N565AS
Service difficulty reports · 509
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 = 'N565AS' 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 = 'N565AS' 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 ASAA2018081525770Transition Panel · corrodedAFT CARGO BAY, LBL 25 TRANSITION PANEL, BETWEEN BS 727 AND 807, HAD AREAS OF CORROSION. ACFT GROUNDED. REMOVED THE CORROSION, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED THE TRANSITION PANEL IAW SRM 51-40-02-0G-0.SDR ASAA2018070825324Motor · faultyFUEL MAIN TANK NR 1 FWD PUMP LOW PRESSURE LIGHT ILLUMINATED FOLLOWED QRH, CALLED MX CONTROL /DISPATCH. GROUNDED - YES. FOUND NR 1 TANK FWD BOOST PUMP C/B OPEN. ACCOMPLISHED FIM 28-22 TASK 813 FOUND FAULTS BOOST PUMP. REMOVED AND REPLACED NR 1 FWD BOOST PUMP MOSDR ASAA2018062525190Position Switch · faultyLT RAM DOOR FULL OPEN LT CAME ON AT LEVEL OFF (CRUISE FLT). GROUNDED - YES. REMOVED AND REPLACED FLAP SWITCH S1051 REF AMM 27-51-63. OPERATIONAL CHECKS OF LT RAM AIR ACTUATOR AND FLAP SWITCH GOOD.SDR ASAA2018062225178Display · malfunctionedNR 2 FMC CDU BLANKED AND REINITIALIZED A MOMENT LATER ENROUTE. GROUNDED - YES. PERFORMED FMC BITE ON NR 2. FOUND ARINC RATE; NO HARDWARE FAULTS. SENSOR DATA GOOD. REF FIM 34-61 TASK 837. PERFORMED 4 C/B RESET, BOTH FMCS POWERED UP. OPS CHECK GOOD. REF FIM 34-6SDR ASAA2018062505162A/C Pack · malfunctionedAT FL 370 DURING CRUISE, THE LT PACK LIGHT ILLUMINATED. OBSERVED A DROP IN LEFT DUCT PRESSURE AND A NOISE REDUCTION. LT PACK TEMP INCREASED FROM APPROXIMATELY 20 DEGREES C TO 40 DEGREES C. ACCOMPLISHED QRH AND PACK CAME BACK ON, LIGHT RESET. PACK TEMP DROPSDR ASAA2018061825121Actuator · malfunctionedLEFT RAM DOOR FULL OPEN LIGHT STAYED ILLUMINATED AT CRUISE ALTITUDE FOR THE FLIGHT. ACFT GROUNDED. REMOVED AND REPLACED THE LEFT RAM AIR INLET ACTUATOR IAW AMM 21-51-21. PERFORMED A PACK ZONE TEMP CONTROLLER BITE TEST IAW AMM 21-61-00. ON VERIFY, GO LIGHT ISDR ASAA2018061855093Blade · damagedWHIILE ACCOMPLISHING T/C 78472002, FOUND THE CU-NI-IN COATING CHIPPED & MISSING ON BLADES 1, 11, 13, 21, & 23. ACFT GROUNDED. REMOVED AND REPLACED THE BLADES IAW T/C 78472002.SDR ASAA2018061325061Fmc · malfunctionedRIGHT FMC FAILED WITH VTK BOTH MAPS FOR APPROX 3 MIN IN CRUISE DID RESTORE AUTOMATICALLY. GROUNDED - YES. FFR ALT FMC FAULTED PRES POS LATE RATE. COMPLETED FIM TASK 34-61 TASK 824. NO ACTIVE FAULTS. RT FMC OPS NORMAL.SDR ASAA2018061325050Display · malfunctionedON POWER UP LEFT FMC FAIL LIGHT. GROUNDED - YES. FOUND LEFT MCDU SCREEN BLANK ALONG WITH FAIL LIGHT. PERFORMED FIM 34-61 TASK 804 (CYCLED