N586AS

Service difficulty reports · 485

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 = 'N586AS' 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 ASAA2016020115291Channel · crackedAFT CARGO COMPARTMENT RT ZEE CHANNEL SIDEPLATE CRACKED AT SEVERAL FRAME LOCATIONS FROM BS 727G-BS767, RBL 21.0, BS 727G - BS 767, RBL 21.0 - RBL 21.0, STR 25R-STR 25R. ACFT GROUNDED. ACCOMPLISHED AFT CARGO COMPARTMENT RT ZEE CHANNEL SIDEPLATE REPAIR FROM BS 7Feb 1, 2016 · N586AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016020115290Floor Panel · corrodedFWD CARGO COMPARTMENT FLOOR PANEL 120DF HAS CORROSION AROUND EDGE. ACFT GROUNDED. REMOVED CORROSION PANEL 120DF FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. FABRICATED NEW FLOOR PANEL 120F IAW 453A2610, REV B APPLIED ALODINE AND PRIMER TO PANEL 120DF IAW SRM Feb 1, 2016 · N586AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2016020115275Floorbeam · corrodedFWD CARGO COMPARTMENT AFT BULKHEAD LOWER FLOOR SUPPORT ANGLE CORRODED BS 500I, RBL 21 - LBL 21. ACFT GROUNDED. REMOVED CORROSION FWD CARGO BULKHEAD LOWER FLOOR SUPPORT ANGLE BS500 ORIGINAL MATERIAL THICKNESS WAS .071 LOST .016 REMAINING IS .055 FOUND TO BE OFeb 1, 2016 · N586AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2016012414983Warning Message · false activationFMC DISAGREE ANNUNCIATED AFTER PUSH BACK. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMCS RESTORED NORMAL.Jan 24, 2016 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016012014935Warning Message · false activationDATALINK FULL ALERT MESSAGE ON CDU. COMPLETED QRH PROCEDURE IAW FLIGHT HANDBOOK. ACFT GROUNDED. ACCOMPLISHED FIM 34-61, TASK 839. OPS NORMAL.Jan 20, 2016 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016011414829Warning Message · false activationON GROUND, FMC DISAGREE LIGHT. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMCS RESTORED NORMAL.Jan 14, 2016 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016010814703Engine · faultedIAW T/C 78273000, FOUND NR 1 ENGINE WITH ECONOMIC FAULT 73-31371. UPPER EGT SECTORS READING HIGH. ACFT GROUNDED. ON DEFERRAL.Jan 8, 2016 · N586AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2016010614643Exciter · failedAPU HAS HISTORY OF NO STARTS. ACFT GROUNDED. R & R IGNITER PLUG, IGNITER PLUG LEAD AND EXCITER IGNITER UNIT IAW AMM 49-41-15, 49-41-52, 49-41-31.Jan 6, 2016 · N586AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA2015122914552Apu · faultedFAULT LIGHT ON APU ATTEMPTED START IAW QRH FAULT LIGHT EXITING. LESS THAN 5 MINUTES ATTEMPTED ANOTHER START, ANOTHER NO START, WITH FAULT LIGHT. ACFT GROUNDED. PERFORMED FIM APU BITE CHECK, IAW MM 49-60-801. FAULT CODE 49-41011 DISPLAYED NO FLAME SHUTDOWN, Dec 29, 2015 · N586AS · Boeing 737890 · Airborne Auxiliary Power Unit (APU) SystemSDR ASAA2015122214358Fuel Nozzle · failedFOUND NR 2 ENGINE W/ ECONOMIC FAULT 73-31372, UPPER EGT SECTORS READ HIGH. ACFT GROUNDED. ACCOMPLISHED T/C POWER REPLACED-73 