · N584AS · Boeing 737890 · Turbine Engine Accessory DriveSDR ASAA1058198Idg · faultyNR 1 DRIVE LIGHT NOT ILLUMINATED DURING PREFLIGHT WITHOUT ENGINES RUNNING. LIGHTS TEST OK. REMOVED AND REPLACED NR 1 IDG IAW AMM 24 11 11 400 801. NO METAL FOUND IN FILTERS. PERFORMED OPERATIONAL TEST FOR IDG NR 1 AND FOUND OPS NORMAL.Aug 16, 2010 · N584AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA1057996Control Valve · failedON TAXI OUT NR 2 ENG N1 ON FMC TAKEOFF REF PAGE 1 SHOWED SPLIT N1 (L) 91.6 (R) 92.2 CYCLING NR 1 PACK EFFECTED CHANGE TO DISPLAYED NR 1 N1 CYCLING NR 2 PACK CAUSED NO CHANGES. REPLACED RIGHT PACK FLOW CONTROL AS PER AMM 21 51 01. LEAK CHECK GOOD. RAN ENGINEJun 20, 2010 · N584AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA1057985Connector · looseNR 1 DRIVE LIGHT NOT ILLUMINATED INTERMITTENTLY TRIPS MASTER CAUTION ELEC WHEN IT GOES OUT. CHECK AND FOUND LOOSE CONNECTOR ON NR 1 IDG. CLEANED AND RE-SECURED CONNECTOR LIGHT OP'S CHECK NORMAL. ALSO RAN BITE CHECK ON NR 1 GCU, NO FAULTS NOTED.Jun 17, 2010 · N584AS · Boeing 737890 · Electrical Power System WiringSDR ASAA1057960Window · defectiveLEFT SIDE FWD WINDOW HEAT SHOWS OVERHEAT. RESET DID NOT HELP. BITE TEST L FWD WINDOW HEAT CTRL SHOWS SENSOR FAULT SEL TO SPARE SENSOR, NO HELP. T/S TO OPEN PRI & SPARE SENSORS. REQ'S WINDOW CHANGE. REPLACED NR 1 WINDOW, OPS CHECK GOOD. OVERHEAT LIGHT DIDJun 15, 2010 · N584AS · Boeing 737890 · Flight Compartment WindowsSDR ASAA1057908O-Ring · leakingF/O REPORTS OIL STREAKS ON NR 2 ENG COWL. FOUND NR 2 ENGINE OIL CAP ASSY LEAKING AT OIL TANK. REPLACED O-RING PACKING ON OIL CAP ASSY REF MM 79 11 01 300 802 F00. RAN NR 2 ENG REF MM 71 71 00 200 801 F00, NO LEAKS NOTED.Jun 8, 2010 · N584AS · Boeing 737890 · Engine Oil Storage (Airframe Furnished)SDR ASAA1057898Actuator · out of rigLT RAM AIR INLET DEFLECTOR DOOR OUT OF RIG. ADJUSTED LT RAM AIR INLET DEFECTOR DOOR, OPS CHECK GOOD REF MM 21 51 11 400 803.Jun 5, 2010 · N584AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA1057651Oil System · lowSTARTING APU THE "MAINT" LIGHT ILLUMINATED. PERFORM BITE CHECK OF APU. CODE 49 11019 PERFORMED FIM 49 10 00 MAINT MESSAGE DID NOT REOCCUR. APU MAINT LIGHT REMAINED OFF. PERFORMED G/I OF APU AND APU OIL QUANTITY ADDED 1.0 QT. NO LEAKS DETECTED. STARTED ANApr 3, 2010 · N584AS · Boeing 737890 · APU Oil SystemSDR ASAA1057559Sensor · failedRIGHT SIDE WINDOW OVERHEAT LIGHT ON. ACCOMP'D FIM TASK 30 41 811 PRI SENSOR OPEN. SWAPPED TO SPARE SENSOR. RIGHT SIDE WINDOW HT CHECKS OK REF SAME.Mar 18, 2010 · N584AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA1057536Unknown · malfunctionedINFO ONLY: FMC DISAGREE ON GROUND PROCEDURE ACCOMPLISHED. ACCOMPLISHED FIM TASK 34 61 00 810 835. VERIFIED NO FMC