N558AS
Service difficulty reports · 535
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 = 'N558AS' 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 = 'N558AS' 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 ASAA2015010910202Warning Message · false activationFMC DISAGREE, ON THE GROUND. ACFT GROUNDED, QRH ACCOMPLISHED SUCCESSFULLY.SDR ASAA2015010610160Valve · failedDURING RECALL, CONTROLLER CABIN ZONE TEMP LIGHT ILLUMINATED. ACFT GROUNDED. R & R CONTROLLER CABIN TRIM AIR MODULATING VALVE IAW AMM 21-61-21-000-801/-400-801. OPS AND LEAK CKS GOOD.SDR ASAA2015010610169Warning Message · false activationFMC DISAGREE ALERT MESSAGE RECEIVED ON THE GROUND. ACFT GROUNDED. CLEARED BY ACCOMPLISHING THE QRH PROCEDURE. NO HISTORY LAST 30 DAYS. NO FURTHER ACTION.SDR ASAA2015010510154Radar · malfunctionedCAPTAIN`S SIDE RADAR DISPLAYS TWO TARGETS AT 10:00 O'CLOCK AND 2:00 O'CLOCK. GREEN PERIMETERS, YELLOW INTERRIDES AT ALL DISTANCE, NO ACTUAL CB OR WEATHER IS PRESENT. F/O'S SIDE DOES NOT DISPLAY THE NONEXISTENT TARGETS. MAINTENANCE & DISPATCH NOTIFIED VIA ACSDR ASAA2015010110125Satcom · lockedSATCOM LOCKUP ON GROUND. ACFT GROUNDED. ACCOMPLISHED QRH 5.300 PROCEDURE, SATCOM OPS NORMAL.SDR ASAA2014120409866Warning Light · false activationCOCKPIT ZONE TEMP LIGHT ILLUMINATES ON RECALL, GOES OUT WITH MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED CAB TEMP CONTINUED BITE FIM 21-62 TASK 801, NR 2 CONTROLLER FAULTED CONT CAB TRIM VALVE. FAULT WAS CLEARED ON RESET AND OPS CHECKED NORMAL AMM 21SDR ASAA2014111509662Bracket · brokenRIGHT RAM AIR EXHAUST DUCT DIFFUSER BRACKETS BROKEN. DIFFUSER IS UNSECURED. ACFT GROUNDED. R & R RT RAM AIR EXHAUST DIFFUSER DUCT LK & OPS NORMAL REF MM 21-51-03.SDR ASAA2014110909626Light · inoperativeMCP LIGHTS INOPERATIVE. ACFT GROUNDED. VERIFIED DISCREPANCY. CYCLED POWER TO MCP, PANEL RETURNED TO NORMAL. GROUND VERIFICATION AND LWMP TESTS ARE SUCCESSFUL REF MM 22-11-34 GRP 32, 22-11-0 GRP 49 LAND VERIFY AND HGS SYS AND SENSOR TEST 34-36-0 SSM. ACFT REMASDR ASAA2014110809620Charger · inoperativeRIGHT AFT OVERWING EXIT BATTERY PACK DISCHARGED. ACFT GROUNDED. R & R OVERWING EXIT BATTERY CHARGER IAW MM 33-51-06.SDR ASAA2014110809614Charger · inoperativeOVERWING EXIT BATTERIES DISCHARGED. ACFT GROUNDED. R & R BATTERY CHARGER IAW MM 33-51 06.SDR ASAA2014110809613Battery Pack · inoperativeR1 EMERGENCY LIGHT BATTERY PACK WILL NOT CHARGE. ACFT GROUNDED. R & R BATTERY PACK IAW MM 33-51-06, OPS NORMAL.SDR ASAA2014090609067Warning Light · illuminatedDURING CRUISE FLT, BLUE ENGINE VALVE CLOSED LIGHT ILLUMINATED . NO OTHER LIGHTS OR ABNORMAL INDICATIONS. LIGHT EXTINGUISHED WHEN ALTITUDE WITH