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 ASAA2013040994433Circuit Breaker · trippedNR 2 ENG SPAR VALVE CIRCUIT BREAKER IS OUT. ACCOMPLISHED CIRCUIT BREAKER RESET PROCEDURE REF MM 20-60-01, NO DEFECTS NOTED. ACCOMPLISHED NR 2 ENGINE FUEL SPAR VALVE ELECTRICAL CONTROL AND INDICATION TEST REF MM 28-22-00-710-801 PARA 4.C.1-2 (N). ALL VOLTAGEApr 9, 2013 · N584AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA2013031394162Filter · cloggedAPU OIL FILTER INDICATOR EXTENDED. R & R OIL FILTER ELEMENT, SERVICED APU, REF AMM 49-91-13-600-801. LEAK CK GOOD.Mar 13, 2013 · N584AS · Boeing 737890 · APU Oil SystemSDR ASAA2013012693751Valve · inoperativeBLEED TRIP OFF ILLUMINATED ON LT SIDE AS THROTTLES BROUGHT BACK TO IDLE TOP OF DESCENT. ACCOMPLISHED FIM 36-10, TASK 801 & ENG BLEED AIR SYS HEALTH CHECK. FOUND HIGH STAGE VALVE & PRECOOLER CONTROL VALVE FAULTS. R & R HIGH STAGE VALVE REF MM 36-11-06 & PRE Jan 26, 2013 · N584AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2013011193644Shim · wornNR 1 ENGINE TREND DATA SHOWS A SUDDEN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. CHECKED INLET AND EXHAUST FOR EVIDENCE OF FOD IAW MM 71-00-00-800-802. ACCOMPLISHED NR 1 ENGINE FAN LUBE IAW TASK CARD 78472002. INSPECTED ALL PLATFORM SEALS AND HARDWAREJan 11, 2013 · N584AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2012113093391Fmc · failedRT FMC FAILED. ACCOMPLISHED FMCS BITE INFLIGHT FAULT SHOWED FMC RT FAIL. R & R RT FMC IAW AMM 34-61-02, SYS GROUND FUNCTION TEST NORMAL.Nov 30, 2012 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012112893379Idg · malfunctionedNR 1 ENGINE IDG DELTA P INDICATOR POPPED. ACCOMPLISHED FIM TASK 24-11 TASK 803. R & R THE NR 1 IDG IAW AMM 24-11-11. FLUSHED THE OIL CIRCUIT IAW AMM 12-13-21. OPS CHECK OF THE IDG WAS GOOD IAW 24-11-00.Nov 28, 2012 · N584AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2012112193340Warning Light · false activationELECRICAL LIGHT ILLUMINATED AFTER ENGINE START. PERFORMED GROUND VERIFICATION TEST TEST PASSED PERFORM BITE PROCEDURE ALL FAULTS CLEARED. ACFT OK FOR CONTINUE SERVICE. NO HISTORY REF FIM TASK 24-31-801.Nov 21, 2012 · N584AS · Boeing 737890 · Indicating/Recording SystemSDR ASAA2012103193217Warning Message · false indicationFMC DISAGREE MESSAGE RECEIVED ON TAXI OUT. ACCOMPLISHED QRH PROCEDURE. CLEARED WARNING MESSAGE.Oct 31, 2012 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012100793044Valve · failedNR 1 ENGINE ANTI-ICE COWL VALVE OPEN LIGHT BRIGHT BLUE WITH SWITCH ON. REPLACED NR 1 ENGINE COWL ANTI-ICE VALVE REF MM 30-21-11 VALVE, OPS CHECKED GOOD & LEAK CHECKED GOOD.Oct 7, 2012 · N584AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2012090892841Transceiver · failedPWS FAIL LIGHT ILLUMINATED. WEATHER RADAR HAS VERTICAL SPIKES PAINTED. TILT APPEARS OFF. REPLACED WEATHER RADAR TRANSCEIVER. OPS CHECKED GOOD IAW MM 34-43-00-710-802-001.Sep 8, 2012 · N584AS · Boeing 