N468AS
Service difficulty reports · 262
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 = 'N468AS' 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 = 'N468AS' 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 ASAA2017031720209Display · intermittentLEVEL AT FL320 VTK ILLUMINATED ON CAPTAIN'S INBOARD DU FOR APPROXIMATELY 1 MINUTE THEN EXTINGUISHED. ACFT GROUNDED. IAW FIM 34-61 TASK 836, APPEARS TO HAVE BEEN AN INTERMITTENT FAULT.SDR ASAA2017031120120Lens · detachedL1 DOOR EMERGENCY LIGHT LENS FELL OFF. ACFT GROUNDED. INSTALLED THE LENS.SDR ASAA2017021219789Fmc · malfunctionedVTK CAME ON INTERMITTENTLY, RECOVERED WITH NO ACTION ON THE PILOT SIDE. ACFT GROUNDEDS. COULD NOT DUPLICATE. PERFORMED FIM 34-61 TASK 836. LEFT FMC OPS NORMAL.SDR ASAA2017011919483Warning System · false activationON TAXI IN FMCS FAILED WITH AMBER "LDG ALT" AND "VSPD" FLAGS ON DISPLAY. GROUNDED - YES. NO HISTORY 30 DAYS PERFORMED FIM 34-61 TASK 801 NO FAULTS NOTED.SDR ASAA2017011119320Switch · failedAUTOTHROTTLES WILL NOT ENGAGE. ACFT GROUNDED. A/T CURRENT STATUS ATTEMPTED, A/T WILL NOT ENGAGE. FOUND THE NR 1 A/T SWITCH NOT CLICKING, SUSPECT BAD SWITCH. FAULT CONFIRMED WITH INPUT FAILED THE TEST. REMOVED AND REPLACED A/T DISENGAGE SWITCH. INSTALLATION TESDR ASAA2016121219023Heater · failedRIGHT SIDE WINDOW HEAT ILLUMINATED AT FL 340 , PERFORMED QRH PROCEDURES , LIGHT REMAINED ILLUMINATED. ACFT GROUNDED. REPLACED THE NR 2 WINDOW IAW AMM 56-12-11 . R2 WINDOW ADJUSTED NR 2 WINDOW IAW AMM 56-12-11. PERFORMED PRESSURE CHECK IAW AMM 05-51-91, OPS CSDR ASAA2016120218914Module · failedAMBER TAI INDICATION OCCURED AFTER STOWING ENGINE ANTI ICE ON UPPER DISPLAY UNIT IN FLIGHT. AFTER RECYCLING ENGINE ANTI-ICE SWITCH THE AMBER TAI INDICATION DISAPPEARED. AMBER TAI INDICATION WAS ON NR 2 ENGINE. ACFT GROUNDED. REMOVED AND REPLACED THE ENGINE SDR ASAA2016120118913Valve · failedAMBER TAI INDICATION ON NR 2 ENGINE WITH ENGINES SHUT DOWN AT GATE. ACFT GROUNDED. REMOVED AND REPLACED THE NO. 2 ENGINE COWL TAI VALVE IAW AMM 30-21-11-401-801 & 000-801 & 000-802. NR 2 COWL TAI VALVE OPS CHECKED NORMAL IAW AMM 30-21-11-400-801. NR 2 ENGINESDR ASAA2016112818874Warning Message · false activationRIGHT SIDE WINDOW HEAT CAUTION LIGHT ILLUMINATED, RESET SWITCH IAW QRH, CAUTION LIGHT ILLUMINATED AGAIN. ACFT GROUNDED. ACCOMPLISHED BITE CHECK OF RIGHT SIDE WHCU. BIT TEST OK. ACCOMPLISHED WINDOW HEAT SYSTEM OPERATIONAL TEST, TEST PASSES FOR RIGHT SIDE WINDOWSDR ASAA2016111918734Valve · failedRIGHT A/C PACK LIGHT ILLUMINATED ON RECALL AND EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED RIGHT PACK, ZONE TEMP CONTROLLER BITE TEST