N568AS
Service difficulty reports · 479
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 = 'N568AS' 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 = 'N568AS' 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 ASAA2021072635602Actuator · faultedWHILE PERFORMING TASK CARD 78273000, #2 ENG HAS SHORT TIME FAULT 75-10452 THE VBV POSITION SIGNALS DISAGREE, ON MUILTIPLE FLIGHT LEGS. GROUNDED - YES. REMOVED AND REPLACED R/H VBV ON #2 ENGINE PER TECH SERVICES RECOMMENDATION, REF B737-800 AMM 75-32-02-400-802SDR ASAA2021072135468Fuel Filter · cloggedAFTER LANDING ENG #1 FILTER BY-PASS LIGHT ILLUMINATED. GROUNDED - YES. RELEASED PER MEL 73-4B #1 ENGINE FUEL FILTER DIFFERENTIAL WARNING SYSTEM INOP. DRAINED FUEL FROM FILTER HOUSING NO GROSS CONTAMINATION NOTED PER B737-800 AMM 73-11-02-400-801 FUEL FILTER NOSDR ASAA2021071135381Connector · dirtyWHILE ACCOMPLISHING T/C 78273000, FOUND # 2 ENG MAINTENANCE MESSAGE: # 75-30452. THE VBV POSITION SIGNALS DISAGREE. SHORT TIME FAULT.DEFERRED PER T/C 78273000. GROUNDED - YES. EEC BITE PER T/C 78273000 SHOWED #2 ENGINE FAULT 75-30452 LOGGED FOR ONLY LEG 10 BUTSDR ASAA2021070835347Motor · failedPRIOR TO ETOPS ENTRY POINT THE L LOW PRESSURE LIGHT FOR CENTER FUEL PUMP ILLUMINATED. GROUNDED - YES. DIVERSION TIME 49 MINUTES - REMOVED AND REPLACED L/H CENTER FUEL PUMP REF B737-800 AMM 28-22-41.OPS LEAK CHECK GOOD. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2021062235151Fmc · malfunctionedFMC #2 WENT MOMENTARILY INOP IN CRUISE FOR ABOUT 10 SECONDS. GROUNDED - YES. REF B737-800 FIM 34-61 TASK 807. FMCS BITE TESTED GOOD W/O FAULTS.SDR ASAA2021061035089Tube · crackedRIGHT SIDE BLEED AIR DUCT PRESSURE IS 7-8 PSI WITH ENGINE AT IDLE THRUST AND ENGINE OFF. GROUNDED - YES. REPLACED THE BAR REF B737-800 AMM 36-11-03. LK CK GOOD. DURING ENGINE RUN BLEED AIR STILL READS 8 PSI MAX. CYCLING SWITCH OFF BLEED AIR GOES TO ZERO. NO HESDR ASAA2021060335032Connector · unsecureCOWL VALVE OPEN LIGHT ON WITH SWITCH IN OFF POSITION. GROUNDED - YES. ACCOMPLISHED GVI OF #2 ENGINE TAI VALVE, FOUND CONNECTOR DP1302 LOOSE. RE-SECURED CONNECTOR IAW B737-800 AMM 30-21-11. OPS CHECK OKSEAMC CARLOS NOTIFIED.SDR ASAA2021051434810Actuator · out of rigINFO ONLY AUTOLAND NOT SUCCESSFUL. GROUNDED - YES. ACCOMP LAND VERIFY TEST REF B737-800 AMM 22-11-00/201. TEST FAILED FOR AIL POS SEN-2 AND AIL POS SEN-1. REMOVED AND REPLACED AIL POS SEN REF AMM 22-11-29-400-801. NO HELP. REPLACED THE AILERON POSITION SENSOR SDR ASAA2021050234715Warning Message · false activationWHEN POWER APPLIED TO ACFT, A MODE CONTROL PANEL LOCKED UP INDICATION DISPLAYED. GROUNDED - YES. PERFORMED MODE CONTROL PANEL TEST IAW FIM 22-11 TASK 803 MCP AUTOTEST PASS, ALL INTERACTIVE TESTS PASSED . NO FURTHER DEFECTS NOTED.SDR ASAA2021041834625Fault Message · false activationENG #1 FAULT MSG 76-11361THE START LEVER SIGNALS DISAGREE LONG TIME FAULT DEFERRED PER T/C 7827300. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 76-11 TASK 801 INITIAL EVALUATION #1 ENG FAULT MSG 76-11361 IS NO LONGER ACTIVE IN RECENT FAULTS AND IN FAULT HISTORY.SDR ASAA2021041634608Sensor · failedWHILE CHECKING APU OIL FROM FLT DK, - NOT ABLE TO CHECK - SHOWS UNKNOWN. GROUNDED - YES. BITE CHECK OF APU PER B737-800 FIM 49-60 TASK 801 SHOWS MSG 49-94304 OIL LEVEL SENSOR SHOWS CIRCUIT FAILURE. PULLED AND TAGGED 2 CB'S TO CHECK OIL LEVEL SENSOR ON APU. CHESDR ASAA2021041334566Fmc · faultedLEFT FMC SCREEN HAS LINE GOING THROUGH IT FROM L3 TO R3 BUTTONS. GROUNDED - YES. CONFIRMED DEFECT - CAPTAIN'S MCDU DISPLAY HAS FAILED LINE OF PIXELS. REMOVED AND REPLACED MULTIFUNCTION CONTROL UNIT DISPLAY REF B737-800 AMM 36-61-01/401. OPS CHECK GOOD. NO OTHESDR ASAA2021041034569Vbv · faultedACCOMPLISHING T/C # 78273000, # 2 ENG FAULT CODE: 75-10452.THE VBV POSITION SIGNALS DISAGREE. SHORT TIME FAULT.DEFERRED PER T/C # 78273000. GROUNDED - YES. PERFORMED B737-800 FIM 75-32 TASK 803 INITIAL EVALUATION NO CURRENT FAULTS NOTED AND NOTHING IN FAULT HISDR ASAA2021031034482Skin · crackedR/H HORIZONTAL STAB. LOWER SKIN AT AFT SPAR, FWD OF FWD ROW FASTENERS @ STAB.STA. 101.90 + 4" MARKED 1.550"L CRACK FOUND. GROUNDED - YES. REPAIRED HORIZONTAL STAB. LOWER SKIN AND RIB FITTING IAW B737-800 SRM 55-10-01-2R-11 REPAIR 11 AND ALASKA EA 800-55EA-2333SDR ASAA2021030734410Bulb · burned outR2 DOOR EXTERIOR EXIT EMERGENCY LIGHT INOP. GROUNDED - YES. RELAMPED R2 DOOR SLIDE LIGHT AND OPS CHECK GOOD IAW ASA B737-800 AMM 33-51-04-960-801.SDR ASAA2021022634207Start Valve · inoperativeENG 2 WON'T START FURTHER T/S NEEDED. GROUNDED - YES. R/R START VALVE ENG #2 REF B737-800 AMM 80-11-03-000-801-F00. OPS CHK GOOD. READY FOR SERVICE.SDR ASAA2020030532352Wire Harness · brokenENG FIRE SWITCH HANDLE LIGHT LOOP B INOP. GROUNDED - YES. VERIFIED, FOUND HERMETICAL SEAL BROKEN AT RIGHT CORE. REMOVED AND REPLACED #2 ENG FIRE DETECTOR WIRE HARNESS PER B737-800 AMM 26-11-02 OPS CHECK GOOD.SDR ASAA2020022832332Regulator · crackedWHILE WORKING DEFECT 12184716, FOUND BLEED AIR REGULATOR HAS A CRACK AT CONNECTOR DP1102 RECEPTACLE LOCATION ON #2 ENGINE. GROUNDED - YES. REMOVED AND REPLACED BLEED AIR REGULATOR, REF B737-800 AMM 36-11-03, OPS CK GOOD AND LEAK CK GOOD.SDR ASAA2020030232337Eec · faultedWHILE ACCOMPLISHING T/C 78273000, FOUND A LONG TIME FAULT ON #2 ENGINE, F/N 73-30782 "INTERNAL EEC FAULT. BSV POSITION SIGNALS DISAGREE. GROUNDED - YES. ON DEFERRAL.SDR ASAA2020022532336Wire Harness · faultyWHILE ACCOMPLISHING T/C 78273000 FOUND A SHORT TIME FAULT ON THE #2 ENG, FAULT # 73-30652, "THE BSV POSITION SIGNALS DISAGREE". GROUNDED - YES. REMOVED & REPLACED J9 HARNESS, REF