N588AS

Service difficulty reports · 577

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 = 'N588AS' 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 ASAA2015090812980Fault Code · activatedFOUND ECONOMIC, 500 HR, FAULT ON ENG NR 2. UPPER EGT SECTORS READING HIGH. FAULT 73-21372 ON FLIGHT LEG 3. ACFT GROUNDED, ON DEFERRAL.Sep 8, 2015 · N588AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2015090812979Fault Code · activatedFOUND ECONOMIC, 500HR, FAULT ON ENG NR 1. UPPER EGT SECTORS READING HIGH. FAULT 73-11372 ON FLIGHT LEG 3. ACFT GROUNDED. ON DEFERRAL.Sep 8, 2015 · N588AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2015082812948Satcom · lockedSATCOM LOCK UP. ACFT GROUNDED. QRH CHECKLIST COMPLETED. NORMAL OPERATION RESTORED.Aug 28, 2015 · N588AS · Boeing 737890 · Communications SystemSDR ASAA2015080312708Warning Light · false activationFMC DISAGREE LIGHT ILLUMINATED ON GROUND W/ASSOCIATED SCRATCH PAD MESSAGE. ACFT GROUNDED. FOLLOWED QRH PROCEDURE FOR C/B RESET AND LIGHT, MESSAGE NO LONGER DISPLAYED.Aug 3, 2015 · N588AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015080112663Warning Message · false activationFMC DISAGREE LIGHT ILLUMINATED AFTER PUSH BACK ON GROUND, ACFT GROUNDED. FOLLOWED CHECKLIST AND MESSAGE CLEARED.Aug 1, 2015 · N588AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015071712473Unknown · unknownNR 1 ENGINE IDG REQUIRES FREQUENT SERVICING. ACFT GROUNDED. PERFORMED THE NR 1 ENGINE IDG STATIC LEAK CHECK IAW AMM 24-11-00. FOUND NO EXTERNAL LEAKS OF THE NR 1 IDG IAW. REPLACED THE IDG VENT VALVE ASSY, AND ALSO SERVICE FITTING IAW AMM 24-11-00. LEAK CHEJul 17, 2015 · N588AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2015061712121Indicator · inoperativeFUELER REPORTED CENTER TANK GAUGE NOT WORKING. ACFT GROUNDED. REPLACED REFUELING PANEL CENTER TANK QTY INDICATOR REF AMMS 28-41-61-000-801 & 28-41-61-400-801. OPS CHECK GOOD.Jun 17, 2015 · N588AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2015061612112Indicator · malfunctionedUNDERWING REFUEL PANEL CENTER TANK INDICATOR INOPERATIVE. ACFT GROUNDED. VERIFIED CENTER TANK INDICATOR INOPERATIVE. OPENED AND CLOSED C4BS. SYS RETURNED TO NORMAL OPS IAW 28-41-51. NO HISTORY IN 30 DAYS.Jun 16, 2015 · N588AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2015060712014Regulator · failedDURING CLIMBOUT, OBSERVED RT PACK PRESSURE INDICATION FLUCTUATIONS, WITH THE LT PACK INDICATION STABLE AT 32 PSI. THE RT PACK NEEDLE WAS OCCILATING BETWEEN APPROXIMATELY 37 TO 46 PSI IN CYCLES OF APPROXIMATELY 1 TO 2 SECONDS. THIS OBSERVATION STAYED CONSISTENJun 7, 2015 · N588AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2015060411985Hf Comm · malfunctionedHF1 AND HF2 BOTH SHOW INOPERATIVE ON BOTH RADIO CONTROL PANELS. ACFT GROUNDED. PERFORMED RADIO TUNING PANEL, INOPERATIVE DISPLAY TOGGLE IAW TC AMM 23-12-41-800-802. OK FOR SERVICE.Jun 4, 2015 · N588AS · Boeing 737890 · HF Communications SystemSDR ASAA2015060211951Control Panel · dimHEADING DISPLAY WINDOW ON MCP IS VERY DIM. ACFT GROUNDED. REPLACED AND TESTED MODE CONTROL PANEL REF MM 22-11-34. OPS NORMAL. PERFORMED DFCS GROUP 32, DFCS