INCREASE POWER CHANGE. ACFT GROUNDED. AS A PRECAUTION REPLACED THE FUEL SYS MODULE, OPS CHECKED GOOD IAW MM 28-22SDR ASAA2014090409068Warning Light · illuminatedDURING CRUISE, WAS NOTIFIED ENGINE VALVE CLOSED, LIGHT ILLUMINATED BRIGHT BLUE ON NR 2 ENGINE WITH ENGINE RUNNING NORMAL AND ALL INDICATION NORMAL, THE LIGHT EXTINGUISHED AFTER 5 MINUTES. ACFT GROUNDED. COULD NOT DUPLICATE. AS A PRECAUTION, REPLACED NR 2 SDR ASAA2014082908998Idg · failedNR 1 GENERATOR DRIVE LIGHT ILLUMINATED FOR SEVERAL SECONDS. ACFT GROUNDED. REPLACED NR 1 IDG, OPS CHECKED GOOD, IAW AMM 24-11-11.SDR ASAA2014082809003Warning Message · false activationDURING TAXI TO DEPART, THE FMC DISAGREE MESSAGE DISPLAYED. ACFT GROUNDED. QRH PROCEDURE CLEARED MESSAGE.SDR ASAA2014082708975Oil System · lowDURING DESCENT, NR 1 GENERATOR DRIVE LIGHT CAME ON AND WENT OUT THREE TIMES. NR 1 GENERATOR VOLTS, FREQUENCIES, AND CYCLES WERE NORMAL. ACFT GROUNDED. INSPECTED AND FOUND NR 1 IDG OIL LEVEL LOW, SERVICED IDG TO FULL IAW AMM 12-13-21. PERFORMED ENGINE RUN ASDR ASAA2014082208926Oil System · lowDURING TAXI, NR 1 DRIVE LIGHT ILLUMINATED AND STAYED ON. ACFT GROUNDED. FOUND OIL LEVEL LOW, SERVICED IDG AS PLACARDED REF MM 12-13-21. RAN ENGINE TWICE. ACCOMPLISHED OPS TEST FOR THE NR 1 IDG IAW AMM 24-11-00-700-802, VOLTS 115, FREQ'S. 399. INDICATION WSDR ASAA2014080908796Start Valve · failedDURING START OF NR 2 ENGINE , NR 2 START VALVE LIGHT REMAINS ILUMMINATED AFTER START. ACFT GROUNDED. REPLACED NR 2 ENGINE START VALVE IAW AMM 80-11-03. OPS AND LEAK CHECKED GOOD. START VALVE INDICATION CHECKED GOOD. GROUND VERIFICATION GOOD IAW AMM 71-00-0SDR ASAA2014080508762Control Module · failedDURING CRUISE AT 37000 FT, AUTO FAIL LIGHT ILLUMINATED. RAN QRH & SWITCHED TO ALTERNATE. ALL PRESSURIZATION INDICATES NORMAL. ACFT GROUNDED. CONFIRMED FAULT. NR 1 CABIN PRESSURE CONTROLLER SHOWS P5 OVERHEAD CABIN PRESSURE CONTROL MODULE LRU FAULT. REPLACSDR ASAA2014080208741Switch · malfunctionedTHE NR 2 ENGINE VALVE CLOSED LIGHT ILLUMINATED BRIGHT BLUE ON CLIMBOUT ALL ENG INDICATIONS NORMAL. LIGHT REMAINED ON FOR 2 HRS THEN WENT OUT. ENGINE VALVE LIGHT RETURNED 30 MIN LATER AND REMAINED ON. ACFT GROUNDED. REPLACED HPSOV SWITCH IAW AMM 73-21-09-00SDR ASAA2014073008719Controller · failedDURING LANDING - MASTER CAUTION ILLUMINATED WITH AUTO FAIL LIGHT ON. ACFT GROUNDED. ACCOMPLISHED AUTO FAIL LIGHT ON FAULT ISOLATION TEST, SYS NR 2 HAS 2 FAULTS, CODE 001 AND 41. ACCOMPLISHED SYS WIRING FAILURE FAULT ISOLATION TEST WITH CPC-PANEL WIRING FAULSDR ASAA2014073008715Actuator · leakingNR 2 ENGINE RT VSV ACTUATOR IS LEAKING 15 DROPS PER MINUTE. ACFT GROUNDED. R & R NR 2 ENGINE RT VSV