B737-800 AMM 73-21-06-000-802-F00, PERFORMED FADEC SYSTEM TEST GOOD AMM 73-21-00-SDR ASAA2020022193229Eec · faultyNUMBER 2 ENGINE "ENGINE CONTROL" BRIEFLY ILLUMINATED ON CLEARING RUNWAY AFTER LANDING. DOES NOT ILLUMINATE ON RECALL. GROUNDED - YES. PERFORMED EEC BITE CHECK PER B737-800 FIM 73-00-801 NOTED FAULT CODE 73-30652. REMOVED & REPLACED #2 ENGINE EEC REF B737-800 MSDR ASAA2020021732210Eec · faultedREF T/C 78273000. #2 ENG LONG TIME FAULT. MAINT MSG 73-10782, INTERNAL EEC FAULT BSV POSITION SIGNALS DISAGREE. GROUNDED - YES. INTERROGATED FMC CDU FOR NO 2 ENG FAULT MSG 73-10782 AND FOUND THIS MESSAGE WAS NO LONGER ACTIVE AT THIS TIME. REF TECH SERVICES NOTSDR ASAA2020021732211Heat Exchanger · leakingFOUND FUEL LEAK ON #1 ENG AT GASKET BETWEEN FUEL-OIL HEAT EXCHANGER AND FUEL PUMP. GROUNDED - YES. REMOVED AND REPLACED THE MAIN OIL/FUEL HEAT EXCHANGER AND TORQUED ATTACHING HARDWARE REF B737-800 AMM 79-21-02/401 LEAK CK GOOD.SDR ASAA2020021283156Eec · no testDISCOVERED FAULT WHILE PERFORMING EEC BITE TEST: "MSG NBR: 73-20782, INTERVAL EEC FAULT. BSV POSITION SIGNALS DISAGREE FLIGHT LEG 1 AND 3 SET." LONG TIME FAULT. DEFERRED PER T/C 78273000. GROUNDED - YES. INTERROGATED FMC CDU FOR NO 2 ENG FAULT MSG 73-20782 ANDSDR ASAA2020020762096Blade · damagedWHILE ACC TC 78472010 FOUND CU-NI DAMAGE BEYOND LIMITS BLADES #2 S/N DD458810-0, #4 S/N DD456025-R, #6 S/N DD455884-0, #7 DD458997-9, #8 S/N DD458595-0, #12 S/N DD457490-M, #14 S/N DD455964-0, #19 S/N DD458135-7, #20 S/N DD457825-1, #22 S/N DD452812-7, #24 S/NSDR ASAA2020020632095Spacer · debondedESN 894424. FAN BLADE SPACERS #9, 15, 16 HAVE DISBOND. GROUNDED - YES. REMOVED & REPLACED SUBJECT SPACERS IN CONJUNCTION WITH TASK CARD 78472010 UNDER W/O 1026210.SDR ASAA2020020632094Platform · debondedESN 894424. ELASTOMER DISBOND ON PLATFORMS #5, 6, 15, 17, 22. GROUNDED - YES. REMOVED & REPLACED SUBJECT PLATFORMS IN CONJUNCTION WITH TASK CARD 78472010 UNDER W/O 1026210.SDR ASAA2020020383019Control Unit · inoperativeMCP HEADING WINDOW UNREADABLE. GROUNDED - YES. REMOVED AND REPLACED DFCS MODE CONTROL PANEL REF B737-800 AMM 22-11-34/401. ACCOMPLISHED MCP INSTALLATION TEST AND THE LLM MAINTENANCE TEST FOR MCP REF AMM 22-11-34-740-801 AND AMM 22-11-34-400-801 STEP F.SDR ASAA2020012982005Warning Light · false activation#2 ENG CONTROL LIGHT ILLUMINATED UPON LANDING AND EXTINGUISHED AT BLOCK IN. GROUNDED - YES. CW/ EEC BITE PROCEDURE B737-800 FIM 73-00 TASK 801 FAULT CODES 73-10652 BSV IS ALWAYS CLOSED. ENG CONTROL LIGHT FAULT. ALSO FOUND 73-20652,73-10782,73-20782 . C/W ACTUASDR ASAA2020010631750Acoustic Panel · delaminatedWHILE DOING INLET INSPECTION #2 ENGINE TC 78472000 FOUND AFT ACOUSTICAL PANEL #6 POSITION DELAMINATED. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE AFT ACOUSTICAL PANEL #6 POSITION REFB737-800 AMM 72-23-02/400SDR ASAA2019110631299Eec · failedWHILE ACCOMPLISHING T/C 7827300 FOUND FAULT CODE 75-20452, #2 ENGINE. THE VBV POSITION SIGNALS DISAGREE, SHORT TIME FAULT. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE EEC REF B737-800 AMM 73-21-60 OPENED/RESET 4 EA C/B P6-2. ALL GND FUNCTIONAL TESTS PASS. PSDR ASAA2019110541241Regulator · no testAFTER BOTH ENGINES STARTED AND AT IDLE THRUST RIGHT DUCT PRESSURE READ 10 PSI LEFT DUCT PRESSURE READ 15. GROUNDED - YES. ACCOMPLISHED #2 ENG BLEED AIR SYS HEALTH CK REF B737-800 AMM 36-11-00. HIGH STAGE REG FAILED TEST. REPLACED HIGH STAGE REGULATOR REF AMM 3SDR ASAA2019090430658Actuator · faultyWHILE PERFORMING T/C 78273000 #2 ENG FOUND FAULT CODE #75-10442 VBV SIGNAL OUT OF RANGE. GROUNDED - YES. REF TSR703795 REMOVED AND REPLACED #2 ENGINE RT VBV ACTUATOR S/N YU023186-K PER AMM 75-32-02. OPS CHECKS AND LEAK CHECKS GOOD. GROUND VERIFICATION SUCCESSFSDR ASAA2019090430611Wire Harness · damagedWHILE ACCOMPLISHING TC N8420001, RIGHT ENGINE- ENGINE HARNESS INSPECTION, FOUND DAMAGE TO J10 HARNESS NEAR CJ9 CONNECTOR. GROUNDED - YES. REMOVED AND REPLACED J10 HARNESS, ROUTED HARNESS AND CONNECTED ALL CONNECTORS REF AMM 73-21-06-400, ALL OPS NML. REF AMM 7SDR ASAA2019082643474Sign · detachedFA REPORTS FWD GALLEY EXIT SIGN IS FALLING DOWN. GROUNDED - YES. SECURED PANEL FWD GALLEY ABOVE CABIN DOOR OPS GOOD.SDR ASAA2019081430400Actuator · leakingFUEL OBSERVED LEAKING OUT FROM BOTTOM OF NR 2 ENG COWL. GROUNDED - YES. REPLACED THE RH VARIABLE BLEED VALVE ACTUATOR ON THE #2 ENGINE. REF B737-800 AMM 75-32-02. NO LEAKS NOTED AT THIS TIME.SDR ASAA2019081643403Computer · failedCOPILOT'S FLIGHT DIRECTOR FLAG ON. GROUNDED - YES. AMM 22-11-33/401. ACCOMPLISHED ALT DEACTIVATION REF CH5 TABLE 3 ITEM 1. REMOVED AND REPLACED FCC-B. REVERSED ALT DEACTIVATIONS. OPS TEST NORMAL. REF HGS-4000 SMM 34-36-00. ACCOMPLISHED HGS OPS TEST. ALL LLM RESDR ASAA2019081543399Warning Light · false indicationMACH TRIM FAIL ILLUMINATED WHEN MASTER RECALL IS PUSHED. LIGHT GOES OUT WHEN RESET. GROUNDED - YES. PERFORMED DFCS BITE REF B737-800 FIM 22-11 TASK 801. FOUND FAULT CODE 22-11317. ACCOMPLISHED FIM 22-14 TASK 801 AND LRU REPLACEMENT TEST REF FIM 22-11 TASK 802.SDR ASAA2019081203366Fmc · malfunctionedAT CRUISE ALTITUDE, WITH FO'S AUTOPILOT ENGAGED, FMC AMBER LIGHT ILLUMINATED. A/P REVERTED TO CWS AND ALT HOLD. ON FO'S PFD A LANDG ALT AND ON THE FO MFD A VTK ANNUNCIATION WAS OBSERVED FOR ABOUT 30 SECONDS. CAPTAINS SIDE REMAINED NORMAL WITH NO FLAGS. NEVER RSDR ASAA2019080230270Warning Light · false activationPACK LIGHT ILLUMINATED ON RECALL LIGHT EXTINGUISHED UPON PRESSING MASTER CAUTION TO RESET. GROUNDED - YES. RAN PACK/ZONE TEMP CONTROLLER BITE TEST FOUND TCV FAULT RAN SYSTEM CHECK REF B737-800 AMM 21-61-00 