IAW AMM 21-60-00. NO FAULTS. LIGHT REMAINS EXTINGUISHED ON RECALL. REMOVED AND REPLACED RIGHT TEMPERSDR ASAA2016111918747Pump · leakingNR 1 ENGINE FUEL PUMP LEAKING AT THE DRAIN LINE APPROXIMATELY 1 DROP PER SECOND. ACFT GROUNDED. REMOVED AND REPLACED THE FUEL PUMP IAW AMM 73-11-01, AMM 79-21-02-400-801-F00 STEP 3. (1), AND AMM 73-11-01-400-801-F00 STEP 3 H (1,2).SDR ASAA2016103018515Warning Light · false activationRIGHT PACK LIGHT ILLUMINATED ON MASTER CAUTION RECALL. RESETS ON MASTER CAUTION RESET. ACFT GROUNDED. TROUBLESHOT THE RIGHT PACK IAW AMM 21-51-00-700-803. NO FAULTS FOUND. SYSTEM GOOD FOR CONTINUED SERVICE.SDR ASAA2016092718140Warning Light · false activationAPU FAILED TO START ON 1ST ATTEMPT. LOW OIL PRESSURE LIGHT NEVER WENT OUT, STARTED ON SECOND TRY. ACFT GROUNDED. PERFORMED BITE TEST OF APU, NO FAULT NOTED, ALSO RUN APU, OPERATIONAL WAS NORMAL.SDR ASAA2016090417891Warning Light · false activationCONTROLO CAB ZONE TEMP ILLUMINATED ON RECALL RESETS WITH M/C. ACFT GROUNDEDS. NO CURRENT FAULT ON RECALL. PACK/ZONE CONTROLLERS IAW AMM 21-61-00-700-806-002 BITE CHECKED OK. NO CURRENT FAULTS. NO HISTORY 60 DAYS. ETOPS GROUND VERIFICATION COMPLETE. RAN BOTHSDR ASAA2016082917950Spacer · debondedNR 2 ENGINE TREND DATA SHOWS A SUDDEN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. DATA SCATTER INDICATES FAN LUBE AND HARDWARE INSPECTION REQUIRED. ACFT GROUNDED. PERFORMED FAN BLADE LUBE ON NR 2 ENGINE. FOUND FOUR SPACERS DEBONDED AT 6, 12, 14 & 15. RESDR ASAA2016082517806Knob · inoperativeF/O COURSE SELECTOR KNOB INOPERATIVE. ACFT GROUNDED. COULD NOT DUPLICATE PROBLEM. PERFORMED OPS TEST OF MCP IAW AMM 22-11-34/401 ALL TESTS PASSED. PERFORMED LAND VERIFY TEST IAW AMM 22-11-00/201 & HGS SYSTEM TEST IAW AMM 34-36-00. ALL TESTS PASSED ACFT RSDR ASAA2016070917323Bottle · low pressureDURING CRUISE FLIGHT, NOTICED CREW OXYGEN GAUGE READING ZERO. IT WAS AT APPROXIMATELY 1550 PSI DURING PREFLIGHT. ACFT GROUNDED. REMOVED AND REPLACED CREW OXYGEN BOTTLE AND OPS CHECKED IAW AMM 12-15-21. PERFORMED LEAK CHECK OF OXYGEN LINE AND B-NUTS IAW AMMSDR ASAA2016062317158Pressure Switch · failedNR 2 FUEL FILTER BYPASS LIGHT ILLUMINATED. ACFT GROUNDED. R & R NR 2 ENGINE DIFFERENTIAL PRESSURE SWITCH, LEAK AND OPS CHECK GOOD, REF AMM 73-34-01. R & R FUEL FILTER AND DRAIN PLUG O-RING, OPS AND LEAK CHECK GOOD REF AMM 73-11-02.SDR ASAA2016061317029Fmc · failedRIGHT FMC FAIL, QRH FOLLOWED, SINGLE FMC OPERATIONS NORMAL. INDICATION: VTK AND MAP WARNINGS ON F/O'S ND AND SINGLE FMC OPERATION ON THE CDU SCRATCH PAD. ACFT GROUNDED. R & R RT FMC COMPUTER. OPS CHECK GOOD, REF AMM 34-61-02 AND IPC 34-61-02-02B.SDR