ACTUATOR IAW AMM 75-31-01-400-802-FOO. VSV ACTUATOR LEAK TESTED GOOD IAW AMM 75-31-01-790-801-FOO. ACCOMPLISHED TEST 12-ACTUATORS TEST, TEST PASS NO FAULTS SDR ASAA2014072108627Outflow Valve · malfunctionedOUTFLOW VALVE STAYED FULL CLOSED WHEN ON THE GROUND. ACFT GROUNDED. PERFORMED GROUND VERIFICATION TASK REF FIM 21-31-801 AND 21-31-802. GROUND TEST ON NR 1 AND NR 2 PRESSURE CONTROLLER. OPS NORMAL. CODE NR 57 FOUND ON PRESSURE CONTROLLER NR 2 CLEARED AND RSDR ASAA2014070508450Shim · wornACCOMPLISHING NR 2 FAN BLADE LUBE IAW T/C 78472002. FOUND FAN BLADE SHIMS MISSING MOLYDAG COATING MORE THAN 25 PERCENT IAW MM 72-21-02-200-801, STEP 2CL. ACFT GROUNDED. REPLACED NR 2 ENGINE FAN BLADE SHIMS IAW T/C 78472002.SDR ASAA2014070408453Warning Light · illuminatedAT CRUISE ALTITUDE, NOTICED NR 2 ENGINE VALVE CLOSED LIGHT ILLUMINATED BRIGHT BLUE. VERIFIED THAT NR 2 ENGINE WAS OPERATING NORMAL AND STABILIZED. NOTIFIED MAINTENANCE CONTROL AND CONTINUED TO DEPARTURE. THE LIGHT EXTINGUISHED RIGHT BEFORE WE STARTED THE DESDR ASAA2014070208439Warning Light · false activationIN CRUISE AT FL 370 MASTER CAUTION - OVERHEAT/DET ILLUMINATED AND APU DET INOPERATIVE ILLUMINATED. ACFT GROUNDED. TSR ISSUED. PERFORMED FIM 26-10, TASK 801. NO FAULTS FOUND IAW TSR STEP 3: REPLACED APU TAIL PIPE DETECTOR REF 26-15-01-000-802. PERFORMED ASDR ASAA2014070108414Detector · unknownAPU INOPERATIVE LIGHT ILLUMINATED FOR A SHORT TIME AFTER TAKEOFF, FOLLOWED QRH. ACFT GROUNDED. PERFORMED FIM TASK 26-10, TASK 801 NO FAULTS FOUND. PERFORMED FIRE SYS & LIGHT CHECK NO DEFECTS NOTED. RUN APU FOR FIVE MINUTES, SHUTDOWN. PERFORMED FIM TASK 26SDR ASAA2014063008403Warning Light · false activationNR 2 ENGINE VALVE CLOSED LIGHT ILLUMINATED INTERMITTENTLY BRIGHT BLUE IN FLIGHT. ACFT GROUNDED. RANG OUT HMU CONTACTS PINS 1&3 AT CONNECTOR DP1207 IAW WDM 76-21-21 IN THE CLOSED POSITION, NO DEFECTS FOUND. RAN NR 2 ENG, ENGINE VALVE CLOSED LIGHT OPS NORMAL,SDR ASAA2014062608375Warning Light · false activationAPU DETECTOR INOPERATIVE WITH OVERHEAT MASTER CAUTION DURING APPROACH. INTERMITTENT ILLUMINATIONS THROUGHOUT APPROACH WITH APU OFF. ACFT GROUNDED. PERFORMED FIM TASK 2610, TASK 801 NO FAULTS FOUND, NO HISTORY PAST 30 DAYS, SUSPECT NUISANCE FAULT DUE TO APU NSDR ASAA2014060408038Cabin Pressure · malfunctionedTWICE IN FLT AUTO FAIL & ALTN LIGHTS CAME ON MOMENTARILY THEN OFF, NOTED THE CABIN DESCENDED AT 500 FT IAW MIN THE CLIMBED 500' PER MINUTE. ACFT GROUNDED. PERFORMED FIM TASK 21-31 TASK 801 DCPC EXISTING & FAULT HISTORY W/NO FAULTS FOUND. ACFT OK FOR SERVICE.SDR ASAA2014060208016Warning Light · illuminatedCLIMBING THROUGH 10,000 FT, FM SJC AUTO FAIL LIGHT