LRU INTERFACE TEST FOR MCP REF MM 22-11-34/501, DFCS GROUP NR 49, LAND VERIFY TEST, REF MM 22-11-00/Jun 2, 2015 · N588AS · Boeing 737890 · Autopilot SystemSDR ASAA2015050811656Filter · cloggedAPU OIL FILTER INDICATOR EXTENDED. ACFT GROUNDED. ACCOMPLISHED AMM TASK 49-91-13-600-801 OIL FILTER INDICATOR SERVICING. R & R LUBE FILTER ELEMENT REF AMM 49-91-12. OPS AND LEAK TEST GOOD.May 8, 2015 · N588AS · Boeing 737890 · APU Oil SystemSDR ASAA2015050311617Valve · failedON CLIMBOUT, RT DUCT PRESSURE VARIED BETWEEN 38-44, PSI AT 8000', 90.4 N1 SAME AT 13000 FEET 95 PERCENT N1. AT FL 290 RT DUCT PRESSURE STEADY AT 42 PSI 98 PERCENT, N1. ACFT GROUNDED. ACCOMPLISHED T/C NG-36WC-00001 HEALTH CHECK ON NR 2 ENGINE. FOUND HIGH STAGEMay 3, 2015 · N588AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2015042711549Engine · faultedWHILE ACCOMP T/C 78273000 FOUND NR 2 ENG ECONOMIC FAULT 73-11372, UPR EGT SECTORS READ HIGH. ACFT GROUNDED. ON DEFERRAL.Apr 27, 2015 · N588AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2015042711550Engine · faultedFOUND NR 2 ENG ECONOMIC FAULT 73-21372, UPPER EGT SECTORS READ HIGH, ESN896160. ACFT GROUNDED. ACCOMPLISHED FIM 73-11, TASK 801 DEFECT DOES NOT APPEAR ON FLT LEG ZERO. THIS CLEARS PLT.Apr 27, 2015 · N588AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2015042711543Probe · malfunctionedIN SMOOTH AIR, 2.5 HRS INTO FLT, FUEL IMBALANCE NOTICED WITH NO CONTROL INDICATION, WING NOT HEAVY ETC. FUEL QTY, 7.3, 8.3, 8.5. BALANCED FUEL NORMALLY, TOTAL FUEL QTY NORMAL AND MONITORED FOR REST OF FLIGHT. APPEARS TO BE AN INDICATION PROBLEM. DURING DESCEApr 27, 2015 · N588AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2015042211462Valve · failedCONTROLLER CAB ZONE TEMP PRIMARY CONTROLLER INOPERATIVE. ACFT GROUNDED. REPLACED CONTROLLER CAB ZONE TEMP PRIMARY CONTROLLER AS REQUIRED. LEAK CKD GOOD, OPS CKD GOOD. PERFORMED PACK/ZONE TEMP CONTROLLER BITE TEST, NO FAULTS FOUND. REF AMM 21-61-21-860-008.Apr 22, 2015 · N588AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2015041911413Control Unit · malfunctionedFUEL QTY LT MAIN FLUCTUATES BY MAX OF 700 FMC FUEL PREDICTIONS OF BELOW EXPECTED QTY'S. ACFT GROUNDED. ACCOMPLISHED FUEL TRANSFER FROM CENTER TACK TO LT WING REF MM 28-26-00-650-802. TRANSFERRED FROM LT WING TO CENTER TANK. NO FAULTS NOTED. VERY STEADY READApr 19, 2015 · N588AS · Boeing 737890 · Fuel Quantity IndicatorSDR ASAA2015040511247Indication Sys · malfunctionedRIGHT AS THE CENTER TANK WAS EMPTY, IMBALANCE SHOWED ON THE FUEL QTY INDICATOR. NR1 MAIN TANK INDICATED 6.85, NR 2 MAIN INDICATED 8.55. FOLLOWED QRH FOR CROSSFEED, AFTER CROSSFEED WAS COMPLETE NR 1 TANK INDICATIONS DID NOT DECREASE FOR AWHILE. THAN INDICATIOApr 5, 2015 · N588AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2015030510877Satcom · inoperativeSATCOM INOPERATIVE, DOES NOT APPEAR ON FMC MENU PAGE. ACFT GROUNDED. PERFORMED FIM TASK 23-15-801. SATCOM SUCCESSFULLY RESET. SATCOM RECOVERED, PROMPT, ON MCDU. OK FOR SERVICE.Mar 5, 2015 · N588AS · Boeing 737890 · Communications SystemSDR ASAA2015030110822Fault Code · activatedFOUND ECONOMIC FAULT CODE 73-31372, LEG 2 ON