SYSTEM OP CHECKS GOOD RESET TEMP CONTROLLER NO DEFECTSSDR ASAA2019071230029Indicator · inoperativeDURING FUELING, #2 FUEL TANK INDICATOR AT RIGHT WING FUELING STATION BLANKED OUT AND DISPLAYED ERRATIC SYMBOLS. GROUNDED - YES. REMOVED AND REPLACED #2 FUEL TANK INDICATOR, OPS CHECK GOOD, REF AMM 28-41-61. A/C RETURNED TO NORMAL CONFIGURATION.SDR ASAA2019070429959Shutoff Valve · failedAFTER TAKEOFF, ANTI-SKID LIGHT ILLUMINATED AND REMAINED ILLUMINATED. HYDRAULIC QUANTITY/PRESSURE NORMAL, ALL CB'S IN. GROUNDED - YES. DIVERSION TIME 17 MINUTES. PERFORMED BITE TEST OF AACU AND FOUND MAINT MSG FOR PARKING BRAKE REF FIM 32-42 TASK 801. ACCOMP FISDR ASAA2019062869843Connector · disconnectedON TAXI IN, #1 ENGINE FUEL FILTER BYPASS LIGHT CAME ON . NO OTHER ABNORMALITIES OBSERVED WITH ENGINE. GROUNDED - YES. OPENED COWL AND NOTICED CANNON PLUG DISCONNECTED FROM FUEL FILTER BYPASS SWITCH. INSTALLED CANNON PLUG TO F.F.B SWITCH AND RAN ENG WITH NORMALSDR ASAA2019053029522Pump · low pressureA/C RIGHT FWD MAIN TANK FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT QRH CHECKLIST COMPLETED PUMP POSITIONED OFF. GROUNDED - YES. REPLACED RIGHT FWD MAIN TANK FUEL BOOST PUMP REF B737-800 AMM 28-22-41. ACCOMPLISHED FUEL BOOST PUMP OPERATIONAL TEST REF AMSDR ASAA2019052229459Fmc · failedRIGHT FMC FAIL IN CRUISE FLIGHT. GROUNDED - YES. RMVD & RPLCD #2 FMC COMPUTER IAW AMM 34-61-02/401, ETOPS GROUND FUNCTIONAL CHECK GOOD IAW AMM 34-61-02-400-801, AXC11.0 SOFTWARE HAS BEEN PROPERLY LOADED IAW AMM 34-61-00/201, ETOPS SIGNIFICANT SYSTEM MAINTENANCSDR ASAA2019052229447Fmc · malfunctionedRIGHT FMC FAIL. GROUNDED - YES. REBOOTED BOTH FMC 1 & 2 IAW FIM 34-61 TASK 836. NO MAP & VTK INDICATION SHOWING. CHECKED GOOD. OPS NORMAL.SDR ASAA2019052129448Fmc · malfunctionedRIGHT FMC FAILED IN CRUISE. GROUNDED - YES. RELEASED PER MEL 34-36J RIGHT HAND FMC IS INOP. PERFORMED FIM 34-61 TASK 836, FMC DOES NOT OPERATE. NO FAULT FOUND. CHECKED GOOD. OPS NORMAL. CLERED MEL 34-36J.SDR ASAA2019052029428Fmc · malfunctionedR FMC FAILED ON DESCENT. GROUNDED - YES. PERFORMED FIM 34-61 TASK 836 RESET FMC OPS CHECK GOOD.SDR ASAA2019051529350Warning System · false activationON CLIMBOUT PASSING 36,000 FT, MASTER CAUTION ILLUMINATED WITH NR 2 FORWARD FUEL LOW PRESSURE LIGHT ON, RAN QRH, FWD FUEL PLACED TO OFF, AFT FUEL PUMP OK. GROUNDED - YES. PERFORMED FUEL BOOST PUMP OPS CHECK ON NR 2 FWD PUMP PER AMM 28-22-41, OPS CHECK GOOD, GRSDR ASAA2019051529345Warning System · false activationCONT CAB ZONE TEMP LITE ILLUMINATED AFTER START ON RECALL, EXTINGUISHES ON MASTER CAUTION RESET. GROUNDED - YES. RELEASED PER MEL 21-21G, PRIMARY FLT DECK TEMP CONTROL - INOP. PERFORMED BITE ON NR 1 & 2 ZONE TEMP CONTROLLERS PER FIM 21-62 TASK 801, OPS CHECK G
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