ILLUMINATED ON PRESSURIZATION CONTROL PANEL. ALTERNATE LIGHT ALSO ILLUMINATED. PRESSURIZATION NORMAL. SWITCHED CONTROL SW TO ALTN IAW QRH. ACFT GROUNDED. PERFORMED PRESSURIZATION SYSTEM GROUND TEST PER AMM 21-SDR ASAA2014052507900Warning Light · illuminatedDURING CLIMBOUT, AUTOFAIL & ALTN LIGHT ILLUMINATED FOR TWO MINUTES. LIGHTS THEN EXTINGUISHED. OPS NORMAL. ACFT GROUNDED. PERFORMED FIM TASK 21-31 TASK 801. BITE CHECKED BOTH PRESSURE CONTROLLERS, NO FAULT FOUND.SDR ASAA2014052207899Warning Light · illuminatedLEFT PACK LIGHT ILLUMINATED TWICE DURING CLIMB. THE RAM DOOR FULL OPEN LIGHT, LEFT, STAYED ILLUMINATED UNTIL APPROXIMATELY FL 300 IN CLIMB. LEVEL AT FL 320, RESET AGAIN AND PACK OPERATED FOR REMAINDER OF FLIGHT. ACFT GROUNDED.SDR ASAA2014052107898Start Valve · failedNO STARTER VALVE OPEN LIGHT FOR NR 2 ENGINE DURING START. NO N1 OR N2 ROTATION. ACFT GROUNDED. REPLACED NR 2 ENGINE START VALVE REF MM 80-11-03. OPS CHECKED GOOD.SDR ASAA2014052107891Warning Light · false activationLEFT PACK LIGHT CAME ON, LEFT PACK SHOWED 50 DEGREE C. RESET, AND ONE MINUTE LATER THE LIGHT CAME ON. RESET A SECOND TIME, AFTER 10 MINUTES, OPS NORMAL. ACFT GROUNDED. ACCOMPLISHED FIM TASK 21-53 TASK 813. NO DEFECTS NOTED. GROUND VERIFICATION COMPLETE. SDR ASAA2014051907865Shaft · damagedRIGHT SIDE INBD LINK ON RAM AIR INLET DOOR DEFLECTOR SHAFT ASSY IS DAMAGED. LT SIDE INBD LINK ON RAM AIR INLET DEFLECTOR DOOR SHAFT IS DAMAGED AND APPEARS TO BE CORRODED. ACFT GROUNDED. REPLACED RT RAM AIR INLET DEFLECTOR DOOR SHAFT ASSY AND LINKS REF AMM 2SDR ASAA2014051807841Controller · unknownAUTO FAIL FL370, SYSTEM SWITCHED TO ALTN AUTOMATICALLY IAW CHECKLIST. SELECTED ALTN, AUTO FAIL EXTINGUISHED. SYSTEM OPERATED NORMALLY IN ALTN. ACFT GROUNDED. COMPLISHED BITE CHECK OF NR 1 CPC. NO LOGGED FAULTS. R & R NR 1 CPC IAW AMM 21-31-01. ACCOMPLISHEDSDR ASAA2014051107771Warning Message · illuminatedDURING TROUBLESHOOTING, NR 2 ENGINE IGNITION FOUND FAULT CODE 73-11452 EVERY FLT LEG SHORT TIME FAULT. ACFT GROUNDED.SDR ASAA2014050707724Exciter · failedNR 2 ENGINE DID NOT START, AFTER 10 SECONDS OF START LEVER IN IDLE POSITION. FUEL FLOW INDICATED 560 LBS/HR LT IGNITION SELECTED. ACFT GROUNDED. SWAPPED LT IGNITOR LEAD TO THE RIGHT EXCITER BOX & L IGNITOR. OPS CHECED GOOD. REINSTALLED RT LEAD TO RT EXCITSDR ASAA2014041507647Seat Track · crackedFWD SEAT TRACK AT LBL 45.75 SHOWS CRACK INDICATIONS. ACFT GROUNDED. REPAIRED IAW REO-G17388, REV A AND EA SB737-53-1296-NG-108.SDR ASAA2014040807478Idg · malfunctionedDURING TAKEOFF ROLL, MASTER CAUTION LIGHT, ELEC 6 PACK LIGHT AND THE NR 2 DRIVE CAME ON FOR ABOUT ONE SECOND AND THEN ALL THREE LIGHTS WENT