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 ASAA2019072430201Diffuser · failedLEFT PACK LIGHT ILLUMINATED ON T/O ROLL AT 100 KIAS. AFTER T/O, PERFORMED QRH CHECKLIST. PACK RESET OK. GROUNDED - YES. FOUND LT PLENUM FAN BYPASS CHECK VALVE AND HINGE PIN MISSING REF AMM 21-51-03. REMOVED AND REPLACED LT PLENUM DIFFUSER ASSEMBLY. REF AMM 21SDR ASAA2019072430200Warning System · false activationDURING PREFLIGHT AT GATE LEFT PACK LIGHT ILLUMINATED. RAN QRH CHECKLIST AND PACK LIGHT EXTINGUISHED AFTER PRESSING TRIP RESET. PACK RESUMED NORMAL OPERATIONS. GROUNDED - YES. PERFORMED FIM 21-53 TASK 803 INTIAL EVAL PACK LIGHT RESET AND REMAINS OUT DETERMINED SDR ASAA2019072230132Check Valve · missingLEFT AMBER PACK LIGHT ILLUMINATED ON TAKE OFF ROLL AT 100KTS, AFTER TAKE OFF, QRH RUN. PACK RESET OK. GROUNDED - YES. PERFORMED MULTIPLE PZTC BITES OF LT AND RT PZTC REF FIM 21-62 TASK 801 WITH NO FAULTS FOUND. PERFORMED GVI OF LT RAM AIR SYSTEM AND HEAT EXCHASDR ASAA2019072130134Warning System · false activationLEFT PACK LIGHT ILLUMINATED ON TAKEOFF ROLL AT APPROXIMATELY 130 KTS. RAN QRH PROCEDURE THE LIGHT EXTINGUISHED. GROUNDED - YES. PERFORMED TEMP CONTROL BITE REF FIM 21 62 TASK 801 AND 21-52 TASK 817 ON RECALL PACK LIGHT REMAINS EXTINGUISHED. GROUND VERIFICATIONSDR ASAA2019072030106Warning System · false activationLEFT PACK LIGHT ILLLUMINATED AFTER T/O. PACK RESET WITH QRH. OPS NORMAL. GROUNDED - YES. PREFORMED PACK/ZONE TEMP CONTROLLER BITE TEST REF AMM 21-61-00. GROUND VERIFIED. OPS CHECK GOOD.SDR ASAA2019070829980Warning System · false activationVTK MESSAGE ON CA ND W ASSOCIATED FMC FAILURE. GROUNDED - YES. PERFORMED FIM 34-61 TASK 801. NO DEFECTS NOTED. OK FOR SERVICE.SDR ASAA2019070829977Warning Message · false activationVTK MESSAGE ON CA ND. GROUNDED - YES. PERFORMED FMC RESET, REF FIM 34-61 TASK 836 FMC OPS NORMAL. AIRCRAFT OKAY FOR SERVICE.SDR ASAA2019061059594Terminal · damaged#1 ENG O/H DET LOOP "B" WILL NOT TEST. GROUNDED - YES. FOUND CORE DETECTOR RH TO HAVE A BROKEN TERMINAL LUG. RE-TERMINATED PER B737-800 AMM 26-11-02-960-801. PERFORMED AN ENGINE FIRE DETECTION OPERATIONAL TEST PER AMM 26-11-00-710-801. CHECKS GOOD. ALTERNATE DSDR ASAA2019060329551Lens · detachedROW 17A EXIT LIGHT COVER MISSING. GROUNDED - YES. FOUND EMER EXIT SIGN (COVER) ON FLT DECK RE-INSTALLED @ ROW 17A.SDR ASAA2019052729490Pin · migrated#1 ENGINE 3RD STAGE ANTI ROTATION SLAB HEADED PIN AT 9 OCLOCK ALF HAS ROTATED 90 DEGREES AND HAS STARTED TO MIGRATE. REF T/C SBCFM56-7B-72-0986-1. PHOTOS IN INSPECTION SERVER REF L/P 11759592, 3RD STAGE AT 3 OCLOCK , ANTI ROTATION REMAINS ROTATED LESS THAN 45 SDR ASAA2019050129243Harness · defectiveON TAKEOFF ENG NR 1, EGT EXCEEDED. REACHED 983 DEGREES. ALSO, THE EGT CAME