MCDU. UPPER EGT SECTORS READING HIGH. ACFT GROUNDED. ACCOMPLISHED FIM 73-11, TASK 801. T49.5 EGT PROBES S1 & S4 PARAMETERS READ NORMAL IN RELATION TO S2 & S3. PERFORMED EEC TEST REF MM 73-21-00-700-804-F00. NO FAUMar 1, 2015 · N588AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2015021410633Control Unit · inoperativeELECTRICAL LIGHT ILLUMINATED ON OVERHEAD PANEL. ACFT GROUNDED. ACCOMPLISHED 05-13 BITE IAW FIM 24-31 TASK 801. FOUND SPCU INOP MESSAGE. ACCOMPLISHED FIM 24-34, TASK 802. RESET SPCU AND FAULTS CLEARED. ELEC LIGHT CLEARED. OK FOR SERVICE.Feb 14, 2015 · N588AS · Boeing 737890 · DC Generating SystemSDR ASAA2015021210640Shroud · damagedDURING MAINTENANCE, FOUND NR 2 ENGINE, FUEL MANIFOLD PROTECTING SHROUDS AT 6 & 5 O'CLOCK POSITIONS DAMAGED, CRACKED. ACFT GROUNDED. R & R 2 RUBBER, SYNTHETIC MATERIAL, FUEL MANIFOLD SHROUDS. INSTALLED SAFETY CABLE IAW AMM 70-20-01. GOOD FOR SERVICE.Feb 12, 2015 · N588AS · Boeing 737890 · Engine Fuel DistributionSDR ASAA2015020110505Warning Light · illuminatedNR 1 MAIN AFT FUEL BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED. ACFT GROUNDED. OPENFeb 1, 2015 · N588AS · Boeing 737890 · Fuel Boost PumpSDR ASAA2015012610445Engine · faultedNR 1 ENGINE FOUND MESSAGE 73-31351, SHORT TIME "THE APPLIED VOLTAGE INPUT TO THE EEC IS OUT OF RANGE". FOUND DURING COMPLETION OF T/C 78273000. ACFT GROUNDED. PERFORMED INITIAL EVALUATION OF FIM 73-22, TASK 808. NO FAULTS FOUND FOR NR 1 ENGINE EEC BITE. REFJan 26, 2015 · N588AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2015012610442Probe · failedON CLIMBOUT AT APPROXIMATELY 12,000 CAPTAIN'S AIRSPEED INDICATION DROPPED TO 90 KTS IN ABOUT A 1 SECOND PERIOD, WITH A CORRESPONDING "AIRSPEED LOW" AURAL WARNING. F/O INSTRUMENTS READ NORMAL. STBY AIRSPEED READ NORMAL. PITCH AND THRUST WERE NORMAL. AFTER 1Jan 26, 2015 · N588AS · Boeing 737890 · Pitot/Static SystemSDR ASAA2015012510417Control Valve · failedTAKE OFF POWER APPLIED SUDDEN AIR SURGE FROM ACFT, DURATION 5 SEC, AT ALTITUDE SAME THING, DURATION CONTINUOUS. DUCT PSI: CLIMBOUT L35, R20. LEVEL FLIGHT 30, 28 AFTER THAT 38, 42. ACFT GROUNDED. PERFORMED FIM TASK 36-10, TASK 804 ON NR 1 ENGINE STEPS E. (16Jan 25, 2015 · N588AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2015012510415Idg · failedPAST EEP, ETOPS, SOURCE OFF LIGHT GEN 1 ILLUMINATED; FOLLOWED QRH. ACFT GROUNDED. PERFORMED NR 1 ENGINE IDG UNSCHEDULED. REMOVEL FOR CAUSE IAW AMM 24-11-11. NO CONTAMINANTS IN FILTERS. R & R NR 1 ENG IDG IAW AMM 24-11-11. OPS & LEAK CHECK GOOD.Jan 25, 2015 · N588AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2015012210402Shim · worn24 EA FAN BLADE SHIMS ON NR 1 ENG REQUIRE REPLACEMENT. ACFT GROUNDED. R & R 24 EA FAN BLADE SHIMS ON NR 1 ENG IAW TASK CARD 78472002.Jan 22, 2015 · N588AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2015012010329Sensor · reads highNR 2 ENGINE RECORDED FAULT CODE 73-31372, UPPER EGT SECTORS READING HIGH ECONOMIC FAULT. ACFT GROUNDED. RAN SYS TEST IAW MM 73-21-00-740-801. NO SYSTEM FAULT DETECTED FOR THE LAST 10 FLIGHTS. SUSPECT TO BE AND INTERMITTENT FAULT. SYSTEM OP CHECKS GOOD.Jan 20, 2015 · N588AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2015011810284Exciter · failedTRIED TO START APU FAULT LIGHT ON. FAULT CODE 49-41011. ACFT GROUNDED. REMOVED APU IGNITION UNIT IAW MM 49-41-31-000-801. INSTALLED NEW APU IGNITION UNIT IAW MM 49-41-31-400-801. APU OPS CHECKED OK. COMPLETED MM 49-41-31-400-801.Jan 18, 2015 · N588AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA2015011310255Warning Message · false activationFMC DISAGREE LIGHT ILLUMINATED WHEN ON GROUND. ACFT GROUNDED. QRH PROCEDURE COMPLETED AND LIGHT EXTINGUISHED. NORMAL OPS RESTORED.Jan 13, 2015 · N588AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014121910008Controller · malfunctionedCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED. ACFT GROUNDED. ZONE TEMP CONTROLLER 2 FAULTS FLT DECK TRIM VALVE. PERFORMED FIM 21-62, TASK 832. ZONE TEMP LIGHT EXTINGUISHED, AND ZONE TEMP CONTROLLER BITE CK GOOD IAW FIM 21-62, TASK 801. RAN PACKS, NO DEFECTS.Dec 19, 2014 · N588AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2014120909908Sensor · shortedAPU FAULT LIGHT CAME ON WHEN APU SWITCHED TO OFF. ACFT GROUNDED. ON EVALUATION, FOUND MAINTENANCE MESSAGES 49-61223, INLET TEMP SENSOR SHORT CIRCUIT, 49-91006 OVERHEAT SHUTDOWN, 49-41012 NO ROTATION SHUTDOWN, REF FIM 49-90 TASK 802, 49-60 TASK 812 AND 49-40 Dec 9, 2014 · N588AS · Boeing 737890 · APU ControlsSDR ASAA2014120809898Unknown · unknownFUEL TANKS DEVELOPED 600 LB IMBALANCE AFTER BEING BALANCED. ENGINE USE WAS NEAR EQUAL BOTH SIDES AT 6.28 & 6.30, RESPECTIVELY. ACFT GROUNDED. VERIFIED ON ACFT ARRIVAL TANKS READ -NR 1, 4.40 & NR 2, 3.83. PERFORMED PORTION OF FIM 28-41, TASK 820 FQIS BITE PRODec 8, 2014 · N588AS · Boeing 737890 · Aircraft Fuel SystemSDR ASAA2014120609876Apu · malfunctionedPRIOR TO MOVING ACFT OFF OF GATE, TURNED ON APU. APU FAULT LIGHT ILLUMINATED, APU NO START. ACFT GROUNDED. ACCOMPLISHED APU BITE IAW MM 49-60-801. NO FAULTS NOTED. GROUND VERIFICATION SUCCESSFUL.Dec 6, 2014 · N588AS · Boeing 737890 · APU Core EngineSDR ASAA2014111309676Warning Message · activatedFOUND NR 2 ENGINE FAULT 73-21372, UPPER EGT SECTORS READING HIGH - ECONOMIC FAULT. ACFT GROUNDED. ACCOMPLISHED T/C 78273000 FOUND NO FAULTS ON NR 2 ENGINE.Nov 13, 2014 · N588AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2014111209646Sensor · failedCONT CAB ZONE TEMP ILLUMINATED. QRC ACCOMPLISHED, ILLUMINATES ON RECALL. ACFT GROUNDED. PERFORMED PACK/ZONE BITE CHECK IAW AMM 21-61-00-700-806-002. FOUND A "FLT DECK DUCT SENSOR" FAULT. RETESTED AND RECEIVED THE SAME FAULT. REPLACED THE CONTROL CABIN DUCTNov 12, 2014 · N588AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2014110909628Transmitter · failedAFTER ENGINE START RT ENGINE "OIL FILTER BYPASS" LIGHT ILLUMINATED. WE SHUTDOWN AND RETURNED TO GATE. ACFT GROUNDED. REPLACED FILTER IAW 79-21-06 AMM, SCAVENGE FILTER RT ENGINE AND REPLACED FILTER TRANSMITTER RT ENGINE IAW 79-21-07 AMM. FILTER EXTINGUISHED LNov 9, 2014 · N588AS · Boeing 737890 · Engine Oil Distribution (Airframe Furnished)SDR ASAA2014102209455Control Valve · malfunctionedLEFT PACK ILLUMINATES DURING RECALL, RESETS W/MC RESET. ACFT GROUNDED. NR 1 TEMP