N563AS
Service difficulty reports · 561
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 = 'N563AS' 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 = 'N563AS' 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 ASAA2019100733941Exciter · intermittentAPU "FAULT" LIGHT WHEN ATTEMPTED TO START APU AFTER LANDING. GROUNDED - YES. FOUND "NO FLAME SHUTDOWN" FAULT. ACCOMPLISHED B737-800 FIM 49-40 TASK 802. ACCOMPLISHED 2 SUCCESSFUL STARTS, NO FAULTS FOUND. REMOVED AND REPLACED APU EXCITER ASSY AND IGNITER PLUG, PSDR ASAA2019091130698Overheat Sensor · defectiveAPU DET INOP ILLUMINATED AT CRUISE, APU WAS NOT RUNNING. GROUNDED - YES. FIRE DETECTION MODULE SHOWS APU-TAILPIPE. ACCOMPLISHED FIM 26-10 TASK 808. TAIL PIPE DETECTOR READS 25K OHMS. PER FIM 26-10 TASK 802 REMOVED AND REPLACED APU TAILPIPE OVERHEAT DETECTOR ELSDR ASAA2019083130583Card · not seatedSAT LOG MODEM STATUS PAGE IN ACARS DISPLAYS LBT-2 AS NOT READY AND SIGNAL STRENGTH 0. GROUNDED - YES. ON SAT CONFIG PAGE. LBT-2 SIM NUMBER WAS BLANK. RESEATED IRIDIUM CONFIG ID MODULE SIM CARDS PER AMM 23-15-00-400-802. ONE MIG-51A INSTALLED/ REMOVED. LBT-2 SISDR ASAA2019072030108Control Panel · inoperativeF/O SIDE COURSE KNOB INOP. GROUNDED - YES. CYCLED POWER-NO HELP. FO COURSE SELECTOR INOP. REMOVED & REPLACED MCP. OP CK NORMAL. REF AMM 22-11-34-000-801 & 22-11-34-400-801, BITE GROUP 32 & 49.SDR ASAA2019071430052Turbine · dented#1 ENGINE REAR TURBINE FLANGE DENTED @ 3&9 OCLOCK POSITION. GROUNDED - YES. REMOVED AND REPLACED #1 ENG REAR TURBINE FLANGE REF. AMM 72-56-00-000-802-F00 STEPS (E) AND (F) 1, 2 AND 4 AND AMM 72-56-00-400-801-F00 F(2), (3) AND G(1) AND (2).SDR ASAA2019061089641Pump · inoperativeMAIN TANK #1 FORWARD FUEL PUMP INOP. GROUNDED - YES. REF B737-800 AMM 28-22-41-000-801/-400-801 REMOVED AND REPLACED #1 TANK FWD BOOST PUMP IMPELLER, #1 BOOST PUMP OPS AND LEAK CHECK GOOD.SDR ASAA2019040848893Indicator · inaccurate#1 FUEL QUANTITY INDICATOR SHOWS IMBALANCE. GROUNDED - YES. CYCLED A/C POWER #1 FUEL IMBALANCE AMBER LIGHT EXTINGUISHED PERFORMED B737-800 FIM TASK 28-41-00-810-801 NO FAULTS FOUND.SDR ASAA2019032228743Pump · failedTHE AFT FUEL PUMP ON THE LEFT MAIN TANK FAILED DURING CRUISE. GROUNDED - YES. REMOVED AND REPLACED LEFT AFT TANK FUEL BOOST PUMP PER AMM 28-22-41. CLEARED MEL 28-1C.SDR ASAA2019032228742Circuit Breaker · trippedLEFT AFT MAIN TANK FUEL PUMP SWITCH ILLUMINATED. GROUNDED - YES. FOUND TANK 1 AFT FUEL BOOST CB OPEN ON P92 PANEL NO DEBRIS FOUND. INSPECTION OF P92 PANEL GOOD. RESECURED P92 PANEL RESET BOOST PUMP CB. OPERATED BOOST PUMP FOR 10 MINS, TURNED OFF AND