ASAA2016060917010Engine · malfunctionedNR 2 ENGINE ATTEMPTED ENGINE START AT 56 PERCENT N2, STARTER WOULD NOT CUTOUT AND EGT WAS ROLLING BACK. ALL ENGINE PARAMETERS NORMAL, FOLLOWED QRH PROCEDURE. ATTEMPTED SECOND START OF NR 2 WITH SAME RESULTS. ACFT GROUNDED. PERFORMED ELECTRONIC ENGINE CONTROLSDR ASAA2016050416623Warning Light · false activationON APU STARTUP, FAULT, LIGHT ILLUMINATED. ACFT GROUNDED. REBOOTED ACFT POWER IAW AMM 24-30-00. OPS NORMAL.SDR ASAA2016042516552Exciter · failedENGINE NR 1 FAILED TO START IGNITION ON RIGHT. ACFT GROUNDED. R & R NR 1 ENGINE RT SIDE IGNITION EXCITER. OPS CHECK NORMAL, NO FAULTS FOUND, REF AMM 74-11-01.SDR ASAA2016031515940Warning Light · false activationLEFT PACK LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. ENROUTE MEL ACCOMPLISHED BY CREW. ACCOMPLISHED FIM TASK 21-62, TASK 802. NO FAULTS FOUND. GROUND VERIFICATION CHECKS NORMAL.SDR ASAA2016030815833Fmc · failedLEFT FMC FAIL AT CRUISE, RAN FMC FAIL CHECKLIST AND DUAL FMC OPS RESTORED. FMC FAILED A SECOND TIME. CONTINUED FLIGHT SINGLE FMC OPS. ACFT GROUNDED. R & R LT FMC COMPUTER REF AMM 34-61-02. SOFTWARE CROSSLOADS GOOD. OPS NORMAL.SDR ASAA2016022315641Fmc · failedLEFT FMC FAILED INTERMITENTLY 4 TIMES. SWITCHED TO, BOTH ON R". SEEMED TO HAPPEN DURING CRUISE WINDS REQUEST. ACFT GROUNDED. ACCOMPLISHED FMC BITE REF FIM 34-61, TASK 801. FOUND, PGM FAULT, ON LT COMPUTER WITH, PRESSURE POSITION LAT, LAST LEG AND 2 OTHER ASDR ASAA2016020915433Pump · failedNR 1 ENGINE MAIN FUEL PUMP HAS HISTORY OF FUEL LEAKAGE FROM THE PAD CAVITY DRAIN DURING ENGINE START. INTERMITTENT INPUT SHAFT SEAL LIFT OFF IS SUSPECT. ACFT GROUNDED. REMOVED NR 1 ENGINE FUEL PUMP PACKAGE REF AMM 73-11-01-000-801-F00. INSTALLED FUEL PUMP PSDR ASAA2016020615311Transceiver · failedHF1 WAS COMPLETELY GARBLED AND UNREADABLE. INITIAL SELCAL CHECK TESTED GOOD. MULTIPLE FREQUENCIES WERE ATTEMPTED. ACFT GROUNDED. R & R NR 1 HF RECEIVER/TRANSMITTER & OPS NORMAL IAW AMM 23-11-21. RECEIVE, TRANSMIT, & SELCAL ALL SATISFACTORY. GROUND VERIFICSDR ASAA2016012515002Warning Message · false activationFMC DATA LINK FULL MESSAGE ON GROUND. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMCS OPERATIONS RESTORED NORMAL.SDR ASAA2016012314960Charger · damagedAUXILIARY BATTERY SHOWS 27 VOLTS AND A CONSTANT CHARGE OF 2 AMP THROUGHTOUT FLIGHT, ABNORMAL. ACFT GROUNDED. ACCOMPLISHED AUXILIARY BATTERY CHARGER. OPS TEST REF AMM 24-31-31. OPS TEST NORMAL, NO FAULTS. DURING GVI OF AUXILIARY CHARGER FOUND ARCING DAMAGESDR ASAA2016011114723Warning Message · false activationCONTROLLER CABIN ZONE TEMP ON RECALL AT ALTITUDE QRH ACCOMPLISHED. ACFT