N514AS
Service difficulty reports · 370
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 = 'N514AS' 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 = 'N514AS' 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 ASAA2015121214202Warning Light · false activationCONT CABIN ZONE TEMP LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED PACK/ZONE TEMP CONTROLLER BITE CHECK IAW FIM 21-62 842. NO FAULTS FOUND. OPS CHECK GOOD.SDR ASAA2015112813956Unknown · unknownAFTER A MOMENTARY PITCH UP, THE A AUTOPILOT WOULD DISENGAGE TRYING TO REACQUIRE ALTITUDE. OCCURRED IN LEVEL FLT, SMOOTH AIR. ACFT GROUNDED.SDR ASAA2015112713955Indicator · inoperativeFORWARD PASSENGER CABIN AIR TEMPERATURE INDICATOR INOPERATIVE. IT READS 0 DEGREES C. ALL OTHER TEMPERATURE INDICATORS NORMAL. ACFT GROUNDED. ON DEFERRAL.SDR ASAA2015112713958Autopilot Sys · malfunctionedA-AUTOPILOT ENGAGES FOR 2 SECONDS THEN DISENGAGES WITH VISUAL AND AURAL ALERTS. B-AUTOPILOT WORKS FINE. ACFT GROUNDED. ACCOMPLISHED DFCS BITE REF FIM 22-11, TASK 801. NO FAULTS IN CURRENT STATUS FAULT HISTORY FOR LEG 1 LOGGED CHANNEL A ELEVATOR SYNC INV, 4 SDR ASAA2015111313759Autopilot Sys · disengagedSECOND AUTOPILOT DISENGAGED DURING PRACTICE AUTOLAND PRIOR TO 1500 AGL OTHER AUTOPILOT WAS DISENGAGED MANUALLY AND HAND FLOWN TO LANDING, NO OTHER DEFECTS NOTED. ACFT GROUNDED. ACCOMPLISHED CURRENT STATUS TEST FOR CHANNEL B REF MM 22-11-00, ALL TESTS PASSED.SDR ASAA2015111113730Valve · failedFWD CAB & AFT CAB TEMP CONTROLLERS FAIL TO CONTROL CABIN TEMP IN AUTO. ROWS 6-12 WERE COLD WHILE AFT CABIN WAS TOO WARM. AS FWD CAB WAS TURNED WARMER, THE FLT CABIN ALSO GOT WARMER. RUNNING CONTROLLERS IN OFF STABILIZED THE TEMP. ACFT GROUNDED. ACCOMPLISHEDSDR ASAA2015111013710Filter · dirtyF/A'S REPORT CABIN TEMP EXCESSIVELY WARM DESPITE ATTEMPS TO COOL IN AUTO. MOVED ALL 3 CABIN TEMP CONTROLLERS TO OFF, APPEARED TO RESOLVE CABIN TEMP BUT FLIGHT DECK BECAME QUITE WARM. ACFT GROUNDED. BITE TEST OF BOTH TEMP CONTROLLERS REF AMM FIM 21-61, TASK SDR ASAA2015110513663Control Valve · failedMID CABIN REPORTED EXCESSIVELY HOT. FWD AND AFT CAB CONTROLLERS SET TO COLD. FWD AND AFT CABIN COLD, MID CABIN STILL HOT IAW QRH 2.7 TURNED OFF TRIM AIR. TEMP NOW CONTROLLABLE THROUGH OUT. ACFT GROUNDED. COULD NOT DUPLICATE FAULT. PERFORMED ZONE TEMP CONSDR ASAA2015110413643Control Valve · failedFORWARD CABIN TEMPERATURE VERY WARM, ESTIMATE 90 DEGREES WITH TEMPERATURE SELECTOR IN FULL COLD POSITION. COMPLIED WITH QRH PROCEDURE AND SELECTED TRIM AIR OFF. TEMPERATURE IN CABIN RETURNED TO NORMAL. ACFT GROUNDED. COULD NOT DUPLICATE MALFUNCTION. PZTC LSDR ASAA2015102813544Warning Message · false activationFMC DISAGREE APPEARED ON THE MCDU SCRATCHPAD DURING TAXI FOR TAKEOFF. THERE HAD BEEN A 60+ SECOND POWER INTERRUPTION AT THE GATE DURING BOARDING WHEN GROUND PERSONNEL PULLED GROUND POWER WITHOUT AUTHORIZATION. ACFT GROUNDED. FOLLOWED QRH FOR FMC DISAGREE ONSDR ASAA2015102713547Autopilot Sys · inoperativeCMD A AUTOPILOT WILL NOT ENGAGE. ACFT GROUNDED. ACCOMPLISHED DFCS BITE FAULT REVIEW. NO FAULTS LOGGED FOR LAST 5 LEGS. REF FIM 22-11, TASK 801. DFCS CURRENT STATUS TEST PASSED. PERFORMED DFCS GROUP 11 AUTOPILOT AND GOUP 47 LRU REPLACEMENT TEST FOR PITCH SDR ASAA2015100713390Satcom · lockedSATCOM LOCK-UP DURING POWER TRANSFER. ACFT GROUNDED. COMPLIED WITH QRH PROCEDURE FOR SATCOM LOCK-UP. SAT PROMPT REAPPEARED.SDR ASAA2015092713231Satcom · lockedNO SATCOM PROMPT AFTER APU POWER TRANSFER, ACFT GROUNDED. SATCOM LOCKUP PROCEDURE ACCOMPLISHED. SYSTEM RETURNED TO NORMAL.SDR ASAA2015092513193Warning Light · false activationDURING CLIMBOUT VNAV COMMANDED 210K INSTEAD OF CLIMB PROGRAMED. ACFT GROUNDED. A/P A & B CHANNELS SHOW NO FAILURES IN CURRENT STATUS. FLT FAULT REVIEW SHOWS NO FAILURES. HAS NO RECENT HISTORY, 30 DAYS. ACFT REMAINS CAT I. STATUS PLACARD REFLECTS SAME.SDR ASAA2015072212547Battery · failedGROUND PWR KICKED OFF WITH BATTERY POWER ON. ACFT GROUNDED. INITIAL CK BOTH MAIN & AUX AT 12V, ELEC LIGHT ON MSG BATTERY CHARGER INOPERATIVE, AUX BATTERY CHARGER INOPERATIVE, STAT INV INOPERATIVE, AND SPCU INOPERATIVE. REPLACED MAIN & AUX BATTERY REF MM 24-SDR ASAA2015071812466Autoland Sys · no testAUTOLAND, HGS CAT 3 EVAL UNSATISFACTORY. WING ROCK AND APPROACH WARN ENCOUNTERED IN FLARE. DISCONNECTED AUTOPILOT, LANDED MANUALLY. ACFT GROUNDED. HGS SHOWS ROLLOUT CAUTION RADIO ALTIMETER 2. DFCS BITE SHOWS NO FAULTS LAST 10 LEGS. ACCOMPLISHED HGS OPS TSDR ASAA2015060511980Module · failedAFTER ENGINE START DURING RECALL "AIR COND" LIGHT ILLUMINATES ALONG WITH "ALL" 3 ZONE TEMP LIGHTS. NO TEMP CONTROL. "AIR COND" LIGHT EXTINGUISHES WITH MASTER CAUTION RESET. ACFT GROUNDED. FLT DECK AND ZONE SELECTOR FAULTS ON BOTH ZONE TEMP CONTROLLERS. REPSDR ASAA2015041611374Filter · cloggedWHILE ACCESSING APU FOR FUEL FILTER CHANGE FOUND OIL FILTER INDICATOR POPPED. ACFT GROUNDED. REMOVED FILTER AND INSPECTED BOWL AND FILTER FOR CONTAMINATION. NONE FOUND. INSTALLED NEW FILTER AND RAN APU OPS AND LEAK CHECK GOOD, REF 49-91-12-400-802.SDR ASAA2015040911301Window · bindingL2 WINDOW BINDS, DIFFICULT TO OPEN AND CLOSE. DOES NOT SMOOTHLY RUN THRU TRAVEL. ACFT GROUNDED. ADJUSTED AND OPS CHECKED L2 WINDOW IAW AMM 56-12-11.SDR ASAA2015032111183Angle · corrodedR1 DOOR CUTOUT LOWER DOOR SILL Z-ANGLE CORRODED. ACFT GROUNDED. REMOVED CORROSION, ORIGINAL THICKNESS .090 MATERIAL, REMOVED .013 REMAINING MATERIAL .077. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15 AND APB SRM 53-10-15, R & R ANGLE IAW SRM 51-40-02, REF BAC SDR ASAA2015032111082Floor Support · crackedMAIN CABIN FLOOR INTERCOSTAL FROM STA 312 TO STA 328 AT RBL 32 IS CRACKED. ACFT GROUNDED. R & R MAIN CABIN FLOOR INTERCOSTAL FROM STA 312 TO STA 328 AT RBL 32 IAW SRM 51-40-02 AND DWG 141A5400. DOT REMOVED.SDR ASAA2015032111081Floor Support · crackedMAIN CABIN FLOOR INTERCOSTAL FROM STA 312 TO STA 328 AT LBL 45 IS CRACKED. ACFT GROUNDED. R & R MAIN CABIN FLOOR INTERCOSTAL FROM STA 312 TO STA 328 AT LBL 45 IAW SRM 51-40-02, REF BAC DWG 141A5400.SDR ASAA2015032011107Floorbeam · crackedMAIN CABIN FLOOR STRUCTURE, PANEL BREAK, AT BS 540 IS CRACKED AT LBL 2. ACFT GROUNDED. REMOVED MAIN CABIN FLOOR STRUCTURE PANEL BREAK AT BS 540 IAW SRM 51-40-02, LOCATED AND DRILLED NEW PANEL BREAK IAW SRM 51-40-02 AND INSTALLED NEW PANEL BREAK AT BS 540 LBLSDR ASAA2015032011080Floorbeam · crackedMAIN CABIN FLOOR STRUCTURE, PANEL BREAK, AT BS 540 IS CRACKED AT RBL 2. ACFT GROUNDED. REMOVED CRACKED PANEL BREAK IAW SRM 51-40-02. LOCATED AND DRILLED NEW PANEL BREAK IAW SRM 51-40-05, REF BAC DWG 143A5240. INSTALLED PANEL BREAK IAW SRM 51-40-02. REMOVEDSDR ASAA2015031310930Probe · out of limitsDIAGNOSTIC REPORTS NR 2 ENGINE TREND DATA SHOWS A SHIFT IN DELTA CRUISE AND TAKEOFF MARGIN INDICATIVE OF EGT INDICATION ERRORS. ACFT GROUNDED. TSR COMPLETED, FOUND S4 EGT PROBE OUT OF LIMITS, R & R PROBE REF 77-21-01, PASSED EEC TEST REF 73-21-00.SDR ASAA2015022610808Unknown · unknownRADAR SHOWS CONSISTENT RETURNS RIGHT OF CENTERLINE AT APPX 50-70 NM WHEN NO WEATHER ACTUALLY EXISTS. RADAR TEST PATTERN USUAL DISPLAY NORMAL. LATER ON IN FLIGHT THE RETURNS WRITTEN ABOUT, THIS ENTRY, DISAPPEARED - DISPLAY HAD NORMAL PRESENTATION. MAINTENANCESDR ASAA2015022110718Satcom · lockedSATCOM LOCK-UP. ACFT GROUNDED. PERFORMED SATCOM LOCK-UP PROCEDURE SUCCESSFUL. OPS RESTORED.SDR ASAA2015021210642Flange · crackedNR 2 ENGINE REAR FLANGE ASSY IS CRACKED AT ALL 8 BOLT HOLE LOCATIONS. ACFT GROUNDED. R & R NR 2 ENG REAR FLANGE ASSY IAW MM 72-56-00. PERFORMED IDLE POWER LEAK CHECK IAW MM TASK 71-00-00-700-801-F00. NO LEAKS NOTED AT THIS TIME.SDR ASAA2015011010194Radio · malfunctionedHF 1 FREQUENCY INDICATOR WILL SHOW "FAIL" SHORTLY AFTER SETTING FREQUENCY. RADIO WORKS FINE. ACFT GROUNDED. VERIFIED, CYCLED VHF 1 COMM CIRCUIT BREAKER FAULT WENT AWAY. ACCOMPLISHED HF BITE REF FIM 23-11, TASK 801, NO FAULTS, NO HISTORY PAST 30 DAYS. CONTRSDR ASAA2014122710073Wire Harness · shortedCIRCUIT BREAKER ENGINE NR 1 ENGINE & WING CONTROL IS OUT. REMAINED ON AFTER TAKEOFF AND IT SHOULD HAVE TRIPPED TO OFF. ACFT GROUNDED. PERFORMED FIM TASK 30-11, TASK 810, CIRCUIT BREAKER C148 OPENS INTERMITTENTLY. DURING TROUBLESHOOTING FOUND CIRCUIT BREAKESDR ASAA2014122210036Sign · detachedF/A REPORTS EXIT ROW SIGN HANGING BY A THREAD. ACFT GROUNDED. REINSTALLED EXIT SIGN AS REQ. OPS CHECK NORMAL.SDR ASAA2014122010016Processing Unit · failedCENTER TANK INDICATOR BLANKED DURING FLIGHT WITH ZERO FUEL IN TANK. ACFT GROUNDED. REPLACED FQPU, OPS TEST GOOD, MM 28-41-81.SDR ASAA2014112709784Warning Light · illuminatedNR 2 ENGINE VALVE CLOSED, LIGHT REMAINED ILLUMINATED BRIGHT BLUE AFTER ENGINE SHUTDOWN. ACFT GROUNDED.SDR ASAA2014112409739Warning Message · false activationCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED DURING RECALL, EXTINGUISHES ON RESET. ACFT GROUNDED. ACCOMPLISHED BITE CHECK OF BOTH TEMP CONTROLLERS IAW FIM TASK 21-62, TASK 801 & NO FAULTS FOUND. ACCOMPLISHED FIM TASK 21-62, TASK 832 AND FOUND TO BE AN INTERMISDR ASAA2014102509485Probe · faultedWHILE PERFORMING T/C 78273000, FOUND NR 2 ENGINE FAULT 77-20872 TOP LT EGT SIGNAL, 49554, OUT OF RANGE. ACFT GROUNDED. R & R T49.5 S1, PROBE ASSY REF AMM 77-21-01. OPS TEST GOOD. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2014102309471Anti-Ice Valve · failedNR 1 ENG "COWL VALVE OPEN" LIGHT DOES NOT ILLUMINATE WHEN SELECTED ON. ACFT GROUNDED. FOUND ENGINE AND WING CONTROL ENGINE 1 CIRCUIT BREAKER TRIPPED ON P18-2. ACCOMPLISHED CIRCUIT BREAKER PROCEDURE IAW 20-60-01. NO DEFECTS NOTED. DUE TO HISTORY SUSPECT ANTSDR ASAA2014101509397Circuit Breaker · trippedWING ANTI-ICE LIGHT WILL NOT TEST. LT COWL VALVE ANTI-ICE LIGHT WILL NOT TEST. ACFT GROUNDED. FOUND P18-3 A6 ENG 1 & WING ANTI ICE CONT CIRCUIT BREAKER OUT. CHECKED BEHIND P18-3 PANEL FOR CONTAMINATION OR DEFECTS, NONE NOTED. RESET CIRCUIT BREAKER IAW SWPM SDR ASAA2014100909332Connector · corrodedENGINE VALVE CLOSED LIGHT ILLUMINATED DURING COCKPIT PREFLIGHT. ACFT GROUNDED. TSR ISSUED. ACCOMPLISHED STEP NR 3 OF TSR. NO DEFECTS NOTED. REPLACED PASS-THROUGH DM6. ACCOMPLISHED STEP 4 OF TSR. FOUND CORROSION ON D30116 SIDE OF DM24 PASS THROUGH. REPLACESDR ASAA2014100709325Apu · unknownAPU DID NOT START. TWO ATTEMPTS MADE. FAULT CODE 49-41012. ACFT GROUNDED. PERFORMED FIM TASK 49-40-803. UNABLE TO DUPLICATE PROBLEM . STARTED APU FOUR TIMES IAW AMM 49-11-00-860-801.SDR ASAA2014100309288Sensor · dirtyCONT CAB ZONE TEMP LIGHT ILLUMINATED UPON RECALL EXTINGUISHES UPON RESET. ACFT GROUNDED. BITE CK PACK/ZONE CONT FOUND FLT DECK SENSOR, CLEANED FLT DECK SENSOR OPS PACK. BITE CK NO FAULTS FOUND REF FIM 21-62, TASK 801 & TASK 