OPERATED FSDR ASAA2019030928551Warning System · false activationHF RADIO NR 1 FAIL. GROUNDED - YES. PERFORMED BITE PROCEDURE ON NR 1 HF TRANSCEIVER PER FIM TASK 23-11-00-810-801, OPS CHECK GOOD, FAIL LIGHT EXTINGUISHED.SDR ASAA2019030528476Unknown · malfunctionedCON CAB & FWD CAB ZONE TEMP CONTROLLERS INOP. GROUNDED - YES. RAN PACK/ZONE TEMP CONT TEST PER AMM 21-61-00 SYSTEM OP CHECKS GOOD NO DEFECTS NOTED. CABIN AND FLIGHT DECK SENSOR FILTERS REPLACED FOR THE "A" CHECK THIS CLEARS MEL 21-19G AND 21-21G.SDR ASAA2019030328503Indicator · inoperativeNR 2 TANK FUELING PANEL GAUGE INOP. GROUNDED - YES. REMOVED AND REPLACED NR 2 TANK FUELING PANEL GAUGE REF AMM 28-41-61. OPERATIONAL CHECK IS NORMAL CLEARS MEL 28-12B.SDR ASAA2019022828440Start Valve · inoperativeENG NR 2 AFTER START SWITCH TO GROUND START VALVE OPEN BUT NO N2 ROTATION. GROUNDED - YES. REMOVED & REPLACED N2 ENG START VALVE IN REF TO AMM 80-11-03 PERFORMED PNU LEAK CHECK AMM TASK 71-00-00-700-809-F00 OPS NORMAL AC IS GOOD FOR SERVICE.SDR ASAA2019022518275Warning Light · false activationAFTER ENGINE START CONT CAB ZONE TEMP LITE ILLUMINATED WILL NOT EXTINGUISH AFTER FOLLOWING QRH. GROUNDED - YES. REF B737-800 FIM 21-61 TASK 801, #1 PZTC BITE TEST PASSED NO FAULT NOTED, #2 PZTC BITE TEST FAULTED FLT DECK TRIM VALVE, NO ACTIVE FAULT SHOWS AFTERSDR ASAA2019012427936Smoke Detector · failedAFT LOWER CARGO FIRE SWITCH LOOP A TEST INOP. GROUNDED - YES. REPLACED (3) SMOKE DETECTORS IN AFT CARGO PIT A SYS M2242, M2243, M2244 PER AMM 26-16-01-400-801. OPS CK PER AMM 26-16-00-730-801.SDR ASAA2019012427914Seal · missingREF T/C 78472010 NR 2 ENGINE FAN BLADE LUBRICATION. FOUND PLATFORMS MISSING RUBBER SEALS BEYOND LIMITS. P/N: 340-001-816-0. 24 EACH. GROUNDED - YES. REPLACED ALL PLATFORMS ON NR 2 ENGINE FAN PER T/C 78472010.SDR ASAA2019012427913Blade · crackedWHILE ACCOMP T/C SBCFM56-7B-72-1033-1, FAN BLADE ROOT ULTRASONIC INSPECTION FOUND BLADE NR 3 S/N DD453914-J 32% INDICATION 5.25" FROM LE CONVEX SIDE. BLADE NR 11 S/N DD454177-5 31% INDICATION 1.25" FROM LE CONVEX SIDE. ALL BEYOND 30% REJECT, ENGINE NR 2 S/N 89SDR ASAA2019012427912Shim · wornDURING FAN LUBE ALL NR 2 ENGINE FAN BLADE SHIMS HAVE WEAR. GROUNDED - YES. REPLACED ALL NR 2 ENGINE SHIMS PER T/C 78472010.SDR ASAA2019011627814Electronic Unit · failedCARGO SMOKE/FIRE DETECTION AFT LOOP "A" WILL NOT TEST. GROUNDED - YES. DUE TO HISTORY, REMOVED AND REPLACED AFT CARGO CEU. OPS TEST GOOD. REF AMM 26-16-02. AFT CARGO DETECTOR SWITCH TO NORMAL POSITION.SDR ASAA2019010927727Unknown · malfunctionedAFT CARGO DETECTOR LOOP A WON'T TEST. GROUNDED - YES. PERFORMED