FAULT MESSAGES PRESENT. NOTIFIED SEAMC MIG 51 S/N 37254 AND 37248 WAS USED.Mar 14, 2010 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1057533Autopilot Sys · malfunctionedAUTOLAND PERFORMED 'FLARE' NOT ANNUNCIATED AT 500 AFL. AUTOPILOTS DID NOT DISENGAGE AT 350 FEET. FLARE WAS ANNUNCIATED AT APPROX 100 FEET AND ACFT FLARED PROPERLY. FLT FAULT REVIEW / CURRENT STATUS LOGGED NO FAULTS. REF FIM TASK 22 11 TASK 801. LAND VERIFMar 13, 2010 · N584AS · Boeing 737890 · Autopilot SystemSDR ASAA1057509Actuator · malfunctionedTHE "A" AUTOPILOT DISENGAGES WHEN SELECTED IN COMMAND MODE (FAULT CODE 221-080-00). ACFT GROUNDED. REPLACED AUTOPILOT ELEVATOR ACTUATOR 'A' (M1020) IAW AMM 22-11-26 PAGE BLOCK 401. ACCOMPLISHED LEAKS CHECK AND AUTOPILOT ELEVATOR ACTUATOR TEST ARE GOOD.Mar 7, 2010 · N584AS · Boeing 737890 · Autopilot SystemSDR ASAA1057471Unknown · malfunctionedLEFT IDG (DRIVE) LIGHT NOT ILLUMINATED WITH ENGINE SHUTDOWN. PERFORMED ENG IDLE RUN VOLTS & FREQS NORMAL, LEFT IDG DRIVE LIGHT REMAINED ON AFTER SHUTDOWN. UNABLE TO DUPLICATE, NO HISTORY 30 DAYS. GROUND VERIFICATION CHECK GOOD. OK FOR SERVICE.Feb 27, 2010 · N584AS · Boeing 737890 · AC Indicating SystemSDR ASAA1057414Unknown · malfunctionedFMC DISAGREE LIGHT ILLUMINATED. ACCOMPLISHED QRH CHECK LIGHT, RESET OPS NORMAL.Feb 18, 2010 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0956868Warning System · malfunctionedON TAXI OUT GOT FMC DISAGREE INDICATION. PERFORMED STEPS IN QRH, OPERATION RESTORED TO NORMAL.Oct 27, 2009 · N584AS · Boeing 737890 · Central WarningSDR ASAA0956852Indicator · false indicationNR 1 ENG IDG DELTA 'P' INDICATOR POPPED. ACCOMPLISHED TASK 24 11 41 200 801 IDG SCAVENGE AND CHARGE FILTER INSP AND CHECK. FOUND BOTH FILTER CLEAN AND NO OIL DISCOLORATION OF OIL. DRAINED IDG AND REPLACED BOTH FILTERS PER TASK 24 11 41 400 801 TABLE 201 FIROct 23, 2009 · N584AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA0956818Sensor · faultyAPU FAULT LIGHT ILLUMINATED ON START AT GATE. FOUND FAULT CODE 49 61224. TROUBLESHOT TO FAULTY INLET TEMPERATURE SENSOR PER FIM TASK 49 60 00 813. REMOVED AND REPLACED APU INLET TEMPERATURE SENSOR IAW AMM 49 61 31 000 801. OPERATED APU. NO FAULTS NOTED.Oct 17, 2009 · N584AS · Boeing 737890 · APU ControlsSDR ASAA0956647Module · intermittentIN CRUISE FLIGHT APU DET INOP CAME ON WITH ASSOCIATED MASTER CAUTION. IT WOULD LIGHT UP EVERY FEW SECONDS FOR A FEW SECONDS GO OUT THEN REPEAT, APU HAS NOT BEEN ON. ACCOMPLISHED APU FIRE DETECTION OPERATIONAL TEST AND ENG/APU FIRE DETECTION CONT MODULE (M279Sep 19, 2009 · N584AS · Boeing 737890 · Fire DetectionSDR ASAA0956646Fire Warning · malfunctionedMASTER CAUTION OVERHEAT/DET APU DET INOP APU FAULT LIGHTS FLASHED ON THEN OFF 5 DIFFERENT TIMES ON