737890 · Weather Radar SystemSDR ASAA2012090692839Control Unit · inoperativeAMBER LIGHT ILLUMINATED ON AC/DC PANEL. PERFORMED BITE TEST SPCU INOPERATIVE, ERROR CODE INDICATED. CLEARED FAULT, FAULT LIGHT EXTINGUISHED. INTERMITTENT FAULT. REF FIM 24-31-00. ACFT OK FOR SERVICE. OPS NORMAL.Sep 6, 2012 · N584AS · Boeing 737890 · Electrical Power SystemSDR ASAA2012092392933Fmc · failedLEFT FMC FAILED. REMOVED AND REPLACED THE LT FMC. CROSSLOADED SOFTWARE FROM RT FMC. FMC OPS NORMAL.Sep 2, 2012 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012091192867Transceiver · failedPWS FAIL LIGHT ILLUMINATED. REMOVED RADAR RT 34-43-41-000-801. INSTALLED RADAR RT 34-43-41-400-801. PERFORMED INSTALLATION TEST REF 34-43-41 STEP F. SYS CKS NML.Sep 1, 2012 · N584AS · Boeing 737890 · Weather Radar SystemSDR ASAA2012082192757Filter · trippedNR 1 ENGINE IDG DELTA P POPPED. ACFT GROUNDED. ACCOMPLISHED IDG DIFFERENTIAL PRESSURE INDICATOR FAULT ISOLATION TASK IAW FIM TASK 24-11-00. OPS CHECK GOOD.Aug 2, 2012 · N584AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2012070392461Sensor · malfunctionedAPU FAULT LIGHT ILLUMINATED. TWO RESTARTS WERE ATTEMPTED AFTER FIVE MINUTE INTERVALS IAW ATTEMPT. AFTER EACH ATTEMPT WITH APU SWITCH OFF, FAULT LIGHT EVENTUALLY EXTINGUISHES. R & R MAIN & AUXILIARY BATTERIES. ACCOMPLISHED OPC CHECK OF MAIN AUXILIARY BATTERIJul 3, 2012 · N584AS · Boeing 737890 · APU ControlsSDR ASAA2012071292534Indicator · activatedNR 1 ENG IDG FILTER INDICATOR EXTENDED. ACFT GROUNDED. REPLACED IDG NR 1 SCAVENGE AND CHARGE FILTERS, PLACARD. LEAK CHECKED GOOD. REF AMM 24-11-41.Jul 1, 2012 · N584AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA12511507Unknown · unknownAFTER 3 HRS OF FLIGHT A AUTOPILOT DISENGAGED SMOOTH AIR. RE-ENGAGED AND WORKED NORMALLY FOR DURATION OF FLIGHT. ACFT GROUNDED. DFCS A LOGGED MSG 22-11-607 MCP DATA INVALID. FOLLOWED FIM 22-11, TASK 817. ALL TEST PASSED. ACCOMPLISHED LWMP CHECKS REF CHECKLIMay 5, 2012 · N584AS · Boeing 737890 · Autopilot SystemSDR ASAA12511476Fmc · malfunctionedFMC DISAGREE LIGHT ILLUMINATED ON TAXI. ACFT GROUNDED. ACCOMPLISHED FMC RESET PROCEDURE IAW FIM 34-61-00-810-835, NO FAULTS NOTED.Apr 28, 2012 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA12511478Fuel Control · malfunctionedWHILE PERFORMING TC 78273000, FOUND FUEL CONTROL 73-10321, HMU FMV CONTROL CURRENT IS OUT OF RANGE. SHORT TIME FAULT NR 1 ENG. ACFT GROUNDED. REPLACED NR 1 ENG EEC IAW AMM 73-21-60-000-801 F00 AND 73-21-60-400-801 F00. PERFORMED TESTS LISTED IN THE POWER PApr 27, 2012 · N584AS · Boeing 737890 · Fuel Control/Turbine EnginesSDR ASAA12511376Metering Valve · out of tolerancePERFORMED T/C 7827300 ON NR 2 AND NR 1 ENGINES NR 1 ENGINE HAD FAULT CODE 73-10321. THE HMU FUEL METERING VALVE CONTROL CURRENT IS OUT OF RANGE. PERFORMED EEC TEST PER FIM 73-25-00-810-801-F00, FAULT NO LONGER ACTIVE EEC TEST PASSES FOR NR 1 ENGINE.Apr 9, 2012 · N584AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA12511374Idg · oil consumptionNR 1 ENGINE IDG BE REPLACED FOR HISTORY OF OIL CONSUMPTION. REMOVED AND REPLACED NR 1 ENG IDG REF MM 24-11-12.Apr 7, 2012 · N584AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA12511301Control Panel · faultyAIRSPEED KNOB WORKS INTERMITTENTLY. REMOVED AND REPLACED DFCS MODE CONTROL PANEL REF MM 22 11 34. INSTALLATION TEST PASSED.Mar 27, 2012 · N584AS · Boeing 737890 · Autopilot SystemSDR ASAA12511294Unknown · malfunctionedPERFORMED TASK CARD 78273000 ENG FMC CDU FAULT FOUND MAINT MSG 76 31361 START LEVER SIGNALS DISAGREE NR 1 ENG. AT 50 HOUR RE CHECK NO FAULTS WERE FOUND. PERFORMED T/S FOR FAULT 76 31361 PER FIM 76 11 00 810 801 F00 ACCOMPLISHED INITIAL EVALUATION SEVERAL TIMMar 24, 2012 · N584AS · Boeing 737890 · Engine Indicating SystemSDR ASAA12511290Filter Element · defectiveACCOMPLISHED TASK CARD 78349013 "APU OIL FILTER DELTA P INDICATOR" FOUND BYPASS BUTTON POPPED. REQUIRES OIL FILTER INDICATOR SERVICING REF AMM 49 91 13 600 801. ACCOMPLISHED AMM 49 91 13 OIL FILTER INDICATOR SERVICING. FILTER ELEMENT REPLACED NO CONTAMINATIMar 24, 2012 · N584AS · Boeing 737890 · APU Oil SystemSDR ASAA12511235Unknown · malfunctionedINFO ONLY FMC DISAGREE MESSAGE ON GRD. ACCOMPLISHED QRH. OPS NORMAL.Mar 12, 2012 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA12511192Spinner · damagedNR 1 ENG REAR SPINNER CONE AFT EDGE (AT FAN BLADE NR 11) HAS DAMAGE ALONG INTERFACE WITH BLADE PLATFORM (MARKED). REMOVED AND REPLACED NR 1 ENGINE REAR SPINNER CONE REF B737NG AMM 71 21 01.Mar 8, 2012 · N584AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA12511160Unknown · malfunctionedFMC DISAGREE ON GROUND. ACCOMPLISHED QRH PROCEDURE. NORMAL OPERATION RESTORED.Feb 27, 2012 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA12511140Bolt · looseNR 1 ENG FAN DUCT PANEL AT 4:00 POS (UPPER CTR BOLT) AND 10:00 POS (LWR AFT BOLT) FASTENERS LOOSE. (FINDING DURING C/W T/C 78472000) RE-TORQUED BOLT AT 4:00 POS (UPPER CTR BOLT) RE-TORQUED BOLT AT 10:00 POS (LWR AFT BOLT) REF M/M 72 23 07, OK FOR SVC.Feb 22, 2012 · N584AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA12510940Unknown · malfunctionedAFTER START CHECKLIST DURING RECALL GOT "CONT CAB" "ZONE TEMP" LIGHT. DOES RESET WITH MASTER CAUTION. BITE CHECK GOOD REF AMM 21 61 00. SYSTEM VERIFIED WORKING.Jan 13, 2012 · N584AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA12510947Window · defectiveLEFT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED, FOLLOWED QRH PROCEDURES. TURNED WINDOW HEAT ON, LIGHT ILLUMINATED AGAIN. CONTINUED FLIGHT WITH WINDOW HEAT OFF. ACCOM WINDOW HEAT CNTRL UNIT BITE TEST PER FIM TASK 30 31 00 810 801. FOUND FLT P5 9/ CNTRL POWER LJan 12, 2012 · N584AS · Boeing 737890 · Flight Compartment WindowsSDR ASAA12510872Valve · malfunctionedLEFT BLEED TRIP OFF LIGHT ILLUMINATED ON DESCENT. WOULD NOT RESET. COMPLETED FIM 36 10 00 