OUT. CONTINUED TAKE OFF AND FLIGHT WITH NO FURTHER PROBLEMS. ACFT GROUNDED. REPLACED NR 2 ENGINE IDG IAW AMM 24-11-1SDR ASAA2014040707464Warning Light · false activationDURING START OF TAKEOFF ROLL, RECEIVED A MASTER CAUTION AND "ELEC" ANNUNCIATION IN 6-PACK. INITIATED REJECTED TAKEOFF BELOW 60 KIAS. MASTER CAUTION AND "ELEC" LIGHTS EXTINGUISHED AS SOON AS THROTTLES WERE RETARDED. NOTED NO OTHER CAUTION LIGHTS AND NO LIGHTSSDR ASAA2014031807238Controller · malfunctionedAT FL370, AUTO FAIL LIGHT ILLUMINATED. PERFORMED QRH PROCEDURE. SWITCHED CONTROLLER TO ALTERNATE. PRESSURIZATION CONTROLLABLE. ACFT GROUNDED. COMPLIED WITH BITE TEST PROCEDURE FOR NR 1 & 2 CABIN PRESSURE CONTROLLERS FOUND LRU FAILED ON NR 1, CLEARED EXISTSDR ASAA2014031407199Warning Message · illuminatedOVERHEAT LIGHT ILLUMINATED ON "RIGHT SIDE". QRH PROCEDURES FOLLOWED AFTER 5 MINUTES: LIGHT REMAINED ON. COMPLETED FLIGHT WITH SWITCH OFF. FLIGHT LIMITATIONS FOLLOWED. ACFT GROUNDED. T/S REF WDM 30-41-11. VERIFIED WINDOW HEAT COMPUTER GOOD, VERIFIED COIL CSDR ASAA2014022607004Warning Light · illuminatedWITH APU ON AND PROVIDING POWER EXTERNAL POWER DISCONNECTED CAUSED ALL POWER TO BE LOST. BATTERY PROVIDING POWER. APU GEN OFF BUSS LIGHTS ON, RECONNECTED APU TO BUSSES AND CDS FAULT LIGHT ILLUMINATED FOR APPROX 3 TO 4 MIN. THEN WENT AWAY. ACFT GROUNDED. PSDR ASAA2014021806894Controller · faultedAUTO FAIL LIGHT ILLUMINATED IAW QRH, MODE SELECTOR IN ALTERNATE, AUTO FAIL LIGHT EXTINGUISHED. ACFT GROUNDED. ACCOMPLISHED BITE CHECK OF BOTH CABIN PRESSURE CONTROLLERS. FOUND CODE NR 057 ON CONTROLLER 1 AND CODE NR 22 ON CONTROLLER 2. BOTH FAULTS WERE ABLSDR ASAA2014020906807Controller · malfunctionedAUTO-FAIL LIGHT ILLUMINATED, QRH FOLLOWED, PRESSURIZATION CONTROLLER IN ALT CABIN, ALTITUDE CONTROLLABLE. ACFT GROUNDED.SDR ASAA2014013106737Warning Light · illuminatedLEFT ELEVATOR PITOT OVERHEAD WARNING LIGHT ILLUMINATED AFTER ENGINE START, P18-3 4C CIRCUIT BREAKER IS IN. ACFT GROUNDED. OPENSDR ASAA2014013006724Warning Light · false activationDURING DESCENT, PRESSURE AUTO FAIL LIGHT ON. SWITCHED TO ALTERNATE, FAILED LIGHT ON AS WELL. ALL DASHES IN WINDOWS. ACFT GROUNDED. PERFORMED BITE CHECK OF PRESSURE CONTROLLERS, NO CURRENT FAULTS LOGGED IAW FIM 21-31 TASK 801. PERFORMED PRESSURIZATION SYS GROSDR ASAA2014012612499Warning Message · false activationAFTER START, ENGINE LIGHT STAYED ILLUMINATED ON FIRST OFFICER`S BOTH ALT MODE LIGHTS ON ENGINE ELECTRONIC CONTROL PANEL CAPTAIN`S IAS DISAGREE. ACFT GROUNDED. PERFORMED EEC BITE TEST REF FIM 73-00, TASK 801, NO FAULTS FOUND, PERFORMED EEC GROUND TEST REF AMM
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