AMM TASK 26-16-00-710-801. CHECKED GOOD. NO HISTORY IN 30 DAYS. OPS NORMAL.SDR ASAA2019010327681Unknown · malfunctionedWHILE IN THE CLIMB, VTK APPREARED ON FO'S ND. FMA WENT FROM LNAV TO CWS AND SCRATCHPAD MESSAGE SINGLE FMC OPERATION WAS DISPLAYED. CONSULTED QRH 11.3 AND BEFORE WE COMPLETED THE CHECKLIST THE RIGHT FMC WAS RESTORED AND WORKING AGAIN. ENTERED PER FLIGHT HANDBOOSDR ASAA2018123027629Compensator · failedIN FLIGHT MAIN TANK NR 1 WAS 600 LBS LOW WHILE USING CENTER TANK FUEL. ON LANDING MAIN TANK NR 1 300 LBS LOW. GROUNDED - YES. ON DEFERRAL. PERFORMED A TANK AND COMP UNITS TEST ON THE NR 1 TANK PER AMM 28-41-21-710-801. FOUND PROBES F15, F4, F5, F6, F7, AND F9 SDR ASAA2018123027630Unknown · malfunctionedSHORTLY AFTER LEVEL AT CRUISE SAW LEFT MAIN FUEL QUANTITY DECREASING WITH ALL 6 FUEL PUMPS ON WITH CENTER TANK FUEL, LEFT TANK SHOWED A 500 LBS DIFFERENCE FROM RIGHT MAIN TANK. RAN QRH FUEL LEAK CHECK LIST. DETERMINED NO LEAK WAS PRESENT. QUANTITY STOPPED DECRSDR ASAA2018122417518Idg · inoperativeDRIVE LIGHT ILLUMINATED. DISCONNECTED DRIVE. GROUNDED - YES. REMOVED/REPLACED/TESTED #1 ENGINE IDG PER B737-800 AMM 24-11-11-000/400-801, 71-00-00-800-811-F00. GROUND VERIFICATION REPAIR CONFIRMATION SUCCESSFUL PER FIM 24-11-801. LIBERATION OF VALVE CAP LIKELYSDR ASAA20181227579Fitting · separatedFOUND TEST PIN FITTING TO HAVE SEPARATED FROM BOSS # 2 ENGINE 1 O'CLOCK POSITION LOOKING FWD. GROUNDED - YES. ON DEFERRALSDR ASAA2018121227383Valve · intermittent#2 ENGINE ANTI-ICE BLUE (COWL VALVE OPEN) LIGHT DOES NOT STAY DIM WHEN ENGINE ANTI ICE SELECTED ON (LT INTERMITTENTLY SWITCHES BACK AND FORTH) (DIM TO BRIGHT). GROUNDED - YES. REF B737-800 WDM'S 30-21-11/30-21-21 PG1, W/DP1303 OFF VALVE, SW ON, AND SHOWS BRIGHSDR ASAA2018113027180Oven · odorAIRCRAFT RIGHT AFT RIGHT HAND OVEN BEGAN TO HEAT UP AND EMIT A HOT ELECTRICAL SMELL AFTER HAVING BEEN TURNED OFF FOR 45 MINUTES HOT ELECTRICAL SMELL STOPPED AFTER PULLING OVEN CIRCUIT BREAKERS. GROUNDED - YES. RESET C/B'S FOR AFT GALLEY OVENS. TURNED ON OVEN ASDR ASAA2018112927153Smoke Detector · intermittentCARGO FIRE TEST AFT FAIL. GROUNDED - YES. UNABLE TO DUPLICATE DEFECT, DUE TO HISTORY REMOVED AND REPLACED AFT CARGO A3 LOOP DETECTOR REF AMM 26-16-01, OPS CHECK NORMAL.SDR ASAA2018120397186Eec · inoperativeENGINE CONTROL LIGHT ILLUMINATED AFTER LANDING. GROUNDED - YES. FOUND FAULTS CODE 73-20131 & 73-21281. FURTHER INSPECTION REVEALED ENG #1 ALTN PWR CHANNEL "A" C/B OPENED. INSPECTED C/B PER B737-800 AMM 20-60-01 NO DEFECTS NOTED. C/B WOULD NOT RESET. DISCONNECTSDR ASAA2018112127061Warning System · false activationFLT CREW REPORTS FAULT LIGHT ILLUMINATED ON AFT CARGO FIRE DETECTION TEST. GROUNDED - YES. PERFORMED FIRE AND OVERHEAT DETECTION CHECK REF AMM 26-10-00-710-801, NO FAULTS FOUND. PERFORMED CARGO FIRE CONTROL PANEL BITE CHECK, NO FAULTS FOUND REF FIM 26-23 TASK SDR ASAA2018111126808Transceiver · failedNR 2 HF DID NOT TEST. GROUNDED - YES. ACCOMPLISHED FIM 23-11 TASK 801. FOUND NUMBER 2 HF TRANSCEIVER WOULD NOT POWER UP FOR BITE TEST. CYCLED A/C POWER OPS AND BITE CHECK GOOD. REMOVED AND REPLACED NR 2 HF TRANSCEIVER PER AMM 23-11-21. OPS AND BITE CK GOOD. OKSDR ASAA2018103126678Modulating Valve · failedCONT CABIN ZONE TEMP ILLUMINATED AFTER ENG START. RAN QRH AND COMPLIED WITH INSTRUCTIONS ZONE LIGHT EXTINGUISHED AFTER MASTER CAUTION WAS RESET. TALKED TO MAINT, AND SAID GOOD TO PROCEED. GROUNDED - YES. BITE CHK NR 2 TEMP CONTROLLER, SHOWED FLT DECK TRIM VALVSDR ASAA2018102626586Transceiver · inoperativeHF RADIO NR 1 INOPERATIVE, RADIO DOES NOT TRANSMIT OR RECEIVE. ANTENNA DOES NOT INDICATE TUNING WHEN MICROPHONE IS KEYED. NO SIDETONE IS HEARD WHEN ATTEMPTING TO TRANSMIT. TWO BEEPS ARE HEARD EVER 12 SECONDS WHEN MONITORING RADIO. USE OF DIFFERENT TUNING HAD, SDR ASAA2018091526248Intercostal · crackedINTERCOSTAL BETWEEN STA. 312 AND 328 LBL 45 CRACKED AT FASTENER HOLE. GROUNDED - YES. REMOVED AND REPLACED CRACKED INTERCOSTAL IAW B737-800 SRM 51-40-02-06-0.SDR ASAA2018091326362Gusset · corrodedUPON REMOVAL OF GEL TAPE AT STA 767 ABOVE STR 25R GUSSET IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED RT STR 25 GUSSET AT BS 767 IAW SRM 51 40 02 0G 0. GUSSET FOUND TO BE OUT OF LIMITS IAW SRM 53 00 53 1A 2 W 1 1/4 O .063 R .051 L 1 1/2 D .012.SDR ASAA2018091326306Transition Panel · corrodedUPON REMOVAL OF GEL TAPE FOUND CORR ON TRANSITIONAL PANEL FROM LT STA 727D+10 TO 727I+10 IN AFT PIT. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53 00 53 1A 2. FABRICATED NEW TRANSITION PNL IAW SRM 53 00 53 2R 5 STEPS 4D AND INSTALLED IAW SDR ASAA2018091326304Transition Panel · corrodedUPON REMOVAL OF GEL TAPE FOUND CORR ON RT TRANSITION PANEL AFT PIT FROM STA 727E TO STA 767. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53 00 53 1A 2 FIG 103 DETAIL D. FABRICATED NEW TRANSITION PNL IAW SRM 53 00 53 2R 5 AND INSTALLED IAW SDR ASAA2018092613253Angle · corrodedUPON REMOVAL OF ANGLE AT STA. 986 LBL45, CORROSION ON LOWER SURFACE (PR). GROUNDED - YES. REMOVED CORROSION ON ANGLE AT STA 986 LBL 45, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1 FIG 104 DETAIL F, LOCATED + DRILLED NEW ANGLE IAW B737-800 SRM 51-4SDR ASAA2018091126335Cargo