BOTH MCDU CB'S) AND NORMAL CDU PROMPTS DISPLAY, FAULT LIGHT EXTINGUISHED. REPAIR CONFIRMATION PASS. FMC'S CDU INSTALLATIONSDR ASAA2018040924182Warning System · false indicationELEC ILLUMINATED ON OVERHEAD PANEL. GROUNDED - YES. ACCOMPLISHED ELEC LIGHT BITE MESSAGE IN REF FIM 24-31 TASK 801. OP'S CHECK GOOD. MESSAGE CLEARED.SDR ASAA2018032624040Actuator · failedLEFT PACK LIGHT ILLUMINATED DURING MASTER CAUTION CHECK. LIGHT EXTINGUISHED WHEN MASTER CAUTION IS RESET. MASTER CAUTION AND AIR COND ALSO EXTINGUISH WHEN MASTER CAUTION IS RESET. ACFT GROUNDED. PERFORMED A PACK/ZONE TEMP CONTROLLER BITE TEST IAW AMM 21-6SDR ASAA2018031823928Warning Light · false activationLEFT PACK LIGHT ILLUMINATED ON RECALL DURING DESCENT, LIGHT EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. TROUBLESHOT IAW FIM 21-62 / 801 & 802. APPEARS TO HAVE BEEN AN INTERMITTENT FAULT. BITE VERIFICATION TESTED NORMAL. NO OTHER RECENT HISTORY.SDR ASAA2018020823462Flange · crackedWHILE ACCOMPLISHING A NR 1 ENGINE INLET INSPECTION IAW T/C 78472000, FOUND THE ENGINE FLANGE CRACKED AT FWD FIRE DETECTOR TRANSPONDER, OTBD HOLE. CONFIRMED WITH HFEC. ACFT GROUNDED. ACCOMPLISHED A REPAIR IAW TASK CARD SBCFM56-7B-72-05801-1. REVERSED ALT DSDR ASAA2017111422580Knob · brokenBANK CONTROL KNOB BROKEN. ACFT GROUNDED. REMOVED & REPLACED DFCS MCP IAW AMM 22-11-34. OPS NORMAL. ALL MAINTENANCE TESTS ACCOMPLISHED.SDR ASAA2017101722226Controller · malfunctionedAMBER AUTO FAIL & GREEN ALTN LIGHTS ILLUMINATED. ACFT GROUNDED. IAW FIM 21-31, TASK 827, RESET CONTROLLER ON AUTO PRESSURE PANEL, LIGHTS CLEARED. INTERROGATED THE NR 1 PRESSURE CONTROLLER, NO FAULTS, IAW FIM 21-31, TASK 801. INTERROGATED THE NR 2 PRESSURE COSDR ASAA2017100122089Fmc · malfunctionedFIRST OFFICER'S FMC VTK & ASSOCIATED FMC LIGHT CYCLES ON & OFF AT INTERVALS OF ABOUT 10 SECONDS. STARTED AFTER LANDING. ACFT GROUNDED. CONFIRMED. NO HISTORY FOR 60 DAYS. PULLED & RESET THE NR 1 & 2 FMCS COMPUTERS AND MCDU CIRCUIT BREAKERS. OPS CHECKED BOTHSDR ASAA2017093022106Sensor · failedTHE NR 1 ENGINE HAS A SHORT TIME FAULT MESSAGE 73-30901 - T12, SIGNALS DISAGREE. ACFT GROUNDED. REMOVED AND REPLACED T12 SENSOR. OPS TEST GOOD IAW AMM 73-21-05.SDR ASAA2017092522047Housing · damagedMID-CABIN EXIT ROW SIGN LENS DETACHED. ACFT GROUNDED. REPLACED THE MID-CABIN, OVERHEAD AISLE EMERGENCY EXIT SIGN HOUSING. OPS CHECKED OK IAW AMM 33-51-01.SDR ASAA2017082621718Control Panel · failedAUTOTHROTTLE ARM LIGHT DOES NOT ILLUMINATE. ACFT GROUNDED. REMOVED & REPLACED DFGC MODE CONTROL PANEL. OPS CHECKED GOOD IAW AMM 22-11-34.SDR ASAA2017082321701Warning Light · false activationELEC LIGHT ILLUMINATED DURING POWER TRANSFER ON GROUND. ACFT GROUNDED. PERFORMED FIM 24-31-801. SPCU 1 INOPERATIVE FAULT APPEARED AND CLEARED DURING BITE TEST. INTERMITTENT FAULT.SDR ASAA2017081121610Lens · detachedR1 DOOR EXIT LIGHT COVER FELL OFF GROUNDED - YES. SECURED R1 DOOR EXIT LIGHT LENS COVER.SDR ASAA2017080321524Smoke Detector · false indicationCREW REPORTED FWD CARGO FIRE DETECTION FAULT. ACFT GROUNDED. PERFORMED FIM 26-16, TASK 805. FOUND FWD CARGO B1 SMOKE DETECTOR FAULTING. REMOVED AND REPLACED THE FWD CARGO SMOKE DETECTOR B1 IAW AMM 26-16-01, OPS CHECKED GOOD.SDR ASAA2017072821493Regulator · failedRIGHT BLEED VALVE APPEARS TO BE CLOSED. ACFT GROUNDED. REPLACED THE NR 2 ENGINE BLEED AIR REGULATOR IAW AMM 36-11-03. LEAK CHECKED GOOD, RAN THE NR 2 ENGINE BLEED AIR WORKS NORMAL.SDR ASAA2017062821350Idg · unknownFOLLOW-UP TO #1 IDG CONTINUED FREQUENT SERVICING. REPLACE IDG. GROUNDED - YES. INSPECTED IDG OIL FILTERS BEFORE REMOVAL. NO DEFECTS NOTED, REF B737-800 AMM 24-11-11-080-801. REMOVED AND REPLACED NR 1 IDG IAW AMM 24-11-11. LEAK AND OPS CHECKED GOOD.SDR ASAA2017061621105Coffeemaker · odorFAS REPORT ELECTRICAL ODOR COMING FROM AFT GALLEY COFFEEMAKERS. CIRCUIT BREAKERS PULLED, ODOR DISAPPEARED. ACFT GROUNDED. REMOVED AND REPLACED THE AFT GALLEY COFFEEMAKER. REVERSED SPECIAL PROCEDURE. OPS CHECKED GOOD.SDR ASAA2017051720816O-Ring · damagedNR 1 ENGINE OIL CAP O-RING HAS EXTRUDED. ACFT GROUNDED. REPLACED THE OIL CAP O-RING IAW AMM 79-11-01.SDR ASAA2017042120497Unknown · malfunctionedVERTICAL SPEED LED PANEL INOP MCP MODE CONTROL PANEL. GROUNDED - YES. POWERED DOWN AIRCRAFT, REPOWERED AIRCRAFT, RAN DFGS TEST PER AMM 22-00-01 SYSTEM OP CHECKS GOOD NO HISTORY LAST 60 DAYS NO DEFECTS NOTED AT THIS TIME AIRCRAFT REMAINS HGS/AUTOLAND QUALIFIED SDR ASAA2017040620392Oil Cooler · leakingNR 1 ENGINE IDG AIR/OIL COOLER LEAKING. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 IDG AIR/OIL COOLER IAW AMM 24-11-21-000-801, AND 24-11-21-400-801. NR 1 ENG IDG OIL COOLER LEAK CHECK GOOD IAW AMM 71-00-00-700-801-F00. ETOPS GROUND VERIFICATION SUCCESSFULSDR ASAA2017040420364Warning Light · false activationAFTER BOTH ENGINES STARTED, ELEC LIGHT ON RECALL. ACFT GROUNDED. ACCOMPLISHED FIM 24-31, TASK 801. SPCU FAULT STORED. ACCOMPLISHED FIM 34-34, TASK 802. FAULT CLEARED & OPS NORMAL. GROUND VERIFICATION TEST GOOD.SDR ASAA2017040220336Combust Chamber · crackedNR 1 ENGINE BORESCOPE INSPECTION OF THE COMBUSTION CHAMBER. FOUND FIVE OUTER LINER PANELS THAT HAD ONE CONTINUOUS AXIAL CRACK WITH COOLING RIB 5 CRACKED THROUGH TO COLD SIDE