N519AS
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 = 'N519AS' 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 = 'N519AS' 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 ASAA2021112836755Unknown · unknownREF T/C NG-21EA-23228-1, #1 PACK ZONE TEMP CONROLLER LOGGED "ZONE" TRIM VALVE FAULT DURING BITE TEST. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 21-62 TASK 801, FAULT CLEARED.SDR ASAA2021111336615Processor · failedLEFT FUEL TANK QTY INOP - BLANK DISPLAY. GROUNDED - YES. TROUBLESHOT TO BAD FQIS COMPUTER, REF B737-800 FIM 28-41 TASK 810. REPLACED FQIS COMPUTER IAW B737-800 AMM 28-41-81. OPS TEST GOOD. LH FUEL TANK QTY RETURNED TO NORMAL. ETOPS GROUND VERIFICATION SUCCESSFSDR ASAA2021110936550Unknown · unknownHF #1 SHOWS FAIL MESSAGE. GROUNDED - YES. CYCLED 4 CIRCUIT BREAKERS ASSOCIATED WITH HF SYSTEM. OPS CKS GOOD.SDR ASAA2021103136472Unknown · unknownFLIGHT ATTENDANT REPORTS L1 DOOR HARD TO OPEN AND CLOSE. GROUNDED - YES. OPEN AND CLOSED DOOR FROM INSIDE AND OUTSIDE, NO DEFECTS NOTED .NO HISTORY 90 DAYS. LUBED GUIDE PLATES AS PRECAUTIONARY OPS CHECK GOOD REF B737-800 AMM 52-11-00.SDR ASAA2021102636414Unknown · unknownHF #2 INDICATES "FAIL FAIL" ON ACTIVE AND STBY WINDOWS. GROUNDED - YES. ACCOMPLISHED RESET HF #2 OPS CK GOOD IAW B737-800 FIM 23-11-806 SEAMC JOEY NOTIFIED.SDR ASAA2021091635980Lens · noneFLIGHT ATTENDANT REPORTS THAT THE EMERGENCY LIGHT COVER BY THE L1 DOOR BROKE AND FELL OFF. GROUNDED - YES. INSTALLED EMERGENCY LIGHT LENS PER B737-800 AMM 33-51-01 OPS CHECK GOOD.SDR ASAA2021090535858Lens · brokenL/H EMERGENCY EXIT LT COVER @16A BROKEN. GROUNDED - YES. 16-A REPLACED L/H LOWER EMERGENCY LT & COVER -OPS CK OK.SDR ASAA2021081635718Cover · missingFAS NOTIFED US OF A MISSING COVER FOR THE EXIT SIGN ON THE WALL IN ROW 17 DEF. GROUNDED - YES. COMPLETED FERRY FLIGHT CLEARS MCT. CN# 16012519 SEAMC JEREMY NOTIFIED.SDR ASAA2021081435703Window · faultedLEFT FORWARD WINDOW HEAT INDICATED AN OVERHEAT. GROUNDED - YES. PERFORMED T/S PER B737-800 FIM 30-41 TASK 812, FOUND PRIMARY SENSOR OPEN AND SPARE SENSOR OUT OF RESISTANCE LIMITS. REQUIRES L1 WINDOW CHANGE. OLD WINDOW WAS AN H12 NEW WINDOW IS AN H11. MOVED TAPSDR ASAA2021081035679Sensor · faultedL1 WINDOW OVERHEAT, NOT IN SUNLIGHT. GROUNDED - YES. HARD FAIL PRESENT. WINDOW HEAT CONT LOGS SEVERAL WINDOW SENSOR FAULTS. SWITCHED TO SPARE SENSOR, FAULT CLEARED AND SYS OPS CKS NML PER B737-800 AMM 30-41-00, GND VERIFICATION SUCCESSFUL.SDR ASAA2021061835140Valve · leaking#2 ENG FUEL LEAK AFTER SHUTDOWN. GROUNDED - YES. #2 ENG. RAN ENGINE AT IDLE, FOUND HPTACC VALVE DRAIN DRIPPING AFTER SHUTDOWN. REMOVED AND REPLACED #2 ENGINE HPTACC VALVE. OP CHECK GOOD, NO LEAKS NOTED, REF B37-800 AMM 75-21-01.SDR ASAA2021061835139Actuator · leaking#2 ENG VSV (LEFT) DRAIN DRIPS FUEL AFTER ENGINE SHUT DOWN. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE LH VSV ACTUATOR PER B737-800 AMM 75-31-01. LEAK AND OPS CHECK GOOD. INSTALLATION TEST PASSED.SDR ASAA2021050634765Pressure Switch · faultedAP A WILL NOT ENGAGE AND A+B WILL ONLY ENGAGE FOR 10 SEC. GROUNDED - YES. PERFORMED DFCS BITE REF B737-800 FIM 22-11 TASK 801. FOUND FAULTS 22-11127,22-11535. REF FIM 2213 TASK 806 REQUIRES REPLACEMENT OF PRESSURE SWITCH S771. REMOVED AND REPLACED HYDRAULIC PRSDR ASAA2021042434671Transceiver · faultedF/O SIDE WEATHER RADAR APPEARS TO POINT DOWN EXCESSIVELY SHOWING EXTREME GROUND CLUTTER, WHEN IN AUTO MODE. GROUNDED - YES. ACCOMPLISHED WXR BITE REF B737-800 FIM 34-43 TASK 801. UNABLE TO DUPLICATE DEFECT. PRECAUTIONARY REPLACED WXR TRANSCEIVER REF B737-800 ASDR ASAA2021042134629Connector · corrodedDURING T/S OF 'B' AUTOPILOT ELEVATOR ACTUATOR FOUND CORROSION ON 'A' ELEVATOR AUTOPILOT ACTUATOR. CONNECTOR #. GROUNDED - YES. REMOVED AUTOPILOT ELEVATOR ACTUATOR "A" REF B737-800 AMM 22-11-26-00-801. INSTALLED NEW "A" AUTOPILOT ACTUATOR. LEAK CHECK OK. REF AMSDR ASAA2021042134628Actuator · faultedDURING ELEV FEEL COMP TEST - FAILED ELEV DUAL AUTHORITY TEST 51.27 - B CHANNEL OUT OF LIMITS. GROUNDED - YES. DID TEST OF "B" ELEV A/P ACT REF B737-800 AMM 22-11-26-820-801. A AND B WITHIN LIMITS AT 2.01. THEN RAN DUAL AUTHORITY TEST REF AMM 22-11-00-820-816 -SDR ASAA2021041734610Spring · brokenFLIGHT CONTROLS BEHAVING HYPER SENSITIVE AND DO NOT PROVIDE THE NORMAL FEEDBACK PRESSURE. ON TAKEOFF MY NORMAL FLIGHT CONTROL PRESSURE CAUSED A HIGH RATE OF ROTATION THAT WAS EVEN NOTICED BY THE NON-FLYING PILOT. DURING ALL PHASES OF FLIGHT THE CONTROLS FELT MSDR ASAA2021041634602Radar · malfunctionedWX RADAR DISPLAY DOES NOT WORK IN AUTO ON FO SIDE. GROUNDED - YES. PERFORMED WEATHER RADAR OPERATIONAL TEST AND SYSTEM TEST PER B737-800 AMM 34-43-00 W/ NO DEFECTS. OBSERVED CORRECT MANUAL AND AUTOMATIC TILT FUNCTION REGARDLESS OF SYSTEM SIDE USED OR DISPLAY SSDR ASAA2021041034544Indicator · malfunctionedRT FUEL QTY INDICATION AND TOTALIZER BLACKED FOR ONE MINUTE FOR EACH OCCURRENCE FOUR OCCURENCES. GROUNDED - YES. PERFORMED FQIS BITE PER B737-800 FIM 28-41 TASK 801. NO DEFECTS/ FAULTS NOTED. COMPARED F/D FUEL INDICATION WITH REFUELING STATION NO DISCREPANCIESSDR ASAA2021030234231Unknown · unknownWHILE INFLIGHT VTK FOLLOWED MAP ON CPTS ND RAN QRH FMC FAIL RH FMC WORKED NORMALLY NORMAL "FMC" SWITCH TO BOTH ON 2 CONTINUED FLIGHT UNEVENTFULLY. GROUNDED - YES. PERFORMED B737-800 FIM 34-61-00-810-801 AND 3-61-00-810-836. OPS CHECK GOOD. TEST PASSED. NO FUALSDR ASAA2021021934160Stop Fitting · out of toleranceAFTER TAKEOFF AT ABOUT 1500' "AFT ENTRY" DOOR LIGHT ILLUMINATED. FA'S REPORT DOOR HANDLE KEEPS POPPING BACK UP. TRIED SEVERAL TIMES. PRESSURIZATION APPEARED NORMAL. GROUNDED - YES. AIR TURN BACK. DIVERSION TIME 5 MINUTES - DURING TROUBLE SHOOTING FOUND SDR ASAA2021021734163Start Valve · failedNUMBER 2 ENG START SWITCH DOES NOT STAY ENGAGED IN GRD AND NO ROTATION. GROUNDED - YES. B737-800 FIM 80-07 TASK 806, OPENED NR 2 ENGINE COWL. DISCONNECTED CANNON PLUG FROM START VALVE CB NOW STAYS IN AND START SWITCH STAYS IN GROUND POSITION. RECONNECT CANNSDR ASAA2021021734117Control Panel · faultedHEADING SELECT KNOB DOESN'T CHANGE THE HEADING BUG. IT IS STUCK ON NR 274. GROUNDED - YES. REMOVED AND REPLACED DFCS MODE CONTROL PANEL REF B737-800 AMM 22-11-34, PERFORMED MCP INSTALLATION TEST REF AMM 22-11-34, NO FAULTS NOTED.SDR ASAA2021011733882Modulating Valve · inoperativeON MASTER RECALL AFTER START CHECKLIST CONT CABIN ZONE TEMP LIGHT ILLUMINATED AND RESET AFTER MASTER CAUTION RESET. GROUNDED-YES. REMOVED AND REPLACED CONT CABIN ZONE TRIM VALVE, IAW B737-800 AMM 21-61-21. OPERATIONS AND LEAK CHECK GOOD.SDR ASAA2021010133796Wire Harness · brokenTECH SERVICE REQUEST. FOLLOW UP TO RECENT REPORT OF NR 1 ENGINE A FIRE LOOP INOPERABLE, REF LOG PG 60007994. GROUNDED-YES. PER B737-800 FIM 26-10 TASK 805. INITIAL EVALUATION. ENGINE FIRE DET OPERATIONS TEST PASS. FIRE DET MODULE BITE TEST PASS. ACCOMPLSDR ASAA2020122433759Oil Filter · cloggedDURING INSPECTION OF APU FOUND OIL FILTER INDICATOR EXTENDED AND WILL NOT RESET. GROUNDED-YES. REMOVED AND INSPECTED BOTH LUBE FILTERS, NO DEBRIS FOUND. REMOVED AND REPLACED OIL FILTER INDICATOR AND LUBE FILTER ELEMENT, PER B737-800 AMM 49-91-13 AND 49-91-1SDR ASAA2020122033726Spacer · debondedWHILE ACCOMPLISHING T/C 78472010 NR 2 ENGINE FOUND 3 FAN BLADE SPACERS DEBONDING ELASTOMER MATERAL. GROUNDED-YES. REMOVED AND REPLACED THE 3 EA FAN BLADE SPACERS NR 2, NR 9 , AND NR 18, REF T/C 78472010 ON NR 2 ENGINE.SDR ASAA2020102633439Terminal · looseAS REQUESTED FOLLOW-UP TO REPORT OF NR 1 ENGINE FAULT LIGHT ON FIRE/OH TEST. GROUNDED-YES. ACCOMPLISHED INSPECTION OF NR 1 ENGINE FIRE/OH DETECTORS LOOPS A AND B CONNECTIONS, PER TSR710220. FOUND TWO TERMINALS LOOSE ON HARNESS FOR THE CORE UPPER RIGHT AND CSDR ASAA2020101933395Warning Light · false activationAFTER ENGINE START CONT CAB ZONE TEMP LIGHT ILLUMINATED WITH MASTER RECALL RESETS OKAY, NO OVERHEAT INDICATED. GROUNDED-YES. PERFORMED PACK/ZONE TEMP CONTROLLER BITE TEST NO CURRENT FAULTS, FOUND FAULT IN HISTORY FOR TRIM VALVE/FLIGHT DECK ON NR 2 CONTROLLERSDR ASAA2020091933192Pressure Switch · faultyLEFT CENTER FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED. GROUNDED-YES. REF