FOR 1 - 2 SECONDS. PERFORMED ENG/APU FIRE DET CONT MODULE BITE PROCEDURE FIM 26 10 00 810 801 BITE TEST PASSED OK. PERFORMED APU FIRE DET, OP TEST OK PER AMM 2Sep 18, 2009 · N584AS · Boeing 737890 · Fire DetectionSDR ASAA0956393Unknown · malfunctionedWX RADAR SHOWS RETURNS (MOISTURE) WHEN NO MOISTURE WAS PRESENT ON F/O CDS/ND. FAULT CODE 344 120 32. UNABLE TO VERIFY DEFECT. PERFORMED WEATHER RADAR SYSTEM BITE PER FIM 34 43 00 810 801 INITIAL EVALUATION FOR FAULT CODE 344 120 32 PER FIM 34 43 00 810 802 Aug 11, 2009 · N584AS · Boeing 737890 · Weather Radar SystemSDR ASAA0956389Unknown · malfunctionedDURING PREFLIGHT MAP FLAG ON F/O NAV DATA DISPLAYS. CYCLED FMC C/B'S P6 1 D15 AND D16 TO REBOOT F/O'S FMC AND CDU. PERFORMED F/O'S FMC BITE PROCEDURE 34 61 00 810 801, NO FAULTS INDICATED OPS NORMAL. PERFORMED F/O'S FMC AND CAPTS FMC OPERATIONAL TEST PER MMAug 10, 2009 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0956284Alternator · faultyFOUND NR 1 ENG FAULT CODE 73 11271 (THE ALTERNATOR VOLTAGE INPUT INTO THE EEC IS OUT OF RANGE). SHORT TIME FAULT. PERFORMED FIM 73 27 00 810 F00 CHANNEL A OF NR 1 EEC ALTERNATOR FAILS RESISTANCE CHECK PER STEP F3B 86143. REMOVED NR 1 EEC ALTERNATOR AND ALTEJul 25, 2009 · N584AS · Boeing 737890 · Fuel Control/Turbine EnginesSDR ASAA0955921Fmc · malfunctionedFMC DISAGREE NOTE IN LEFT FMC SCRATCH PAD. PERFORMED FMC DISAGREE CHECK LIST OPS NORMAL. VERIFIED DEFECT INFLIGHT FAULT NR 1 LOGGED R FMC FAILURE. FOLLOWED FIM 34 61 TASK 835 GROUND VERIFCATION TEST PASSED SEAMC NOTIFIED.Jun 8, 2009 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0955870Unknown · malfunctionedAFTER TOUCH DOWN IN SEATTLE THE SPAR VALVE CLOSED LIGHT ILLUMINATED BRIGHT BLUE IN TRANSIT FOR THE NR 1 ENGINE. ENGINE RAN FINE ON TAXI IN AND SHUT DOWN NORMALLY WITH LIGHT GIVING NORMAL INDICATIONS ONCE THE START LEVER MOVED TO CUTOFF. PER MC REQUEST ACCOMPJun 6, 2009 · N584AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA0955728Warning System · malfunctionedDURING TAXI IN LEFT SPAR VALVE ILLUMINATED BRIGHT BLUE REMAINED UNTIL ENGINE SHUTDOWN CYCLED START LEVER AND LIGHT APPEAR TO OPERATE NORMALLY. PERFORMED THE NUMBER ONE ENGINE SPAR VALVE FIM TASK 28 22 00 810 809 WITH NO DISCREP FOUND, INTERM FAULT. GROUND VEMay 25, 2009 · N584AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA0955050Warning System · malfunctionedNR 1 ENG GENERATOR DRIVE LIGHT INOP. TESTS OK. BULBS REPLACED. PERFORMED FIM TASK 24 11 00 810 801. PERFORMED GCU BITE. NO FAULTS FOUND. ENG RUN BY FLIGHT CREW. GEN DRIVE LIGHT, OPS NORMAL. VERIFIED NO GCU FAULTS. NO 30 DAY HISTORY.Apr 5, 2009 · N584AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA0954435Apu · leakingAPU IS LEAKING OIL FROM THE DRAIN MAST. REF