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 ASAA2012100192985Warning Light · false activationAUTO FAIL LIGHT ILLUMINATED ON GROUND, COMPLIED WITH QRH PROCEDURES, SELECTED ALTERNATE AND AUTO FAIL LIGHT EXTINGUISHED. THIS PARTICULAR FAULT WAS A RECOVERABLE FAULT AND THE FAULT HAS BEEN CORRECTED AND THE CONTROLLER IS OPERATING NORMALLY.SDR ASAA2012092892968Indicator · activatedFOUND NR 1 ENG IDG DELTA P INDICATOR RED BUTTON EXTENDED. ACCOMPLISHED FIM TASK 24-11-00-810-803, T/CS 78273000 & 78424000 C/W. REMOVED NR 3 FROM DPI RESET COUNTER DECAL. DPI RED BUTTON RESET AND REMAINED RETRACTED AFTER ENGINE RUN. ETOPS GROUND VERIFICATISDR ASAA2012091892907Warning Light · false activationZONE TEMP LIGHT ACTIVATES ON RECALL EXT WITH MC RESET. TEMP CONT 2 LOGGED FLT DECK TRIM VALVE - SYS BITE TEST GOOD. FAULT RESET.SDR ASAA2012080792679Panel · damagedNR 1 ENG FAN DUCT PANEL, NR 12 HAS 1 ATTACH FASTENER PULLED THROUGH PANEL. ACFT GROUNDED. R & R NR 1 ENG, NR 12 FAN DUCT PANEL, REF AMM 72-23-07.SDR ASAA2012082592773Circuit Breaker · trippedFLIGHT DECK PREFLY AFCS INTERLINK 2 CIRCUIT BREAKER DISCOVERED TRIPPED (P6-2). ACFT GROUNDED. RESET CIRCUIT BREAKER IAW MM 20-60-01. INSPECTED WIRING BEHIND P6-2 PANEL, WIRES SHOW NO DAMAGE. PERFORMED INITIAL EVALUATION IAW FIM 22-13-00, TASK 822. NO CURRESDR ASAA2012082492771Control Valve · malfunctionedDURING MASTER CAUTION RECALL, RT PACK LIGHT ILLUMINATED. THE LIGHT EXTINGUISHES WHEN MASTER CAUTION SYS IS RESET. ACFT GROUNDED. BITE TEST OF NR 2 TEMP CONTROL VALVE HAS FAULT. CLEARED FAULT AND RAN RT PACK. NO FAULTS. LIGHT STAYED OFF, REF FIM 21-53-00-SDR ASAA2012081092691Valve · failedON CLIMB OUT DUCT PRESSURE INDICATORS WERE DISCREPANT BY 20 PSI (RGT=18PSI & LT=38PSI). IN CRUISE AT FL 360 DISCREPENCY WAS 14 PSI (RGT=22 PSI & LT=36 PSI). ACFT GROUNDED. ACCOMPLISHED TASK CARD NG-36WC-00001. FOUND PRSOV AND PRECOOLER CONTROL VALVE BAD. R SDR ASAA2012080192650Detector · inoperativeAPU DETECTOR INOPERATIVE LIGHT ON. REMOVED DEFECTIVE DETECTOR IAW AMM 26-15-01-400-802. GROUND VERIFICATION SUCCESSFUL. PERFORMED OPS CHECK IAW AMM 26-15-00. TESTED OK.SDR ASAA2012071892563Controller · malfunctionedRT PACK LIGHT ILLUMINATED WITH RECALL, EXTINGUISHES ON RESET. RESET PACK/ZONE TEMP CONTROLLER IAW MM 21-61-00, SYS. OPS CHECK GOOD.SDR ASAA2012071292542Fmc · failedON TAXI IN WITH APU PWR ON LT FMC FAIL INDICATION VTK ON CAPTAIN SIDE. ACFT GROUNDED. R & R NR 1 FMC COMPUTER IAW MM 34-61-02. SYS OPS CHECK GOOD.SDR ASAA12511649Transmitter · failedOIL FILTER BYPASS ON LANDING DURING