COMPARTMENT-07267-2. REPLACED MAIN ENGINE FUEL NOZZLES. ECONOMIC FAULT 73-31372, CLEARED.Dec 22, 2015 · N586AS · Boeing 737890 · Fuel Injector NozzleSDR ASAA2015122114378Wire Harness · damagedNR 2 ENGINE RT UPPER FIRE WARNING HARNESS TERMINAL END AT FIRE LOOP IS BROKEN. ACFT GROUNDED. R & R NR 2 ENGINE CORE FIRE DETECTION HARNESS MW0326, REF AMM 26-11-02. OPS NORMAL REF AMM 26-11-00.Dec 21, 2015 · N586AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2015120114065Satcom · lockedSATCOM LOCKUP. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. SATCOM RESTORED NORMAL.Dec 1, 2015 · N586AS · Boeing 737890 · Communications SystemSDR ASAA2015112413969Warning Light · false indicationELECTRIC ANNUNCIATOR LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED FIM 24-31, TASK 801, ELECTRIC FAULT CLEARED.Nov 24, 2015 · N586AS · Boeing 737890 · Central WarningSDR ASAA2015100513343Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. RAN QRH. OPS NORMAL.Oct 5, 2015 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015093013287Warning Light · false activationELEC WARNING LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED ELECTRONIC LIGHT BITE PROC REF FIM 24-31, TASK 801. LOGGED SPCU INOPERATIVE MSG. PERFORMED FIM 24-34, TASK 802 & FAULT CLEARED. DRD FUNCTIONAL TEST PASSED. NO HISTORY OF FAULT LAST 30 DAYS.Sep 30, 2015 · N586AS · Boeing 737890 · Central WarningSDR ASAA2015090912989Sign · detachedFRONT HALF OF MID CABIN EXIT SIGN FELL OFF. ACFT GROUNDED. REINSTALLED MID CABIN SIGN, EXIT.Sep 9, 2015 · N586AS · Boeing 737890 · Emergency LightingSDR ASAA2015090612960Fault Code · activatedWHILE ACCOMPLISHING TASK CARD 78273000, INTEROGATE THE FMC CDU FOR ENGINE FAULTS, FOUND ECONOMIC FAULTS: 73-31371, UPPER EGT SECTORS READING HIGH, 73-31372, UPPER EGT SECTORS READING HIGH. ACFT GROUNDED. RE-ACCOMPLISHED T/C 78273000 FMC CDU ENGINE INTERROGATSep 6, 2015 · N586AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2015080812764Warning Light · false activationON RECALL, LEFT PACK LIGHT ILLUMINATED. LIGHT OUT WHEN MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED BITE CHECK ON BOTH TEMP CONTROLLERS. LEFT TEMP CONTROLLER LOGGED TCV FAULT. FAULT REST, ON TEMP CONTROLLER LEFT TEMP CONTROLL GROUND VERIFICATION CHECKAug 8, 2015 · N586AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2015080212682Display · failedWHILE TAXIING TO THE GATE THE CAPTAIN'S CDU WENT BLANK. ACFT GROUNDED. R & R LT CDU REF MM 34-61-01, OPS CHECK NORMAL.Aug 2, 2015 · N586AS · Boeing 737890 · Central DisplaySDR ASAA2015080212677Control Valve · failedLEFT PACK LIGHT ILLUMINATED, DOES NOT GO OUT WITH TRIP RESET. ACFT GROUNDED. R & R NR 1 PACK TCV IAW AMM 21-51-10, OPS AND LEAK CHECK GOOD.Aug 2, 2015 · N586AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2015073112661Display · malfunctionedCA CDU SCREEN FAILED. ACFT GROUNDED. CYCLED NR 1 MCDU CIRCUIT BREAKER. NR 1 FMC AND CDU OPS CHECKED GOOD IAW MM 20-60-01 AND 34-61, TASK 835.Jul 31, 2015 