DOWN INTO BARELY NORMAL RANGE BUT WOULD LOWER AND SPIKE UP THEN DROP. IT REPEATED MULTIPLE TIMES. GROUNDED - YES. DIV TIME: 32 MINUTES. REMOVED AND REPLACED S3,S4 PROBES REF AMM 77-21-0SDR ASAA2019042829215Warning System · false activationREF T/C 78273000 ENGINE NR 1 SHOWS LONG TIME FAULT 77-20861. BOTTOM LEFT EGT SIGNAL OUT OF RANGE. DEFERRED PER T/C 78273000. GROUNDED - YES. NO FAULT STORED AT THIS TIME. CLEARS 'PLT'.SDR ASAA2019042629176Actuator · leakingDURING #2 ENG LEAK CHECK NOTICED FUEL LEAKING FROM #2 ENG R/H VSV ACTUATOR DRAIN. GROUNDED - YES. REMOVED VSV ACTUATOR AND INSTALLED TO STEP 2(E) REF B737-800 AMM 75-31-01-400-802. RIGHT VSV ACTUATOR INSTALLATION COMPLETE & LEAK TEST PASSED REF AMM 75-31-01-79SDR ASAA2019042299077Motor · inoperativeL CTR FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT WITH 11.0 FUEL IN CTR TANK. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 28-22 TASK 801. DETERMINED L/H CTR MOTOR IMPELLER NOT WORKING. REMOVED AND REPLACED MOTOR IMPELLER PER B737-800 AMM 28-22-41. PERFORMSDR ASAA2019041538968Warning Light · false activationSAT PROMPT MISSING FROM MCDU. GROUNDED - YES. PERFORMED QRH PROCEDURE AND SATCOM FUNCTION RETURNED TO NORMAL.SDR ASAA2019040548891Warning Message · false activationON RECALL HAD A ZONE TEMP LIGHT. IT WAS ABLE TO RESET. GROUNDED - YES. FLIGHT DECK PRIMARY TEMP CONTROL SYSTEM INOP. NR 2 PACK/ZONE TEMP CONTROLLER LOGGED FLT DECK TRIM VALVE FAULT. RESET FAULT. NR 2 PACK/ZONE TEMP CONTROLLER PASSES ALL BITE TESTS. REF B737-8SDR ASAA2019040188836Key · inoperativeCAPTAINS MCDU DEP/ARR AND HOLD BUTTONS INOP. GROUNDED - YES. PERFORMED B737-800 FIM 34-61 TASK 802-VERIFIED CAPTS MCDU DEP/ARR AND HOLD BUTTONS FAILED/INOP. REF B737-800 AMM 34-61-01,REPLACED CAPTS CDU. INSTALLATION OPS TEST PASSED. CAPTS MCDU DEP/ARR AND HOLDSDR ASAA2019032528771Indicator · erraticAIR CONDITIONING TEMPERATURE GAUGE INOP - ALL TEMPS READING EXTREMELY LOW - PEGGED TO BOTTOM OF SCALE. GROUNDED - YES. RMVD & RPLCD CABIN TEMP INDICATOR IAW AMM 21-61-32/401. CHECKED GOOD. OPS NORMAL. CLEARED MEL 21-17E, MEL21-17F & MEL 21-17G.SDR ASAA2019031628634Sensor · dirtyTEMP INDICATOR FOR PAX CABIN INDICATES COLDER THAN ACTUAL "NORMAL" CABIN TEMP. GROUNDED - YES. CLEANED SENSOR OPS NORMAL.SDR ASAA2019031028547Indicator · failedCABIN TEMPERATURE CONTROL PANEL GAUGE SHOWS NO TEMPERATURE INDICATING WHEN LEFT OR RIGHT PACK SOURCE SELECTED. GROUNDED - YES. VERIFIED DEFECT REMOVED AND REPLACED TEMP CONT MODULE & TEMP GAUGE PER AMM 21-61-15 ALL OPS CKD NML.SDR ASAA2019022628301Wire · disconnectedFWD CAB TEMP CONTROL WILL NOT MANAGE CABIN TEMP. CABIN TEMP SPIKES HOT/COLD WITH SMALL INPUTS TO THE KNOB. PLACED IN THE OFF POSITION CABIN TEMP IS ACCEPTABLE. GROUNDED - YES. CONFIRMED FAULT, FWD PASS CABIN TEMP SENSOR FAN INOP. REMOVED CEILING PANEL, FOUND PSDR ASAA2019022518298Controller · malfunctionedFWD CABIN TEMP CONTROLLER IN "AUTO" DOES NOT HOLD SELECTED TEMP. SUPPLY DUCT TEMP FLUCTUATES BETWEEN 0-60C RESULTING IN THE CABIN GETTING TOO HOT AND TOO COLD, BACK AND FORTH. GROUNDED - YES. REF B737-800 FIM 21-61 TASK 864. COULD NOT DUPLICATE. CLEANED FWD CASDR ASAA2019021428177Battery Pack · dischargedEMERGENCY LIGHTS INOP AT R/H SEAT ROWS 3-12, RT 27-29, AND ALL EMERGENCY LIGHTS AROUND R2 DOOR. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK AT STATIONS 500C+7 WL 213 RBL 67 (M1676) AND STATION 952 WL 291 RBL 14 (M1672) IAW AMM 33-51-06. SYSTEM CHECKS GOOSDR ASAA2019011527890Transition Panel · corrodedFWD PIT RT TRANSITION PANEL BETWEEN STATIONS 500G TO 500H REQUIRES REPAIR. DUE TO CORROSION OUT OF LIMITS. GROUNDED - YES. REPAIRED THE RIGHT HAND TRANSITION PANEL IN THE FORWARD CARGO IAW SRM 53-00-53-R2-5. FROM STA 500G TO STA 500H. AND SRM 53-30-53;51-20-01SDR ASAA2019011128178Bulkhead · damagedAFT PRESSURE BULKHEAD STRINGER S-7L, TOWARD THE CENTER OF THE BULKHEAD IS SEPARATING FROM THE SKIN WITH THE MOST INSIDE CENTER FASTENER PULLING THROUGH THE STRINGER. THE SAME STRINGER, S-7L ALSO HAS WAVINESS THROUGHOUT THE LOWER THIRD OF TIE STRINGER AND AROUNSDR ASAA2019011127981Strap · corrodedAFT CARGO COMPT STA 787-807, CARGO DOOR THRESHOLD INNER STRAP IS CORRODED. GROUNDED - YES. REMOVED CORROSION FROM INNER STRAP PER SRM 53-60-15, ORIG THICKNESS .100 PER SRM 53-60-15, REMOVED .017 MAT REMAINING IS .083 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60SDR ASAA2019011127961Threshold · corrodedAFT CARGO COMPT. CARGO DOOR THRESHOLD WEB IS CORRODED. GROUNDED - YES. REMOVED CORROSION AFT PIT WEB PER SRM 53-60-15-1A-1 ORIGINAL THICKNESS .045 PER DWG 146A8123-25 REV A, REMOVED .013 REMAINING IS .033. OUT OF LIMITS PER SRM 53-60-15-1A 14G3. REMOVED AFT WESDR ASAA2019011127960Floor Support · corrodedMAIN CABIN FLOOR SUPPORT STRUCTURE UPPER SURFACE CORRODED BETWEEN STA 312 AND 328 AT APPROX. RBL 55. GROUNDED - YES. REMOVED AND REPLACED R1 DOOR AREA INNER CHORD IAW BAC DWG 141A8310 REV B AND SRM 51-40-02, ORIGINAL MATERIAL THICKNESS .080 REMOVED .025 REMAINSDR ASAA2019011127888Intercostal · gougedMAIN CABIN FLOOR STRUCTURE - APPROX 10 INCHES FWD OF STATION 294.5, INTERCOSTAL AT BL 0 HAS SMALL GOUGES ON LOWER SIDE OF FLOOR ATTACHMENT HOLE. GROUNDED - YES. REMOVED & REPLACED INTERCOSTAL REFERENCE: BAC DWG 141A54001, REV: -, SHEET 20 & SRM 51-40-02. ME-04SDR ASAA2019011127820Intercostal · crackedCABIN STA 312-328 LBL 47 INTERCOSTAL CRACKED AT UPPER FLANGE. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02 AND DWG 141A5400 REV B.SDR ASAA2019011027959Transition Panel · corrodedAFT PIT, RT TRANSITION PANEL HAS CORROSION IN 12 AREAS FROM STA 727F-727H. GROUNDED - YES. REMOVED CORROSION IAW SRM 51-10-02, ORIGINAL MATERIAL WAS .040 IAW SRM 53-60-53. REMAINING THICKNESS IS .030 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. REMOVED DAMAGED SDR ASAA2019011027955Transition Panel · corrodedAFT PIT, RT TRANSITION PANEL HAS CORROSION IN 17 AREAS FROM STA 727D-727F. GROUNDED - YES. REMOVED DAMAGED SECTION OF TRANSITION PANEL FROM STA 727D - 727F IAW SRM 53-00-53, REMOVED CORROSION FROM DAMAGED SECTION OF TRANSITION PANEL IAW SRM 51-10-02, ORIG. MATSDR ASAA2019011027887Transition Panel · corrodedAFT PIT, LT TRANSITION PANEL HAS CORROSION IN 7 AREAS FROM STA 727F-727H. GROUNDED - YES. REMOVED CORROSION FROM TRANSITION PANEL IAW SRM 51-10-02 ORG. THICKNESS IS .040 IAW SRM 53-60-53 AT STA 727G+12 REMAINING THICKNESS IS .010 LOSS OF .030 WILL BE OUT OF LISDR ASAA2019010927919Threshold · crackedFWD CARGO DOOR LWR CUTOUT THRESHOLD HAS 1EA DENT AT O/B FASTENER HOLE BETWEEN STA 460 AND STA 480. GROUNDED - YES. UPON FURTHER INVESTIGATION, FOUND CRACK AT DAMAGED HOLE LOCATION, REMOVED AND REPLACED WEB P/N 654A0003-58, PO 935525.1 IAW BAC DWG 143A8330 REV SDR ASAA2018122417507Outflow Valve · peelingAFT OUTFLOW VALVE AFT GATE ANTI SKATING FOIL PEELING. GROUNDED - YES. REMOVED THE LOOSE FOIL FROM THE AFT OUTFLOW VALVE AFT GATE REF B737-800 AMM 21-31-03-400-801 STEP 3F(4). THE OUTFLOW VALVE IS SERVICEABLE, NO FURTHER MAINTENANCE NECESSARY.SDR ASAA2018121077270Pressure Switch · failed#1 FUEL FILTER BYPASS LIGHT ILLUMINATED IN CLIMB. #1 ENG OPS NORMAL. GROUNDED - YES. PERFORMED FUEL FILTER BYPASS FAULT ISOLATION REF B737-800 AMM 73-05 NO FAULT MESSAGES. REMOVED + REPLACED FUEL FILTER ELEMENT REF AMM 73-11-02. NO CONTAMINATION FOUND REMOVED SDR ASAA2018112637052Valve · faultedCONT CAB ZONE TEMP LIGHT ILLUMINATED DURING MASTER CAUTION RECAL AFTER ENGINE START CHECK LIST. QRH PROCEDURES ACCOMPLISHED VERIFIED BACK UP OPS NORMAL, OCCURED ZERO MORE ENROUTE. GROUNDED - YES. ACCOMPLISHED PACK TEMP CONTROL BITE IAW B737-800 FIM 21-61 TASK SDR ASAA2018111646864Guide Vane · damagedFOUND #2 ENG 4 O'CLOCK POSITION, 1 OUTLET GUIDE VANE HAS DAMAGE OUT OF LIMIT. GROUNDED - YES. REMOVED AND REPLACED #2 ENG 4 O'CLOCK POSITION, 1 OUTLET GUIDE VANE REF B737-800 AMM 72-23-01.SDR ASAA2018111126820Unknown · malfunctionedFO PFD AND ND HAS SEVERAL WARNING FLAGS, NO VSPD LNP ALT AND MAP. MCDU SHOWS MESSAGE, SINGLE FMC OPERATION. GROUNDED - YES. ACCOMPLISHED RESYNC, PLACED FMC SELECTOR SWITCH TO BOTH ON LEFT AND OPERATION RESTORED. VERIFIED OPERATION OF FMC PER FIM 34-61 TASK 836SDR ASAA2018102926631Transceiver · failedUNABLE TO TRANSMIT ON HF1. CAN RECEIVE OK AND ABLE TO RECEIVE CELL