ROLL OUT QRH PERFORMED AND SHUT THE ENGINE DOWN. ACCOMPLISHED EEC BITE FAILS WITH FAULT CODE 79-31122, NR 2 ENG OIL FILTER SIGNALS DISAGREE. BYPASS SWITCH S125, READS 2047 OHMS. REQUIRED TO BE 5 OHMS OR LESS. REPLACED SCASDR ASAA2012062792430Transceiver · inoperativeUNABLE TO TRANSMIT OR RECEIVE ON HF 2. CHANNELIZE TONE LASTED 5 SECONDS ON EACH TUNE ATTEMPT. NO SIDE TONE ON TRANSMITT. UNABLE TO HEAR WWV ON RECEIVE CHECK. VERIFIED HF 2 FROM CAPTAINS AND F/O INOPERATIVE. R & R HF 2 TRANSCEIVER, REF MM 23-11-21. OPSSDR ASAA2012061792356Display · malfunctionedON DESCENT, FOS ND DISPLAYED VTK AND MAP AND SYMBOLOGY WAS LOST FOR 20-30 SECONDS- ND RESTORED ITSELF TO NORMAL OPS WITHOUT PILOT INTERVENTION. ACFT GROUNDED. PERFORMED FMCS BITE CHECK, CHECKED GOOD, NO FAULTS AT THIS TIME REF FIM 34-61-00.SDR ASAA2012061192329Fmc · warning lightON TAXI OUT HAD FMC DISAGREE FAULT. ACFT GROUNDED. CLEARED IAW CHECKLIST QRH. OPS NORMAL.SDR ASAA12511610Shim · wornNR1 ENG FAN LUBE ALL 24 EA FAN BLADE SHIMS WORN. ACFT GROUNDED. REPLACED ALL 24 FAN BLADE SHIMS ON NR 1 ENG REF MM 72-21-02-400-801-F00 & T/C 78472002.SDR ASAA12511579Panel · wornNR 2 ENG, NR 3 &NR 4 FAN DUCT PANELS ARE WORN THRU AT ATTACH POINT. ACFT GROUNDED. REPLACED NR 3 & NR 4 FAN DUCT PANELS IAW AMM 72-23-07-400-801-F00.SDR ASAA12511555Control Valve · failedFL390, IN CRUISE POWER SETTINGS, NR 1 AT 92.2, NR 2 AT 92.1 RIGHT PAC INDICATING 15 PSI LEFT PAC AT 37 PSI. PAC BELOW MN DUCT PRESSURE OF 18 PSI AND DIFFERENTIAL PRESSURE GREATER THAN 20 PSI AT FL 390 OAT 44C ISA DEVIATION PLUS 13 DEG C. CABIN ALT AT 7000SDR ASAA12511391Heater · malfunctionedR2 WINDOW OVERHEAT LIGHTS. ACFT GROUNDED. R2 WINDOW IS A H16 TAP 1 60.1 OHMS. NO FAULT WITH SPARE SENSOR READS 289 OHMS. USED SPARE SENSOR REF WDM 30-41-11. OPS TESTED GOOD REF AMM 30-41-00.SDR ASAA12511387Shim · damagedWHILE ACCOMPLISHING FAN BLADE LUBE ON NR 2 ENGINE REF T/C 78472002 FOUND FAN BLADE SHIMS MISSING COATING ON ALL 24 SHIMS. REPLACED FAN BLADE SHIMS IN THE PROCESS OF T/C 78472002.SDR ASAA12511359Warning Light · false activationFIRST OFFICER SIDE WINDOW OVERHEATED. UNABLE TO DUPLICATE MALFUNCTION. RT SIDE WINDOW HEAT BITE CHECKED GOOD REF MM 34-41-11. WINDSHIELD HEAT CONTROL UNIT LOGGED NO FAULTS.SDR ASAA12511281Wire Harness · damagedRIGHT SIDE WINDOW HEAT. OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED QRH PROCEDURES. SWITCH OFF FOR 5 MINUTES TURNED WINDOW HEAT BACK ON AND OVERHEAT LIGHT ILLUMINATED IMMEDIATELY. TURNED SWITCH OFF FOR REMAINDER OF FLIGHT. BITE OF WHCU DOES NOT HAVE ANY