JUST BELOW RT MAIN IGNITER. FOUND BURNED THROUGH AREA IN OUTER LINERS NR 4 & 5 PANELSSDR ASAA2017031220143Transceiver · failedNR 1 HF RADIO FAILED. ACFT GROUNDED. REMOVED & REPLACED THE NR 1 HF TRANSCEIVER. OPS CHECKED NORMAL IAW AMM 23-11-21-000-801, & 23-11-21-400-801.SDR ASAA2017021519835Regulator · faultedLEFT DUCT PRESSURE IS 10 PSI AT IDLE TRUST ON THE GROUND. ACFT GROUNDED. ACCOMPLISHED THE PNEUMATIC SYSTEM TROUBLESHOOTING IAW AMM 36-11-00-700-804 - NO DEFECTS WERE NOTED. REMOVED AND REPLACED THE NR 1 ENG HIGH STAGE VALVE IAW AMM 36-11-06-00-000-801 ANDSDR ASAA2017021219788Indicator · inaccurateCENTER TANK GUAGE IN FUELING PANEL INACCURATE. ACFT GROUNDED. REMOVED AND REPLACED THE CENTER REFUEL QTY INDICATOR IAW AMM 28-41-61, OPS NORMAL.SDR ASAA2017012419538Idg · failedNR 2 GENERATOR WILL NOT CONNECT. 0 VOLTS, 0 FREQS. ACFT GROUNDED. REPLACED THE NR 2 ENGINE IDG. OPS CHECKED GOOD. NO LEAKS FOUND IAW AMM 24-11-11.SDR ASAA2017012119479Warning System · false activationAFTER ENGINE START NR 2 ENGINE GEN OFF BUS AND SOURCE OFF LIGHTS ILLUMINATED. GEN TRIPPED OFF AFTER BEING CONNECTED TO BUS. GROUNDED - YES. ACCOMPLISHED NR 2 GENERATOR CONTROL UNIT BITE PROCEDURE. FOUND IDG FAULT LIGHT ILLUMINATED. RESET FAULT LIGHT. RE-CONNECSDR ASAA2016121719072Connector · dirtyAFTER SETTING CLIMB POWER EGT INDICATION ON ENG NR 1 CLIMBED TO THE AMBER BAND 925 DEG. DISENGAGED AUTO THROTTLES & REDUCED THRUST, EGT DECREASED BUT REMAINED 150 DEG ABOVE NR 2 AT CRUISE POWER. ALL OTHER INDICATIONS NORMAL. GROUNDED - YES. PERFORMED FIM 71-06SDR ASAA2016121619067Door · obstructedR2 DOOR IS JAMMED. GROUNDED - YES. OPENED DOOR, INSPECTED AND CLEARED DEBRIS. CYCLED DOOR OPS NORMAL IAW AMM 52-41-00. OKAY FOR SERVICE.SDR ASAA2016121519062Check Valve · failedNR 1 WING FUEL GAUGE INOPERATIVE. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 WING REFUEL PANEL GAUGE, OP CHECKED GOOD IAW AMM 28-41-61.SDR ASAA2016121419031Warning Message · false activationWARNING LIGHT ILLUMINATED ON OVERHEAD PANEL. ACFT GROUNDED. BITE TEST SHOWS AUX BATTERY CHARGER INOPERATIVE MESSAGE. ACCOMPLISHED FIM 24-31 TASK 825. GROUND VERIFICATION TESTED NORMAL.SDR ASAA2016112018765Compensator · out of limitsWHILE ACCOMPLISHING TSR818110, FOUND RT NR 2 FUEL TANK UNITS F1, F2, F3, F9, F10, AND COMPENSATOR PROBE F15 EMPTY CAPACITANCE TO BE OUT OF LIMITS, IAW AMM 24-41-21-710-801. ACFT GROUNDED. REPLACED THE COMPENSATOR PROBE F15, AND T/U F1, 9, AND 10, IAW AMM 28-SDR ASAA2016111518741Not Reported · failedTECH SERVICES REQUEST CHECK NR 1 FUEL TANK UNIT AND COMPENSATOR VALUES. GROUNDED, YES. ACCOMPLISHED