MM 49 16 11 200 801 STEP D B(4) NO OIL LEAKAGE ALLOWED FROM MIDDLE DRAIN REQ'S APU CHANGE. REMOVED AND REPLACED APU PER T/C 78349010 PARTS VERIFIED BY SEAMC, OPS & LEAK CHECK GOOD.Feb 11, 2009 · N584AS · Boeing 737890 · APU Core EngineSDR ASAA0954344Exciter · gougedNR 1 ENGINE LOWER IGNITER BOX CANNON PLUG CONNECTION POINT THREADS GOUGED. GROUNDED YES. R&R NR 1 ENG IGNITION EXCITER BOX IAW AMM 74-11-01-000-801-F00 AND 74-11-01-400-80- F00.Feb 3, 2009 · N584AS · Boeing 737890 · ExciterSDR ASAA0954342Floor Panel · crackedAFT CARGO BAY FLOOR PANEL INBD OF THRESHOLD HAS A 1 INCH CRACK APPROX STA 807. R&R PANEL.Feb 2, 2009 · N584AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA0954326Floor Panel · gougedAFT CARGO BAY NR 2 FLOOR PANEL HAS MULTIPLE DENTS AND GOUGES. REMOVED FLOOR PANEL FABRICATED NEW PANEL AND INSTALLED.Jan 31, 2009 · N584AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA0954325Floor Panel · gougedAFT CARGO BAY NR 3 FLOOR PANEL HAS MULTIPLE DENTS AND GOUGES. R&R NR 3 FLOOR PANEL.Jan 28, 2009 · N584AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA0854047Fmc · intermittentMAP FLAG VISIBLE ON F/O'S DISPLAY AND SINGLE FMC OPERATION ANNUNCIATED ON SCRATCH PAD. GROUNDED YES. PERFORMED FIM 34 61TASK801 FMC CK'S GOOD. PER SEAMC ED GROUND VERIFICATION SUCCESSFUL.Dec 14, 2008 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0853888Idg · malfunctionedNR 2 GEN DRIVE LIGHT DOES NOT ILLUMINATE REPLACED NR 2 IDG REF MM 24 11 11 400 801. OPS CKS GOOD REF MM 24 11 00 700 803 ETOPS CRITICAL PART VERIFIED BY SEAMC MARK.Nov 28, 2008 · N584AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA0853565Regulator · failedEXCESSIVE DUCT SPLIT DURING CLIMB & CRUISE FLT LT DUCT 20 RIGHT DUCT 38. ENGINES TRIMMED DURING CRUISE N1 87.7 87.7 N2 62.7 61.8 FF 2.34 2.34 THIS WAS AT CRUISE FL 400. ACCOMP ENG BLEED AIR SYS HEALTH CK NR 1 ENG REF MM 36-11-00-700-801. HIGH STAGE REG FAILOct 8, 2008 · N584AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA0853479Starter Gen · malfunctionedMAINTENANCE ANNUNCIATOR ILLUMINATED UPON APU SHUTDOWN. REPLACED STARTER GENERATOR AND STARTER POWER UNIT.Sep 7, 2008 · N584AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA0853333Cdu · failedNR 2 FMC "L2" BUTTON VERY DIFFICULT TO PRESS. REPLACED NR 2 FMCS CONTROL DISPLAY UNIT, OPS NML REF MM 36 61 01.Aug 15, 2008 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0853319Control Panel · failedNR1 HF LIGHT ILLUMINATED ON CAPTAIN`S RADIO SELECT TUNE PANEL REGARDLESS OF WHICH RADIO IS SELECTED REMOVED AND REPLACED NR1 HF VHF COMM FRQ TUNING PANEL NR1 COMM OPS CK GOOD REF MM 23 11 01.Aug 4, 2008 · N584AS · Boeing 737890 · HF Communications System
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