B737-800 FIM 28-22 TASK 801, COULD NOT DUPLICATE FAULT. OPS TESTS NORMAL. AS A PRECAUTION, REMOVED AND REPLACED CENTER TANK LEFT BOOST PUMP RELAY, REF B737-800 AMM 28-22-18/401 AND CENSDR ASAA2020091743185Valve · failedABORTED TAKEOFF AT 70 KTS DUE NR 2 COWL ANTI-ICE CAUTION LIGHT. LIGHT EXTINGUISHED WHEN THRUST REDUCED TO IDLE. GROUNDED-YES. REMOVED & REPLACED ENGINE COWL TAI VALVE, REF B737-800 AMM 30-21-11 & ENGINE ANTI-ICE PRESSURE SENSOR REF B737-800 AMM 30-21-21. LSDR ASAA2020070632869Sensor · shortedAPU FAILURE TO START. FAULT MESSAGE INLET TEMP SENSOR SHOWS SHORT. GROUNDED - YES. REMOVED AND REPLACED APU INLET TEMP SENSOR PER AMM 49-61-31. OPS TEST NORMAL.SDR ASAA2020070632864Battery Pack · dischargedRT EMERGENCY EXIT LIGHTS GO OUT IMMEDIATELLY AFTER LIGHTS ARE TURNED ON. GROUNDED - YES. REPLACED BATTERY PACK PER AMM 33-51-06-960-805. OPS CHECKED GOOD.SDR ASAA2020041332632Warning System · false activationAFTER START, RECALL SHOWS ZONE TEMP LIGHT. LIGHT DISTINGUISHED ON RESET. GROUNDED - YES. ACCOMPLISHED #2 PACK TEMP CONTROL BITE, LOGGED: TRIM VALVE, FLT DECK . FAULT CLEARED, REF B737-800 FIM 21-62 TASK 801. ACCOMPLISHED CONTROL CABIN AUTO TEMP CONTROL FIM 21-SDR ASAA2020022482232Warning Light · false activationLEFT PACK ON WITH RECALL EXTINGUISHES ON RESET. GROUNDED - YES. PERFORMED PACK/ZONE TEMP CONTROLLER BITE TEST REF 737-800 AMM 21-61-00 FOUND PREVIOUS LEFT PACK TCV FAULT, CLEARS AFTER RESET. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2020021103141Battery Pack · failedREF T/C 78233001AFT LH EMERGENCY EXIT LIGHTS FAILED AFTER RECHARGE. GROUNDED - YES. REMOVED AND REPLACED AFT LH POWER SUPPLY BATTERY PACK IAW B737-800 AMM 33-51-06-960-805. GROUND VERIFICATION TEST IS GOOD.SDR ASAA2020021083124Display · inoperative#2 MCDU HAS TWO VERTICAL LINES. GROUNDED - YES. REMOVED AND REPLACED #2 MCDU REF B737-800 AMM 34-61-01-000/400-802. ALL GROUND VERIFICATION TESTS PASS.SDR ASAA2020012843968Sliding Window · malfunctionedLEFT SIDE WINDOW HEAT OVERHEAT LIGHT CAME ON. RAN QRH - AFTER 2 MINUTES WITH WINDOW OFF - TURNED IT BACK ON. 27 MINUTES LATER SAME OVERHEAT LIGHT ILLUMINATED. SWITCH WAS TURNED OFF FOR THE REMAINDER OF THE FLIGHT AND AIRSPEED RESTRICTIONS WERE REVIEWED. GROUNDSDR ASAA2020011731911Warning Message · false activation35 MINS INTO FLIGHT, FL350, -39C OAT- "L SIDE WINDOW" "OVERHEAT" LIGHT ON. QRH P6 3.5, OFF FOR 5 MINUTES, SWITCH ON - LT ON AGAIN. SWITCHED OFF REMAINDER OF FLIGHT. GROUNDED - YES. PER B737-800 FIM 30-41 TASK 809 WHCU BITE PASSES. HAS SENSOR FAULT IN HISTORY. SDR ASAA2020011331821Warning System · false activationLEFT SIDE WINDOW HEAT OVERHEAT LIGHT ILLUMINATED IN FLIGHT AND THEN REILLUMINATED AFTER A 5 