TSR818109 ALL STEPS. FOUND NR 1 FUEL TANK F15=75.01, F1=67.42, F2=43.09, F3=42.93 ARE OUT OF LIMITS REF AMM 28-41-21-710-801. REMOVED AND REPLACED F15 AND F1, ASDR ASAA2016111518701Compensator · failedNR 2 MAIN TANK SHUT OFF AT 8400 LBS, THEN JUMPED TO 8900 LBS. ACFT GROUNDED. COMPLIED WITH FQIS BITE TEST, IAW FIM 28-41 TASK 801. FOUND FAULTS TANK 1, 28-41108 COMPENSATOR DATA BAD AND TANK 2, 28-41208 COMPENSATOR DATA BAD. COMPLIED WITH FIM 28-41 TASK 807SDR ASAA2016110918615Actuator · faultedLEFT PACK LIGHT ILLUMINATED DURING RECALL & RESETS WITH MASTER CAUTION. ACFT GROUNDED. ACCOMPLISHED PACK / ZONE TEMP CONTROL BITE TEST IAW AMM 21-61-00-00, RAM AIR INLET ACTUATOR FAULTED. REMOVED AND REPLACED THE RAM INLET ACTUATOR AMM 21-51-21 AND FAULT CLSDR ASAA2016101518492Bulkhead Web · gougedLEFT MLG WHEEL WELL UPPER PRESURE WEB GOUGED ABOVE LFT MLG ALT EXTEND QUADRANT. ACFT GROUNDED. ACCOMPLISHED REPAIRS TO LT MLG WHEEL WELL PRESSURE DECK WEB IAW REO-G20365 REV A AND EA 800-57EA-17911 REV 00.SDR ASAA2016101318469Baffle · crackedFWD CARGO BAY UNDER TRANSITION PANEL RT BAFFLE CRACKED BS 500C - 500D, STRINGERS 24-25R. ACFT GROUNDED. REMOVED AND REPLACED THE BAFFLE IAW SRM 51-40-02 AND DWG 143A7505 REV.SDR ASAA2016101318468Web · corrodedAFT CARGO BAY LOWER DOOR CUTOUT AREA, FLOOR SUPPORT WEB HAS CORROSION. ACFT GROUNDED. BLENDOUT CORROSION IAW SRM 53-60-15 1A-1 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15. REMOVED AND REPLACED IAW SRM 51-40-02, SRM 51-40-05, AND AMM 53-11-02-420-801.SDR ASAA2016101318467Attach Angle · crackedFWD CARGO BAY, UNDER TRANSITION PANEL, LT BAFFLE ATTACH ANGLE, FWD SIDE OF FRAME, CRACK BS 500H, STRINGERS 24-25R. ACFT GROUNDED. REMOVED AND REPLACED IAW SRM 51-40-02 AND DWG 143A7505 REV.SDR ASAA2016101318463Support · corrodedAFT CARGO BAY, LEFT TRANSITION PANEL SUPPORT FROM BS 727C +10- 727J +10 AND FOUND OUT OF LIMITS. REMOVED AND REPLACED IAW SRM 53-00-53-2R-5 REPAIR 5 AND SRM 53-00-53-2R-5 REPAIR 5.SDR ASAA2016101318458Support Angle · corrodedFWD CARGO BAY LEFT SIDE WALL SUPPORT ANGLE UPPER SURFACE CORRODED BS 500D, STRINGERS 22-25L. ACFT GROUNDED. BLENDED CORROSION IAW SRM 53-00-07, AND FOUND OUT OF LIMITS IAW SRM 53-00-07, REMOVED AND REPLACED THE SIDEWALL SUPPORT ANGLE IAW SRM 51-40-02.SDR ASAA2016101318429Attach Angle · crackedFWD CARGO BAY UNDER TRANSITION PANEL THE ATTACH ANGLE AT THE AFT END OF THE FRAME WAS FOUND CRACKED BS 500H, STRINGERS 24-25R. ACFT GROUNDED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-05, SRM 51-40-02, AND DWG 143A7505.
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