GROUNDED. COULD NOT DUPLICATE. PZTC BITE AND VERIFY TEST GOOD, REF AMM 21-61-00.SDR ASAA2016010514651Wire Harness · damagedWHILE PERFORMING TC N842001, STEP C4 FOUND MW0326 HARNESS DAMAGED ON NR 2 ENGINE. ACFT GROUNDED. R & R MW0326 FIRE DETECTOR HARNESS, REF AMM 26-11-02. ACCOMPLISHED DETECTOR OPS TEST REF AMM 26-11-00 ON NR 2 ENGINE. SYS CHECKED NORMAL.SDR ASAA2015122314463Warning Light · false activationDURING CRUISE AT FL 340, RECEIVED AN FMC P/RST LIGHT ON FWD GLARESHIELD WITH VTK DISPLAYED ON F/O, PILOT FLYING ND FMA DROPPED OUT OF NAV, VNAV PATH TO CONTROL WHEEL STEERING AND NAV DATA DISAPPEARED ON F/O SIDE. SELECTED "A" AUTOPILOT SINCE CA SIDE OK. NO SCSDR ASAA2015112513979Warning Message · false activationFMC "DATA LINK FULL" MESSAGE. ACFT GROUNDED. PEFORMED FMC DISAGREE QRH PROCEDURE. RESTORED NORMAL.SDR ASAA2015102013482Fmc · failedAT CRUISE ALT THE RT SIDE FMC FAILED WITH AMBER VTK AND MAP FLAGS. QRH WAS FOLLOWED WITH NO SUCCESS OF RESTORATION. FMS TRANFER SWITCH TO BOTH ON LT FOR REMAINDER OF FLIGHT. ALL BREAKERS ON FLIGHT DECK IN. ACFT GROUNDED. VERFIED DISCREPANCY, PLACED FMC TRSDR ASAA2015101713516Circuit Breaker · trippedFWD LEFT FRONT CIRCUIT BREAKER OUT. ACFT GROUNDED. RESET CIRCUIT BREAKER IAW MM 20-60-01. FWD LT WINDOW HEAT, OPS CHECKED GOOD, IAW MM TASK 30-41-00-710-801. GROUND VERIFICATION TEST, OPS CK GOOD. NO HISTORY 30 DAYS.SDR ASAA2015091113024Converter · faultedAPU FAULT ON START. AFTER LANDING. ACFT GROUNDED. REPLACED APU START CONVERTER UNIT REF AMM 49-41-61. OPS CHECKS NORMAL.SDR ASAA2015090912994Warning Message · false activationAT FL 340, RT FMC FAILED VTK, FOLLOWED BY MAP FLAG. QRH 11.3 COMPLETE. DUAL OPS NOT RESTORED, CONTINUED WITH SINGLE FMC OPS. ACFT GROUNDED. UNABLE TO DUPLICATE DEFECT, RT FMC OPS NORMAL REF MM 34-61-00. NO VTK OR MAP FLAGS. SELECT SWITCH PLACED TO NORMAL.SDR ASAA2015081716475Floor Panel · damagedDENTS & GOUGES FOUND IN FWD CARGO BAY FLOOR PANEL BS 505L, BL 0. ACFT GROUNDED. FABRICATED A NEW FLOOR PANEL IAW DWG 453A1610, REV:B. R & R FLOOR PANEL IAW AMM 25-52-10.SDR ASAA2015080312711Filter · cloggedFOUND APU OIL FILTER "DELTA-P" RED INDICATOR HAS EXTENDED. ACFT GROUNDED. R & R APU OIL FILTER ELEMENT IAW AMM 49-91-13. OPS CK GOOD, LEAK CK GOOD. INSPECTION OF MAGNETIC DRAIN PLUG GOOD, NO DEFECTS NOTED.SDR ASAA2015072812617Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. RAN QRH AND RESET.SDR ASAA2015070112305Unknown · unknownCONTROL CABIN WENT TO 65 DEGREES C AFTER T/O. NOT CONTROLLABLE IN NORMAL RANGE. TURNED ALL CONTROLLERS OFF. TEMP CAME DOWN. AT FL350 CONTROL CABIN STABILIZED AT 42 DEGREES C, FWD CAB 24 C. AFT CAB 24 DEGREES