CONTROLLER BIT & LAST FLIGHT REVIEW SHOWS "THIS PACK TCV FAULT". REPLACED LT PACK TCV WITH NEW REF: AMM 21-51-10. INTERROGATED PACK ZONE TEMP CONTROLLER AND ALL FAULTS CLEAR. REOct 22, 2014 · N588AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2014101809409Hf Comm · malfunctionedNR 1 HF RADIO WILL NOT TRANSMIT, RECIEVES OK, SAME FOR BOTH SIDES CAPTAIN & FIRST OFFICER, NR 2 OPS NORMAL. ACFT GROUNDED. NR 1 HF OPS NORMAL. COMMUNICATION & OPS TESTED GOOD, IAW MM 23-11-00, SYSTEMS TEST. READS LOUD AND CLEAR. NO HISTORY LAST 30 DAYS.Oct 18, 2014 · N588AS · Boeing 737890 · HF Communications SystemSDR ASAA2014101009348Filter · malfunctionedNR 2 ENGINE OIL BYPASS LIGHT CAME ON DURING TAXI IN. QRH PROCEDURE FOLLOWED & ENGINE SHUTDOWN DURING TAXI. ACFT GROUNDED. UNABLE TO REMOVE SCAVENGE FILTER BOWL IT IS FROZEN IN PLACE. REMOVED SCAVENGE FILTER ASSY RE AMM 79-21-04-000-801-F00. INSPECTED AFB/Oct 10, 2014 · N588AS · Boeing 737890 · Engine Oil Distribution (Airframe Furnished)SDR ASAA2014100709328Eec · faultedNR 2 ENGINE HAS EEC BITE TEST FAULT. NR 2 ENGINE MESSAGE FAULT 79-31122 OIL FILTER SIGNALS DISAGREE. ACFT GROUNDED.Oct 7, 2014 · N588AS · Boeing 737890 · Engine Oil Distribution (Airframe Furnished)SDR ASAA2014092209222Switch · faultedWHILE PERFORMING T/C 78273000, FOUND FAULT CODE 73-30311 ON NR 1 ENGINE, START SWITCH SIGNAL AND BUSS DATA DISAGREE. ACFT GROUNDED. PERFORMED FURTHER TROUBLESHOOTING IAW FIM REF 73-24, TASK 813. NO CURRENT FAULT. NUMEROUS PREVIOUS FAULTS. EEC TEST PASSED.Sep 22, 2014 · N588AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA2014091109117Fmc · malfunctionedLEFT FMC FAILED SHORTLY AFTER LEVEL OFF FOR ABOUT TEN SECONDS. THE REMAINDER OF THE FLIGHT NO PROBLEMS, FMC WORKED CONTINUOUSLY. ACFT GROUNDED. ACCOMPLISHED FIM TASK 34-61, TASK 836. CAPTAIN`S FMC OPS NORMAL.Sep 11, 2014 · N588AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014091109113Servo · failedAUTOTHROTTLES FAILED AND WOULD NOT RE-ENGAGE. TRIED BOTH AUTOPILOT`S AND FLIGHT DIRECTOR`S. DID NOTICE THAT WHEN AUTOTHROTTLES WERE ENGAGED, THE RT THRUST LEVER WOULD NOT MOVE WHILE THE LT ONE DID-AT THAT TIME THE AUTO THROTTLES WOULD DISCONNECT. ACFT GROUNSep 11, 2014 · N588AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2014082909010Indicator · trippedAPU OIL FILTER BYPASS INDICATOR POPPED, ACFT GROUNDED. PERFORMED OIL FILTER INDICATOR SERVICING REF MM 49-91-13. NO DEFECTS FOUND, NO LEAKS NOTED, OK FOR SERVICE.Aug 29, 2014 · N588AS · Boeing 737890 · APU Oil SystemSDR ASAA2014081808880Autothrottle Sys · malfunctionedAUTOTHROTTLE WILL NOT STAY ENGAGED. ACFT GROUNDED. OPENAug 18, 2014 · N588AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2014080508764Plenum · wornFOUND RT HEAT EXCHANGER AFT PLENUM WORN. ACFT GROUNDED. R & R PLENUM, IAW AMM 21-51-400-804-002.Aug 5, 2014 · N588AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2014072408683Warning Message · false activationFMC DISAGREE LT ON GROUND. ACFT GROUNDED. RESOLVED BY APPLYING QRH PROCEDURE.Jul 24, 2014 · N588AS · Boeing 737890 · Flight Management Computing Hardware System
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