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015072812614Controller · malfunctionedLT PACK LIGHT ILLUMINATED ON MASTER CAUTION RECALL, GOES DARK ON RESET. ACFT GROUNDED. PERFORMED BITE TEST NR 1 TEMP CONTROLLER, RESET CONTROLLER. OPS CHECKED NORMAL, REF TASK 21-61-00-700-806-002. NO HISTORY LAST 30 DAYS.Jul 28, 2015 · N586AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2015072612607Engine · sparksWHILE POWERING UP TO TAKE RUNWAY FOR TAKEOFF, ANOTHER ACFT OBSERVED SPARKS AND/OR FLAMES COMING FROM NR 1 TAILPIPE. ALL ENGINE INDICATIONS WERE NORMAL WITH NO FIRE INDICATIONS. ACCOMPLISHED ENGINE TAILPIPE FIRE CHECKLIST. NO FURTHER SPARKS OF FLAMES OBSERVJul 26, 2015 · N586AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2015072612598Start Valve · failedSTART VALVE FAILED TO CLOSE ON NR 1 ENGINE START. ACFT GROUNDED.Jul 26, 2015 · N586AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA2015072112508Probe · out of limitsNR 1 ENGINE TREND DATA SHOWS INCREASE IN EGT AND A DECREASE IN EGT HOT DAY MARGIN. ACFT GROUNDED. ACCOMPLISHED NR 1 ENGINE EGT SYSTEM INSPECTION, REF 77-21-01. FOUND S1 AND S4 OUT OF LIMITS IAW TABLE C. REPLACED EGT PROBES S1 AND S4 IAW 77-21-01. PERFORMEJul 21, 2015 · N586AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2015071912507Actuator · damagedDURING REMOVAL OF CONNECTOR DP1002, FOUND RUBBER ISOLATOR FOR PINS DAMAGED ON VSV ACTUATOR, NR 1 ENGINE. ACFT GROUNDED. REMOVED LT VSV ACTUATOR IAW AMM 75-31-01-000-801-F00, INSTALLED SERVICABLE LT VSV ACTUATOR IAW AMM 75-31-01-400-801-F00.Jul 19, 2015 · N586AS · Boeing 737890 · Compressor Bleed ControlSDR ASAA2015071912506Circuit Breaker · trippedENGINE 1 ALTN POWER CHANNEL A CIRCUIT BREAKER FOUND POPPED ON PREFLIGHT. ACFT GROUNDED. CHECKED C/B PANEL, RESET C/B, PREFORMED FIM 73-00, TASK 801, NO FURTHER PROBLEMS, OPS GOOD, REF MM 20-60-01. PERFORMED GROUND VERIFICATION TEST IAW MM 73-21-00-700-804-FJul 19, 2015 · N586AS · Boeing 737890 · AC Power Distribution SystemSDR ASAA2015071812489Wire Harness · damagedNR 1 ENGINE EGT SHOWED HIGH TEMPERATURE EXCEEDANCE. ON TAKEOFF, APPROXIMATELY 1000 DEGREES FOR A FEW SECONDS. AUTO THROTTLES WERE ON ENGINE OPERATED NORMALLY AFTER THAT EVENT. AT CRUISE NR 1 ENGINE TEMPERATURE SHOWED 30 DEGREES HIGHER THAN NR 2 ENGINE. ACFJul 18, 2015 · N586AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2015071412442Warning Light · false activationPRIOR TO TAKEOFF IN FMC DISAGREE LIGHT BOTH SIDES. ACFT GROUNDED. QRH PROCEDURE UTILIZED. LIGHT EXTINGUISHED. CONTINUE NORMAL OPS.Jul 14, 2015 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015061112076Light · inoperativeFWD LEFT EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. R & R THE EMERGENCY LIGHT. OPS CHECKED GOOD IAW AMM 33-51-04.Jun 11, 2015 · N586AS · Boeing 737890 · Emergency LightingSDR ASAA2015060511990Circuit Breaker · trippedGENERATOR NR 1 DISC CIRCUIT BREAKER TRIPPED. ACFT GROUNDED. CHECKED HISTORY. NO HISTORY 90 DAYS. RESET CIRCUIT