810 801 A THRU E(2). BLEED TRIP RESET SUCCESSFUL ON GROUND. CREW STATED DESCENT FROM 38 000 FEET LEFT PACK TRIPPED WAITED 1:30 MIN TRIED TO RESET NO GOOD. DUCT PRESSDec 30, 2011 · N584AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA11510869Sensor · defectiveLT SIDE WINDOW OVHT LIGHT ILLUMINATED DURING PREFLIGHT. PERFORMED BITE CHECK OF LT SIDE WHCU. FOUND LT SIDE SENSOR FAULT. PERFORMED FIM TASK 30 41 00 810 811. ON LT SIDE WINDOW SWAPPED SENSOR TO SPARE SENSOR. SYSTEM OPS CHECK NORMAL PER AMM 30 41 00 710 8Dec 28, 2011 · N584AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA11510864Wire Harness · defectiveDURING CRUISE FLIGHT 4 HOURS AFTER TAKEOFF LEFT SIDE WINDOW HEAT AMBER OVERHEAT OCCURRED. QRH FOLLOWED. OVERHEAT CONDITION WOULD NOT RESET. PERFORMED WINDOW HEAT CONTROL UNIT BITE CHECK NO ACTIVE FAULTS FOUND. HISTORICAL FAULT LT SIDE WINDOW SENSOR SHOWN. CDec 27, 2011 · N584AS · Boeing 737890 · Ice/Rain Protection System WiringSDR ASAA11510800Unknown · malfunctionedAFTER ENGINE START FMC DISAGREE LIGHT ON. PERFORMED QRH PROCEDURE FAULT CLEARED.Dec 14, 2011 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA11510740Transceiver · faultyON T/O ROLL PWS FAIL /WXR FAIL ILLUMINATED ON BOTH ND'S. REPLACED WEATHER RADAR RT UNIT REF MM 34 43 41 000 801 AND 400 801. GROUND VERIFIED CHECKED GOOD REF 34 13 00 710 802 0011.Dec 2, 2011 · N584AS · Boeing 737890 · Weather Radar SystemSDR ASAA11510739Drive Unit · faultyON T/O AT 500' PWS FAIL ILLUMINATED ON BOTH ND'S. DEBRIEFED CREW ALSO REPORTED THAT THE BLUE "ANT" LIGHT WAS ILLUMUNATED. "ANT" LIGHT DID GO OUT. REPLACED ANTENNA DRIVE UNIT REF MM 34 43 11, OPS CHECKS GOOD REF MM 34 43 00.Dec 2, 2011 · N584AS · Boeing 737890 · Weather Radar SystemSDR ASAA11510734Valve · faultyLEFT BLEED TRIP OFF LIGHT ILLUMINATED. QRH TRIP RESET PROCEDURE SUCCESSFUL. REPLACED NR 1 ENG HIGH STAGE REGULATOR PER MM 36 11 07, NO HELP. ACCOMPLISHED ENG BLEED AIR SYSTEM HEALTH CHECK ON NR 1 ENG PER MM 36 11 00. FOUND HIGH STAGE VALVE BAD. REPLACED NNov 30, 2011 · N584AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA11510595Unknown · malfunctionedNR 1 ENGINE IDG DPI IS POPPED. EXAMINED THE SCAVANGE/CHARGE FILTER CONDITION AND OIL CONDITION AND FOUND TO BE GOOD. DPI WAS RESET.Oct 28, 2011 · N584AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA11510585Regulator · malfunctionedAT FL 410 LEFT PACK "BLEED TRIP OFF" LIGHT CAME ON. RESET & LIGHT WENT OUT PER QRH. NORMAL PRESSURE RESTORED. FIVE MINUTES LATER LIGHT CAME BACK ON & AGAIN RESET & STAYED OUT. PRESSURE 30 PSI BOTH SIDES WERE THE SAME. REPLACED LT ENGINE BLEED AIR REGULATOOct 25, 2011 · N584AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA11510582Unknown · malfunctionedFMC DISAGREE ON GROUND IN SAN. ACCOMPLISHED QRH PROCEDURE. LIGHT EXTINGUISHED. OPS NORMAL.Oct 25, 2011 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA11510545Pump · malfunctionedLEFT CTR FUEL PUMP