813. NO HISTORY PAST 30 DAYS.SDR ASAA2014092009181Control Unit · failedWHILE WORKING T/C 78273000, INTERROGATE THE FMC CDU FOR ENGINE FAULTS, EEC DATA FOR CHANNEL B ON NR 2 ENG NOT AVAILABLE SHOWS. FOUND CIRCUIT BREAKER POPPED AT P6-2 ROW D, COL 7, ENG 2 ALT POWER CHANEL B. ACFT GROUNDED. REMOVED ON NR 2 EEC CONN DP0202, INSPESDR ASAA2014090309049Static Inverter · failedAFTER ENGINE START, RECEIVED AN ELECTRIC LIGHT. RETURNED TO GATE. ACFT GROUNDED. REPLACED STATIC INVERTER IAW MM 24-34-21-000-801 AND 24-34-21-400-801. OPS CHECK GOOD.SDR ASAA2014090209043Warning Light · illuminatedNR 2 ENGINE VALVE CLOSED LIGHT IS ILLUMINATED BRIGHT, WITH NR 2 START LEVER IN CUTOFF. ACFT GROUNDED. COULD NOT DUPLICATE. AS A PRECAUTION, REPLACED NR 2 ENG NACELLE WIRING HARNESS, IAW MM 71-51-03 AND WDM 76-21-21. OPS CHECKED NORMAL, PERFORMED ENGINE RUSDR ASAA2014082809012Warning Light · illuminatedAFTER ENGINE SHUTDOWN, NR 2 ENGINE VALVE CLOSED, LIGHT ILLUMINATED BRIGHT BLUE. ACFT GROUNDED. TROUBLESHOT IAW FIM 73-06, TASK 804, NO DEFECTS FOUND. DUE TO HISTORY, REPLACED P5-2 PANEL. OPS CHECKED GOOD.SDR ASAA2014082308919Battery Pack · no testWHILE PERFORMING TASKCARD 78233001, EMERGENCY LIGHTS OPERATIONS & BATTERY PACKS FUNCTIONAL CHECK AFT LEFT SECTION OF EMERGENCY LIGHTS FAILED AFTER FOUR MINUTES. ACFT GROUNDED. REPLACED AFT LT BATTERY PACK IN THE GALLEY AREA IAW MM 33-51-06, SYSTEM OPS CHECKESDR ASAA2014082308913Warning Message · false activationAFTER BOTH ENGINE STARTED, RECEIVED A PACK TRIP OFF ON RT SIDE DURING MASTER CAUTION CHECK. PACK TRIP LIGHT EXTINGUISHED ON RESET. QRC COMPLETED. ACFT GROUNDED. PERFORMED FIM 21-62 TASK 801, NO FAULTS NOTED. PRESSING RESET SWITCH SHOWS VERIFY AND GO. NO FASDR ASAA2014082008901Autopilot Sys · malfunctionedDURING CLIMB OUT AT APPROXIMATLY 12000 FEET, AUTOPILOT A WAS ENGAGED AND IMMEDIATLEY BUMPED AND STARTED TO CLIMB AT ABOUT 2000 FPM. AUTOPILOT WAS DISENGAGED AND SWITCHED TO AUTOPILOT B AND OPERATED NORMALLY. ACFT GROUNDED. OPENSDR ASAA2014081908890Computer · failedDURING CLIMB BETWEEN 12,000 AND 17,000 FT, THE A AUTOPILOT WAS ENGAGED AND IT IMMEDIATELY "PUMPED" THE YOKE ONCE, FELT BY EVERYONE AND THEN IT SEARCHED FOR A VERTICAL SPEED TO MAINTAIN, VARYING BY 2,000 FPM. IT WAS DISCONNECTED AND A 2ND ATTEMPT MADE WITH SAMSDR ASAA2014080708795Warning Light · illuminatedDURING SHUTDOWN OF NR 2 ENGINE, VALVE CLOSED LIGHT REMAINS ILLUMINATED BRIGHT BLUE. ACFT GROUNDED.SDR ASAA2014072708695Satcom · malfunctionedNO SATCOM PROMPT WHILE ON GROUND. ACFT GROUNDED. QRH SATCOM GROUND RESET PROCEDURE DONE. SATCOM NOW APPEARS ON MENU PAGE.
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