CURRESDR ASAA12511278Unknown · malfunctionedRIGHT SIDE WINDOW HEAT OVERHEAT LIGHT ON. FOLLOWED QRH. AFTER 5 MIN COOLING TURNED BACK ON AND IMMEDIATELY SAW OVERHEAT LIGHT AGAIN. LEFT SWITCH IN OFF. WINDOW DID NOT FEEL EXCESSIVELY WARM TO TOUCH. TESTED RT SIDE WINDOW HEAT REF FIM 30 41 00. TESTS OK.SDR ASAA12511213Unknown · malfunctionedAPU WILL NOT TEST. RESET APU "T" HANDLE PERFORMED FIM TASK 29 10 00 810 801. OPS CHECKS GOOD.SDR ASAA12511004Unknown · malfunctionedWEATHER RADAR IN WX WX T MAP SHOWS GROUND RETURNS ON RIGHT SIDE OF NAV DISPLAY ON BOTH CAPT AND F/O'S DISPLAYS. PILOTS REPORTED THAT THERE WERE NO GROUND RETURNS ON LEFT PART OF SCREENS (BOTH CAPTAINS AND F/O'S SIDE). RESET SYSTEM AND CHECKED RADAR IAW AMM 3SDR ASAA12511006Panel · damagedWHILE ACCOMPLISHING ASA T/C 78472000 ON NR 1 ENG FOUND FASTENER ON NR 2 FAN DUCT PANEL BETWEEN NR 2 & NR 3 STRUTS PULLING THRU PANEL. UPPER CENTER FASTENER REF MM 72 23 07 000 801 F00 FIG 401. REPLACED FAN DUCT PANEL REF MM 72 23 07.SDR ASAA12510944Actuator · failedRIGHT RAM AIR DOOR OPEN LIGHT ILLUMINATED CONTINUOUSLY IN FLIGHT. RIGHT PACK LIGHT ILLUMINATES ON MASTER CAUTION RECALL. LIGHT GOES OUT ON MASTER CAUTION RESET. PERFORMED FIM TASK 21 51 TASK 803 FOUND ACTUATOR FAILED. REPLACED RAM AIR ACTUATOR RT REF MM 21SDR ASAA12510949Position Switch · faultyWHILE ACCOMPLISHING TASKCARD 78349002 FOUND FAULT MSG 49 15218 APU INLET DOOR DID NOT CLOSE. TROUBLESHOT FOUND POSITION SWITCH S284 LOOSE. TIGHTENED SWITCH IAW TASK 49 15 41 400 801. DID BITE CHECKED. FAULT CLEARED BUT THEN RE-APPEARED. SUSPECT BAD SWITCHSDR ASAA11510768Unknown · malfunctionedSTAB OUT OF TRIM LIGHT ILLUMINATED IN FLIGHT. FOLLOWED CHECKLIST AND FOUND AUTOPILOT NOT TRIMMING. MANUAL TRIMMED REMAINDER OF FLIGHT. ACCOMPLISHED FIM TASK 22 11 00 810 801, ACCOMPLISHED DFCS BITE PROCEDURES. ALL FAULTS CLEARED & DFCS BITE TEST PASSED. DSDR ASAA11510741Filter Element · unserviceableAPU OIL FILTER INDICATOR SERVICING REQUIRED PER T/C 78349013. ACCOMPLISHED APU OIL FILTER INDICATOR SERVICING REF MM 49 91 13 600 801.SDR ASAA11510721Unknown · malfunctionedLG SPLIT ON DUCT PRESSURE. 370 R25 L45. CLIMB TO 380 R25 L40. AT 380 R26 L40. AT 380 OAT 54 N1 91.8 91.7 M.80. ACCOMPLISHED RT ENGINE BLEED AIR SYSTEM HEALTH CHECK. NO DEFECTS FOUND. REF AMM 36 11 00 701 801.SDR ASAA11510651Filter · defectiveAPU LUBE FILTER DELTA P INDICATOR EXTENDED. PERFORMED OIL FILTER INDICATOR INSPECTION. REPLACED LUBE FILTER ELEMENT NO CONTAMINANTS FOUND ON MAGNETIC DRAIN PLUG. RAN APU STILL NO CONTAMINANTS FOUND ON MAGNETIC DRAIN