LT ILLUMINATED WITH PUMP ON AND FUEL IN CTR TANK. RESET LEFT CENTER BOOST PUMP C/B PER MM 20 60 01. NO FAULTS NOTED. GROUND VERIFICATION SUCCESSFUL.Oct 18, 2011 · N584AS · Boeing 737890 · Fuel Boost PumpSDR ASAA11510544Stator · defectiveWHILE ACCOMPLISHING TASK CARD 78273000 ENGINE NR 2 LOGGED SHORT TIME FAULT CODE 73 21272 (THE ALTERNATOR VOLTAGE INPUT TO THE EEC IS OUT OF RANGE.) PERFORMED FIM TASK 73 27 00 810 804 F00 ALTERNATOR VOLTAGE INPUT TO THE EEC IS OUT OF RANGE. AT STEP F3 FOUND Oct 16, 2011 · N584AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA11510517Unknown · malfunctionedON TAXI OUT FMC DISAGREE LIGHT ILLUMINATED. ACCOMPLISHED QRH AND FMC DISAGREE LIGHT ON BOTH ND'S EXTINGUISHED.Oct 15, 2011 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA11510486Eec · faultyABORTED START NR 1 ENG ALL PARAMETERS NORMAL BUT NO EGT RISE. QRC AND QRH PROCEDURES ACCOMPLISHED. START ATTEMPTS WERE ON IGN R LT ENG STARTS NORMAL ON IGN L. SWAPPED POWER SUPPLIES TO LT ENG EXCITERS NO FIX NO AUDIBLE ON IGN R. RESTORED TO ORIGINAL REF 74Oct 7, 2011 · N584AS · Boeing 737890 · Fuel Control/Turbine EnginesSDR ASAA11510407Warning System · false activationAT FL 300 AFTER USING WING ANTI ICE HAD A L BLEED TRIP LIGHT ILLUMINATE. PERFORMED QRH LIGHT EXTINGUISHED. ACCOMP FIM 36 10 00 810 801 STEPS F (1) (2) (B) AND STEPS F (3) (7) NO DEFECTS NOTED. PER TABLE ON PAGE 5 WTAI AT CRUISE CAN CAUSE BLEED TRIP.Sep 22, 2011 · N584AS · Boeing 737890 · Pneumatic Indicating SystemSDR ASAA11510381Unknown · malfunctionedWXR STAB LIGHT ILLUMINATED IN FLIGHT. NO FAULTS LOGGED. VERIFIED RADAR CONTROL PANEL SETTINGS. RADAR BITE CHECK OP CK & ANTENNA TILT CHECK NORMAL. REF MM 34 42 00 810 801 34 43 00 710 802 001 1 & 34 43 00 730 802 001 1.Sep 17, 2011 · N584AS · Boeing 737890 · Weather Radar SystemSDR ASAA11510380Unknown · malfunctionedFMC DISAGREE LIGHT ILLUMINATED DURING TAXI OUT. PERFORMED QRH PROCEDURE. OPS CHECK NORMAL.Sep 16, 2011 · N584AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA11510336Filter Element · defectiveCLOGGED FILTER INDICATION BUTTON POPPED OUT ON APU LUBE OIL FILTER. REPLACED CLOGGED FILTER INDICATOR FILTER BOWL BOTH OIL FILTER NO MATERIAL OR DEBRIS IN FILTER OR ON MAGNETIC CHIP DECTOR OPS AND LEAK CK OK REF AMM 49 91 13 600 801, OK FOR SERVICE.Sep 2, 2011 · N584AS · Boeing 737890 · APU Oil SystemSDR ASAA11510319Unknown · malfunctionedNR 2 ENG GENERATOR DRIVE LIGHT IS NOT ILLUMINATED BULB TESTS GOOD. UNABLE TO DUPLICATE RESISTANCE CHECKED AT DP1206 PRESSURE SW NO DEFECT NOTED REF WDM 24 11 21. RAN ENG DRIVE LIGHT, OPS NORMAL.Aug 27, 2011 · N584AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA1159915Unknown · malfunctionedTR 3 CIRCUIT BREAKER OUT. FOUND TR 3 DC IND C/B ON P 5 OUT. ACCOMPLISHED C/B RESET PROCEDURE REF AMM 20 60 01. GROUND OPS VERIFICATION CHECKS GOOD REF AMM 24 32 11.Jun 22, 2011 · N584AS · Boeing 737890 · DC Generating System
Back to N584AS