Track · wornAFT PIT CARGO NET TIE DOWN AT STA 787 LT LUGS ARE WORN. GROUNDED - YES. AFT PIT CARGO TRACK AND LUG WERE REPAIRED AND REFINISHED IAW EA 800 53EA 20761 AND SRM 53 00 53 2R 3.SDR ASAA2018091126305Door Sill · corrodedAFT PIT CARGO THRESHOLD SILL HAS CORR. GROUNDED - YES. REMOVED CORR REMAINING MATL FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED THRESHOLD SILL IAW SRM 51 40 02 0G 0 W 1 O .05 R .043 L 24 D .007.SDR ASAA2018091126303Angle · crackedDRY AREA FLOOR STRUCTURE ANGLE CRACKED FWD SIDE OF STA 520 FLOORBEAM BL0. GROUNDED - YES. REMOVED AND REPLACED WITH NEW ANGLE AT DRY AREA FLOOR STRUCTURES AT STA 520 BL0 IAW SRM 51 40 02 0G 0.SDR ASAA2018091126302Angle · crackedDRY AREA FLOOR STRUCTURE ANGLE CRACKED IN RADIUS AT STA 540 RBL 2. GROUNDED - YES. REMOVED AND REPLACED DRY AREA FLOOR STRUCTURE ANGLE AT STA 540 RBL2 IAW B737 800 SRM 51 40 02 0G 0.SDR ASAA2018091126301Angle · crackedDRY AREA FLOOR STRUCTURE ANGLE CRACKED IN RADIUS AT STA 54O LBL 2. GROUNDED - YES. REMOVED AND REPLACED DRY AREA FLOOR STRUCTURE ANGLE AT STA 540 LBL 2 IAW SRM 51-40-02-00-0.SDR ASAA2018100826378Floorbeam · corrodedAFT WET AREA FLOORBEAM STA. 986 HAS CORROSION ALONG TOP CAP. GROUNDED - YES. REPAIRED 986 FLOORBEAM UPPER HORZ. FLANGE IAW SRM 53-70-51-2R-4.SDR ASAA2018100526363Intercostal · crackedFWD WET AREA INTERCOSTAL BETWEEN STA 277 AND 294 BL0 IS CRACKED AT FASTENER HOLE. GROUNDED - YES. REMOVED CRACKED INTERCOSTAL BETWEEN STA 277 AND 294 BL0 AND INSTALLED NEW INTERCOSTAL IAW SRM 51 40 05 0G 0 AND 51 40 02 0G 07.SDR ASAA2018092106257Floorbeam · corrodedAFT WET AREA FLOOR BEAM STA. 947 HAS A CORROSION PIT O/B OF RH LAV. MOUNT. GROUNDED - YES. REPAIRED FLOOR BEAM HORIZONTAL FLANGE IAW 737-800 SRM 53-70-51-2R-5.SDR ASAA2018092526249Intercostal · crackedFWD WET AREA INTERCOSTAL BETWEEN STA 312 AND 328 RBL 30 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED CRACKED INTERCOSTAL IAW B737-800 SRM 51-40-02-06-0.SDR ASAA2018082975931Feeder Cable · not reportedL2 WINDOW OVERHEAT LIGHT ILLUMINATED DURING CLIMB. REMAINED OUT AFTER QRH. ACFT GROUNDED. REMOVED AND REPLACED THE COIL CORD AT THE L2 WINDOW IAW AMM 30-41-00. OPS TESTED GOOD.SDR ASAA2018082755917Warning Light · false activationLEFT SIDE WINDOW OVERHEAT ILLUMINATED IN FLIGHT. ACFT GROUNDED. COMPLETED QRH OPS NORMAL.SDR ASAA2018082725909Controller · failedPRESSURIZATION SELECTOR SWITCH WAS IN AUTO POSITION & GREEN ALTERNATE LIGHT ON. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 CABIN PRESSURE CONTROLLER, OPS NORMAL IAW AMM 21-31-01.
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