PLUG AND FILTER HOUSING INDICATOR REMAINESDR ASAA11510650Warning System · false activationAPU FAULT LIGHT ON START. PERFORMED APU BITE MX MES 49 41010. PERFORMED FIM TASK 49 40 00 810 801 NO ACCELERATION SHUTDOWN FOR FAULT 49 41010. NO OTHER FAULTS FOUND CURRENT STATUS NO FAULT FOUND. GROUND VERIFICATION OPS CHECKS NORMAL. OK FOR CONTINUED SERVSDR ASAA11510619Processing Unit · faultyEN ROUTE THE FUEL QUANTITY INDICATOR AND THE TOTAL QUANTITY INDICATOR WOULD BLANK FOR APPROX 30 SECONDS THEN COME BACK ON. ALL OTHER INDICATIONS ARE NORMAL. INFLIGHT FAULTS LOGGED FAULT CODE 28 41109 PROCESSOR FAILURE. FOLLOWED FIM 28 41 TASK 808 REPLACED FSDR ASAA11510623Apu · failedFOLLOW UP TO REPORTS OF APU HOT START GROUNDED YES. PERFORMED APU FIRST STAGE TURBINE WHEEL INSPECTION WITH BOROSCOPE REF 49 21 00. FOUND NO WALKING OF TURBINE BLADES OR DEFECTS. PLUG REINSTALLED FROM AIR/OIL SEPERATOR ADAPTER IAW AMM 49 21 00. OPS AND LEAKSDR ASAA1150614Autoland Sys · malfunctionedUNSAT AUTOLAND. AIRCRAFT LANDED 20 FEET TO THE RIGHT OF RUNWAY CENTER LINE 16R. FFR SHOWS NO PROBLEMS LAST LEG. ACCOMPLISHED DFCS LAND VERIFY AND HGS SYSTEM TEST REF MM 34 36 00. OPS NORMAL.SDR ASAA11510587Solenoid Valve · failedAPU HAS REPORT OF START EGT OF 1000 DEGREES AND FAULT LIGHT ILLUMINATING WITH FAULT MESSAGE 49-41010 LOGGED ON CDU. ACFT GROUNDED. PERFORMED FIM TASKS NO PROBLEMS NOTED. REPLACED T2 AND P2 SENSORS (AMM REFERENCE 49-61-31 AND 49-52-31). REPLACED THE FFD SOLENOSDR ASAA11510580Regulator · failedINITIAL CLIMBOUT RIGHT DUCT PRESSURE 44 LEFT DUCT PRESSURE 22 STAYED LIKE THAT UNTIL FL 300 RIGHT 40 LEFT 25. LEVEL FL 360 V 380 DUCT PRESSURE VARIED FROM 7-20 PSI DIFFERENCE. RIGHT HIGH. PERFORMED BLEED AIR HEALTH CHECK ON NR 1 ENG. REF AMM 36-11-00-700-8SDR ASAA11510568Unknown · malfunctionedON GROUND STARTED APU & EGT CLIMBED TO 1000 & THE FAULT LIGHT CAME ON. ACCOMPLISHED FIM TASK 49 40 00 810 801 PG 2 &3 STEP 26 A D LOGGED FAULT 49 41010 FROM ORIGINAL DEFECT. ACCOMPLISHED 4 APU STARTS A/C AND D/C NO FAULTS LAGGED. A/C CLEARED FOR SERVICE.SDR ASAA11510547Fuel Control · faultyAPU HAS HISTORY OF FAULT MESSAGE 49 31016 BEING LOGGED IN CDU APU FAULT HISTORY. COMPLETED FIM TASK 49 30 TASK 803 PARA F STEPS 1 THRU 4 NO FAULTS FOUND. PER STEP 4 REPLACED APU FUEL CONTROL REF M/M 49 31 11 OPS AND LEAK CHECKS GOOD.SDR ASAA11510450Regulator · malfunctionedON CLIMBOUT RIGHT BLEED TRIP LIGHT ILLUMINATED AT APPROX 6000FT. QRH FOLOWED. BLEED TRIP WOULD NOT RESET. DIVERSION TIME: 18 MINUTES. FOUND 5TH STAGE BLEED AIR DUCT UNCOUPLED FROM ENGINE