MINUTE COOL DOWN. GROUNDED - YES. PERFORMED BITE LEFT SIDE WHCU IAW FIM 30-41 TASK 801. NO CURRENT FAULTS ON BITE, AND WINDOW SENSOR FAULT IN HISTORY. REMOVED AND REPLASDR ASAA2020011031820Warning System · false activationLEFT SIDE WINDOW HEAT OVERHEAT LT ILLUMINATED AT CRUISE. GROUNDED - YES. RAN QRH & LT EXTINGUISHED & REMAINED SO FOR THE DURATION OF THE FLIGHT.SDR ASAA2019123061719Warning Message · false activationCAPTAIN LEFT SIDE WINDOW HEAT OVER HEAT ILLUMINATED AT CRUISE FL340, RAN QRH WITH SWITCH OFF THEN BACK ON. OPS NORMAL. GROUNDED - YES. GROUND FUNCTIONAL CHECK GOOD IAW B737-800 AMM 30-41-11.SDR ASAA2019121131564Warning Light · false activationLEFT SIDE WINDOWS HEAT OVERHEAT LIGHT ILLUMINATED UPON LANDING. GROUNDED - YES. PERFORMED WINDOW HEAT CONT SYS TEST PER B737-800 AMM 30-41-11 ALL TESTS PASSED WITH NO FAULTS FOUND.SDR ASAA2019120971538Shutoff Valve · inoperativeAPU FAULT LT ILLUMINATED A FEW MINUTES AFTER SHUTTING APU OFF. GROUNDED - YES. ACCOMPLISHED BITE CK ON APU REF B737-800 FIM 49-60 TASK 801. MAINT MESSAGE 49-31001 APU FUEL VALVE SHUTDOWN DISPLAYED. FOLLOWED FIM 49-30 TASK 801. APU FUEL VALVE FAILED IN OPEN OSDR ASAA201912091544Actuator · out of limitsWHILE PERFORMING T/C 78273000 FOUND FAULT CODE 75-30401 VSV POSITION SIGNALS DISAGREE SHORT TIME FAULT DEFERRED PER T/C 78273000. GROUNDED - YES. ACCOMPLISHED T/C 78273000 FAULT MSG 75-30401 (THE VSV POSITION SIGNALS DISAGREE) IS NO LONGER ACTIVE, FAULT CODE 7SDR ASAA2019102931194Gfi · openLEFT FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED, RAN QRH FOR FUEL PUMP LOW PRESSURE LIGHT. QRH ACCOMPLISHED. GROUNDED - YES. T/S PER B737-800 FIM 28-22 TASK 801 . FOUND GFI R54 OPEN. RESET R54. XFERED FUEL TO CTR TANK. SUCCESSFULLY XFERRED FUEL OUT WITH BOTH CTRSDR ASAA2019102631135Unknown · malfunctionedHF RADIOS ARE NOT TRANSMITTING. GROUNDED - YES. REF L/P 12139150 FOR FLIGHT CREWS VERIFIED BOTH HF RADIOS OPERATE NORMALLY. BOTH HF RADIOS COMMUNICATION TEST OK PER B737-800 AMM TASK 23-11-00-730-801. REMOVED MEL 23-11C.SDR ASAA2019100753926Valve · overheatedZONE TEMP FLT DECK (CONT CAB) ILLUMINATED ON RECALL, EXTINGUISHES ON MASTER CAUTION RESET. GROUNDED - YES. CONFIRMED FAULT, "CONT CAB" ZONE TEMP LIGHT COMES ON EVERYTIME, RECALL PRESSED. R/H PACK/ZONE TEMP CONTROLLER SHOWS HARD FAIL "FLT DECK TCV" (V143). GVI SDR ASAA2019092230786Satcom · lockedSATCOM LOCKUP. GROUNDED - YES. ACCOMPLISHED RESET PROCEDURE PER QRH. SATCOM RESTORED NORMAL.SDR ASAA2019081423394Indicator · inoperativeREFUELING CENTR TANK QTY INDICATOR INOP. GROUNDED - YES. REMOVED AND REPLACED REFUELING CENTER TANK QTY INDICATOR. REF B737-800 AMM 28-41-61 OPS CHECK GOOD.
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