CALL. NO SIDE TONE W/ PTT. GROUNDED - YES. CYCLED C/B FOR HF-1 NO HELP. REMOVED AND REPLACED NR 1 HF TRANSCEIVER REF AMM 23-11-21. OPS NORMAL.SDR ASAA2018102326582Filter Element · cloggedFOUND OIL FILTER INDICATOR HAS EXTENDED. GROUNDED - YES. SERVICED APU OIL FILTER INDICATOR REF AMM 49-91-13.SDR ASAA2018100226349Transceiver · defectiveUNABLE TO TRANSMIT ON HF RADIO NR 1. ALL OTHER FUNCTIONS WORK. GROUNDED - YES. DUPLICATED DEFECT COULD RECEIVE BUT NOT TRANSMIT. REPLACED NR 1 HF TRANSCEIVER REF AMM 23-11-21, OPS CHECK NORMAL, SUCCESSFUL GROUND VERIFICATION.SDR ASAA201808205836Autopilot Sys · disconnectedAUTOPILOT A DISCONNECTED AT CRUISE. RE-ENGAGED AUTOPILOT, OPERATED NORMALLY REMAINDER OF FLIGHT. ACFT GROUNDED. PERFORMED DFCS BITE PROCEDURE IAW FIM 22-11-TASK 801. TEST PASSED, NO FURTHER FAULTS NOTED.SDR ASAA2018082025813Unknown · unknownAUTOPILOT B DISENGAGED 3 TIMES IN FLIGHT, ONCE IN CLIMB AT 24,000' AND TWICE AT FL360: BOTH ALTITUDES IN SMOOTH AIR. AUTOPILOT A FUNCTION CORRECTLY. GROUNDED - YES. FFR LOGGED NUMEROUS 22-11607 FAULTS. MCP DATA INV. COULD NOT DUPLICATE MALFUNCTION. OP CK NORMASDR ASAA2018081645806Door · lack of lubeF/A REPORTED THE L1 DOOR WAS HARD TO OPEN. ACFT GROUNDED. ACCOMPLISHED FIM 52-10, TASK 807. NO DEFECTS NOTED. LUBRICATED THE EXTERNAL DOOR IAW AMM 12-25-11-640-801. FWD ENTRY DOOR HANDLE FORCE & DOOR SYSTEM TEST CHECKEDS GOOD IAW AMM 52-11-00-700-804.SDR ASAA2018072525528Warning System · false activationCONT CAB ZONE TEMP LIGHT ILLUMINATES DURING RECALL. ZONE TEMP LIGHT EXTINGUISHES WHEN MASTER CAUTION IS RESET. GROUNDED - YES. PERFORMED PACK/ZONE TEMP CONTROLLER NR 1 AND NR 2 BITE TEST REF AMM 21-61-00-700-806-002. NR 2 CONTROLLER HAS "FLT DECK" FAULT. FAULTSDR ASAA2018072425523Control Panel · defectiveF/O'S MCP COURSE WINDOW 100'S AND 1'S DIGIT INOP (VERY DIFFICULT TO READ AS THEY STICK). GROUNDED - YES. REMOVED & REPLACED MCP REF AMM 22-11-34-400-801. ACCOMPLISHED MCP INSTALLATION TEST REF AMM 22-11-34-740-801. OPS CK GOOD. ACCOMPLISHED DFCS LRU REPLACEMENSDR ASAA2018071625405Lens · missingFA REPORT EMERGENCY EXIT SIGN COVER ROW 17 ACFT RIGHT SIDE MISSING. GROUNDED - YES. INSTALLED NEW EMERGENCY LIGHT COVER ROW 17 RIGHT SIDE.SDR ASAA2018070825298Unknown · malfunctionedBATTERY SWITCH ON, EXTERNAL PWR DROPPED OFF. ELECT LIGHT ON. GROUNDED - YES. PERFORMED BITE TEST OF BATT SYSTEM PER FIM 24-31 TASK 801. FAULTS INTERMITTENT, AND BATTERY FULLY CHARGED WITH NO PRESENT FAULTS.SDR ASAA2018061625087Blade · damagedDURING ACCOMPLISHMENT OF T/C 78472002 ON THE NR 2 ENGINE, FOUND BLADES 1, 13, 16, 17, 19, 23, AND 24 CU-NI-IN COATING DAMAGED BEYOND LIMITS. ACFT GROUNDED. INSTALLED NEW FAN BLADES IAW T/C 78472002.
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