CASE. REPLACED BLEED AIR REG. REF MM 36 11 03 000 801. REPLACED HIGSDR ASAA11510406Unknown · malfunctionedAPU IN FLIGHT START ATTEMPT. FIRST ATTEMPT AT FL380 UNSUCCESSFUL FAULT LIGHT. SECOND ATTEMPT UNSUCCESSFUL W/ HIGH EGT FAULT FL380. NO FURTHER ATTEMPTS MADE. BITE CHECK SHOW MAINT MESSAGE 49 31016. REF FIM TASK 49 30 00 810 803. STEP E (1) SUSPECT AN INTERMSDR ASAA11510373Eec · malfunctionedON TAXI IN ENGINES AT IDLE RIGHT OIL FILTER BYPASS LIGHT ILLUMINATED. REPLACED SCAVENGE OIL FILTER. NO DEFECTS NOTED. PERFORMED CDU CHECK INPUT MONITORING FILTER SCREEN FILTER BYPASS STATUS INDICATES A CONDITION OTHER THAN CLOGGED. ON EEC BITE TEST FOUND FSDR ASAA11510292Unknown · malfunctionedFMC DISAGREE LIGHT ON GROUND. PERFORMED QRH PROCEDURE. RESET LIGHT.SDR ASAA11510226Actuator · corrodedRIGHT AIR CONDITIONING COMPARTMENT RAM AIR DOOR ACTUATOR ROD END BEARING RUSTY. REPLACED RT RAM AIR DOOR ACTUATOR RIG AND OPS CHECK GOOD REF B737 NG MM 21 51 22 AND 21 51 21.SDR ASAA11510240Trans Panel · corrodedAFT CARGO COMPARTMENT LT SIDEWALL TRANSITIONAL PANEL STA. 727+4 TO STA 792 STR 25 HAS CORROSION AROUND SEVERAL FASTENER HOLES BS 712 BS 792 LBL 25 STR 25L. REMOVED CORROSION FROM BS 727B +10 BS 757 ORIG .040 MAT LOSS .010 REMAINING .030 FOUND TO BE OUT OF LIMSDR ASAA11510234Support Angle · corrodedFWD CARGO COMPARTMENT AFT BULKHEAD LEFT THRESHOLD SUPPORT ANGLE IS CORRODED AT LOWER END. REMOVED CORROSION IAW B737 800 SRM 53 00 07 ALLOW DAMAGE 1. ORIG MAT 071 REMAINING MAT 061 EXCEEDS ALLOWABLE LIMITS. REPLACED SUPPORT ANGLE P/N 143A9485 23 PO 719724.1SDR ASAA11510223Floor Support · corrodedFORWARD CARGO COMPARTMENT AFT BULKHEAD CENTER THRESHOLD FLOOR SUPPORT ANGLE HAS AREAS OF CORROSION. REPLACED CORRODED PART.SDR ASAA11510172Idg · failedGEN 2 "SOURCE OFF" LIGHT ILLUMINATED 15 MINUTES AFTER TAKEOFF. QRH PROCEDURE ACCOMPLISHED. NR 2 DRIVE LIGHT ILLUMINATED 2 MINUTES AFTER "SOURCE OFF" LIGHT. NR 2 DRIVE DISCONNECTED PER QRH PROCEDURE. DIVERSION TIME 31 MINUTES. PERFORMED TASK 24 11 11 090 8SDR ASAA11510152Actuator · faultyRIGHT SPAR VALVE CLOSED LIGHT ILLUMINATED DIM ENGINE INDICATIONS ALL NORMAL. CHECKED NR 2 ENG SPAR VALVE CB NORMAL PERFORMED ENG NR 2 SPAR VALVE FAULT ISOLATION REF 28 22 00 GROUND VERIFICATION NORMAL. FOLLOWUP TSR ISSUED. REPLACED NR 2 ENG SPAR VLV ACTUATOSDR ASAA1159886Control Unit · malfunctionedOVERHEAT LIGHT ON RIGHT FWD WINDSHIELD IS ILLUMINATED. ACCOMPLISHED FIM TASK 30 40 00 WINDOW HEAT CONTROL UNIT OPS CHECK NORMAL. GND VERIFY SUCCESSFUL.
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