BREAKER ON P6-4 GENERATOR DISC 1, IAW WDM 24-11-11 AND MM 20-60-01. RAN NR 1 ENGINE AND OPS TESTED DISCONNECT FOR NR 1 IDG. OPS NORMAL. RESET IJun 5, 2015 · N586AS · Boeing 737890 · Alternator-Generator DriveSDR ASAA2015060311956Warning Light · false activationRIGHT PACK LT ILLUMINATED DURING CLIMB IAW QRH RESET. ACFT GROUNDED. PERFORMED PACK ZONE TEMP CONTROLLER BITE TEST. NO FAULT FOUND. GROUND VERIFICATION COMPLETE REF AMM 21-61-00. NO HISTORY LAST 30 DAYS.Jun 3, 2015 · N586AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2015042411488Warning Message · false activationFMC DISAGREE ON GROUND. GROUNDED - YES. COMPLETED QRH CHECKLIST. FMC DISAGREE MSG NO LONGER DISPLAYED.Apr 24, 2015 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015042211467Engine · fault messageWHILE ACCOMP T/C 78273000, FOUND NR 2 ENG WITH ECONOMIC FAULT 73-31372, UPPER EGT SECTORS READ HIGH. ACFT GROUNDED. ACCOMPLISHED T/C 78273000. NO FAULTS LOGGED.Apr 22, 2015 · N586AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2015041611390Engine · malfunctionedDURING START OF NR 2 ENGINE, NO FUEL FLOW AND EGT WHEN START LEVER PLACED TO IDLE. NR 2 ENGINE RT IGNITION C/B DISCOVERED OPEN. ACFT GROUNDED. INSPECT NR 2 CB FOR DEFECTS NO DEFECTS NOTE. RESET CC IAW AMM 20-60-01-860-801. PERFORMED AMM TASK 74-00-00-750-8Apr 16, 2015 · N586AS · Boeing 737890 · Ignition Power SupplySDR ASAA2015041511363Transceiver · failedNR 1 HF INCOMING COMMS GARBLED AND UNREADABLE. OUTGOING TRANSMISSIONS WORK FINE. TRIED TUNING & DETUNING SEVERAL FREQUENCIES WITH NO CHANGE. PREFLIGHT HF NR 1 CHECK HAD ALL COMMS NORMAL. HF NR 2 WORKS PERFECTLY. ACFT GROUNDED. REMOVED AND INSTALLED NR 1 HF Apr 15, 2015 · N586AS · Boeing 737890 · HF Communications SystemSDR ASAA2015040911304Probe · faultedDIAGNOSTIC REPORTS NR 1 ENGINE TREND DATA SHOWS A SHIFT IN CRUISE AND TAKEOFF MARGIN INDICATIVE OF EGT INDICATION ERRORS. ACFT GROUNDED. WHILE COMPLYING WITH TC 78273000 FOUND ECONOMIC FAULT 77-20861 ON ENGINE 1ESN894921. READINGS OF ENGINE NR 1 T49.5 PROBEApr 9, 2015 · N586AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2015040111203Satcom · lockedSATCOM APPEARS TO BE LOCKED UP. ACFT GROUNDED. REBOOTED SATCOM SYS REF FIM 23-15-00-23-801. NO HISTORY 30 DAYS. GROUND VERIFICATION GOOD.Apr 1, 2015 · N586AS · Boeing 737890 · Communications SystemSDR ASAA2015012610444Panel · looseNR 1 ENGINE, INLET FAN DUCT PANEL NR 8 HAS LOOSE FASTENERS. ACFT GROUNDED. RETIGHTENED FASTENERS REF AMM 72-23-07-000-801-F00.Jan 26, 2015 · N586AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2015012010327Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. QRH COMPLIED WITH OPS NORMAL.Jan 20, 2015 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015012010326Fmc · malfunctionedAT TOP OF CLIMB, 34000, CAPTAIN'S FMC'S SCREEN WENT BLACK, AFTER A FEW SECONDS IT RETURNED TO NORMAL OPERATIONS AFTER A START UP TEST SCREEN. ACFT GROUNDED. PERFORMED FIM TASK 34-61 TASK 801 NO DEFECTS NOTED NO HISTORY