C, LT PACK 29 DEGREES C, RT PACK 24 DEGREES C. SDR ASAA2015062412218Control Valve · failedON TAKEOFF THE CONTROL CABIN TEMP BECAME UNCONTROLLABLE, WENT TO 82 AND STAYED THERE EVEN WHEN OFF SELECTED. ACFT GROUNDED. REPLACED CABIN TRIM AIR VALVE IAW AMM 21-61-21. RAN BITE TEST FOR TEMP CONTROLLERS IAW AMM 21-61-00. ALL TESTS PASSED.SDR ASAA2015061512094Control Valve · faultedDURING DESCENT, THE LT PACK TEMP HIGH ILLUMINATED. ACFT GROUNDED. PERFORMED PACK ZONE TEMP CONTROLLER BITE READS TCV NR 1 CONTROLLER. REPLACED TCV IAW MM 21-51-10. CONTROLLER BITE MM 21-61-00. LEAK CHECKED AND ALL PASSED. ACFT GOOD FOR SERVICE.SDR ASAA2015061112071Fault Code · false activationDURING MASTER CAUTION RECALL, LEFT PACK LIGHT ILLUMINATED. LIGHT EXTINGUISHED WHEN MASTER CAUTION SYSTEM IS RESET. ACFT GROUNDED. NR 1 ZONE TEMP CONTROLLER WITH TEMP CONTROL VALVE FAULT. CLEARED FAULT AND BITE TESTS NORMAL IAW FIM 21-61, TASK 801. ETOPS SISDR ASAA2015060812026Not Reported · malfunctionedSHORTLY AFTER TAKEOFF, THE FLIGHT DECK AIR TEMPERATURE BECAME UNCONTROLLABLE. BECAME EXTREMELY HOT. SUPPLY DUCT TEMPERATURE IN THE CONTROL CABIN POSITION SHOWED 70 DEG C. DESPITE TURNING DOWN THE TEMPERATURE CONTROL KNOB IN AUTO AND TURNING IT TO THE OFF POSDR ASAA2015053116473Floor Panel · damagedFWD CARGO BAY FLOOR PANEL DENTED WITH A GOUGE AT BS 500C BL 0. ACFT GROUNDED. REMOVED DAMAGED FLOOR PANEL IAW AMM 25-52-10-00-801. FABRICATED A NEW FLOOR PANEL IAW DWG 453A1610, REV -. INSTALLED A NEW FLOOR PANEL IAW AMM 25-52-10-400-801.SDR ASAA2015052911901Satcom · malfunctionedSATCOM CIRCUIT BREAKER P18-2: D14 IS POPPED. ACFT GROUNDED. ACCOMPLISHED CIRCUIT BREAKER RESET PROCEDURES REF MM 20-60-01-860-801, NO DISCREPANCY NOTED. ACCOMPLISHED SATCOM OPS TEST, OPS NORMAL, REF MM 23-15-00-730-801 AND REF WDM 23-15-11/906.SDR ASAA2015051611750Pump · malfunctionedNR 2 ENGINE HAS HISTORY OF FUEL LEAKS. ACFT GROUNDED. REMOVED NR 2 ENGINE FUEL PUMP PACKAGE IAW AMM 73-11-01-000. COMPLETED FUEL PUMP PACKAGE INSTALLATION REF BOEING AMM 73-11-01-400-801-F00. GROUND VERIFICATION ACCOMPLISHED.SDR ASAA2015051511729Fmc · malfunctionedFMC DISAGREE ON GROUND AFTER FLAPS SELECTED FOR FLIGHT. ELECTRICAL EXTERNAL POWER HAD FAILED AT END OF PREVIOUS FLIGHT SO THAT INTERNAL FMC DATA WAS NOT PROPERLY CLEARED. ACFT GROUNDED. QRH PROCEDURE RESOLVED DISAGREE.SDR ASAA2015041916474Floor Panel · damagedRAMP REPORTED MULTIPLE DENTS, GOUGES AND SCRATCH LOCATED ON FWD CARGO BAY FLOOR PANEL. ACFT GROUNDED. REMOVED THE FLOOR PANEL IAW AMM 25-52-10-000-801. FABRICATED THE FLOOR PANEL IAW DWG 453A1610, REV: A INSTALLED NEW FLOOR PANEL IAW AMM 25-52-10-400-801.
Back to N468AS