LAST 30 DAYS. ACFT OK FOR SERVICE.Jan 20, 2015 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014122510066Radio · malfunctionedNR 1 HF RADIO FREQUENCY DISPLAY READS "FAIL/FAIL". RADIO TUNES AND TRANSMIT, RECEIVES NORMAL. AFTER 10 SECONDS FAIL WARNING APPEARS. ACFT GROUNDED. RESET NR 1 HF AND NR 2 HF, PERFORMED BITE CHECK PROCEDURE. NO FAULTS NOTED, NO FAIL INDICATED, REF AMM FIMDec 25, 2014 · N586AS · Boeing 737890 · HF Communications SystemSDR ASAA2014121109934Bleed Valve · failedBLEED TRIP OFF LIGHT LT SIDE CAME ON CLIMBING THROUGH ABOUT 20,000'. RESET PROCEDURES IAW QRH UNSUCCESSFUL. DUCT PRESSURE 0 PSI LT SIDE. ACFT GROUNDED. ACCOMPLISHED FIM 36-10, TASK 801. REPLACED NR 1 PCCV IAW AMM 36-12-02. OPS CHECK NORMAL. R & R NR 1 PCCDec 11, 2014 · N586AS · Boeing 737890 · Compressor Bleed ValveSDR ASAA2014121109921Autothrottle Sys · malfunctionedAUTOTHROTTLES ARMED FOR TAKEOFF, AUTOTHROTTLES DISCONNECTED AND BOTH FD MASTER LITES ILLUMINATED WHEN TOGA BUTTON WAS PUSHED. ACFT GROUNDED. ACCOMPLISHED DFCS BITE CHECK IAW FIM 22-11, TASK 801 FOUND IRU DATA INVALID IN HISTORY. NO CURRENT FAULTS. ACCOMPLIDec 11, 2014 · N586AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2014120109846Warning Message · false activation"DATALINK FULL" MESSAGE ON GROUND. ACFT GROUNDED. ACCOMPLISHED QRH. OPS NORMAL.Dec 1, 2014 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014112809783Shim · wornR 2 ENGINE FOUND ALL FAN BLADE SHIMS EXHIBIT MORE THAN 25 PERCENT MOLYDAG COATING IAW MM 72-21-02-200-801, STEP 2. L, 1, B, 1. ACFT GROUNDED. REPLACED ALL SHIMS ON NR 2 ENG FAN BLADES, REF T/C 78472002.Nov 28, 2014 · N586AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2014112309731Controller · failedNOTICED RAPID EAR PRESSURE CHANGE, CABIN CLIMB GAUGE WAS PEGGED AT NO AUTO FAIL LIGHT LIGHT. OUTFLOW VALVE INDICATOR WAS SHOWING FULL CLOSED. DURING DESCENT BELOW ABOUT 18000 FT, CABIN ALTITUDE WAS GOING BELOW SEA LEVEL. AT THIS TIME WE MOVED PRESS CONTROLLNov 23, 2014 · N586AS · Boeing 737890 · Cabin Pressure ControllerSDR ASAA2014112209737Probe · failedDIAGNOSTICS REPORTED NR 1 ENGINE TREND DATA SHOWED A SHIFT IN DELTA CRUISE AND TAKEOFF MARGIN INDICATIVE OF EGT INDICATION ERRORS. ACFT GROUNDED. T49.5 S2 PROBE HIGH RESISTANCE. REPLACED S2 PROBE IAW MM 77-21-01, EEC TEST PASS. EGT SYS INSPECTION NORMAL REF Nov 22, 2014 · N586AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2014112209727Shim · wornNR 1 ENGINE, FAN BLADE SHIM WORN AND DAMAGED. ACFT GROUNDED. R & R FAN BLADE SHIM IAW TC 78472002.Nov 22, 2014 · N586AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2014112209726Blade · wornFOUND CU-NI-IN COATING MISSING, CHIPPED MORE THAN AREA Y ON NR 1 ENGINE FAN BLADES: NR 1 , 7 , 11, 12, 13, 19, 23, 24, REF MM 72-21-02-200-801-FOO AND T/C 78472003, AND FAN BLADE NR14 HAS WEAR FROM SHIM IN AREA G MEASURED AT .0095 WITH SMARTSCOPE. ACFT GROUNNov 22, 2014 · N586AS · Boeing 737890 · Turbine Engine Air Inlet Section
Back to N586AS