N566AS
Service difficulty reports · 575
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 = 'N566AS' 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 = 'N566AS' 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 ASAA2015100113309Fmc · fault messageWHILE ACCOMPLISHING FMC CDU INTERROGATE TASK CARD 78273000, FOUND RECENT FAULT AND NR 73-31372 ECONOMIC FAULT, NR 2 ENGINE. ACFT GROUNDED, ON DEFERRAL.SDR ASAA2015100113279Unknown · leakingNR 1 ENGINE IDG FREQUENT SERVICING. ACFT GROUNDED. NR 1 ENG, TSR ACCOMPLISHED, NO LEAKS FOUND. REPLACED IDG VENT AND IDG SERVICE FITTING, IAW MM 24-11-00 AND CMM 24-11-85, NO LEAKS FOUND AFTER REPLACEMENT.SDR ASAA2015070312317Window · malfunctionedWINDOW HEAT RT SIDE OVERHEAT LIGHT ILLUMINATED DURING PREFLIGHT. ACFT GROUNDED. REPLACED R-2 WINDOW. OPS CHECK OF WINDOW GOOD PRESSURIZED AC TO 3.5 PSI NO LEAKS NOTED. REF AMM 56-12-11 FOR WORK ACCOMPLISHED.SDR ASAA2015062312196Satcom · lockedSATCOM LOCKUP OCCURRED WITH BUS TRANSFER. ACFT GROUNDED. QRH COMPLIED WITH.SDR ASAA2015050911651Satcom · lockedSATCOM LOCKUP, ACFT GROUNDED. SATCOM LOCKUP CLEARED FOLLOWING QRH PROCEDURE.SDR ASAA2015042311480Transceiver · failedNUMBER 1 HF AUDIO UNUSABLE. GROUNDED - YES. VERIFIED UNREADABLE AUDIO ON GROUND. REPLACED #1 HF TRANSCEIVER PER AMM 23-11-21.SDR ASAA2015040111199Light · inoperativeTHE BACK LIGHTING ON THE FLT ALT AND LAND ALT DIGITAL DISPLAY HAS GONE BLANK. ACFT GROUNDED. REPLACED CABIN PRESSURE CONTROL MODULE IAW AMM 21-31-02-400-801 & 21-31-02-000-801. SYSTEM CM TEST NORMAL, GROUND VERIFICATION SUCCESSFUL, ACFT OK FOR SERVICE.SDR ASAA2015031210937Module · failedPRES PANEL DITG REEAOUT STUCK AT 340-345 IN BOTH AUTO AND ALT MODES. ACFT GROUNDED. VERFIED DISCREPANCY. REMOVED AND INSTALLED NEW CPC MODULE ON P5 PANEL. REF 21-31-02-000-801. INSTALL REF 21-31-02. OPS CHEKS PERFORMED. SYS CHECKS NORMAL.SDR ASAA2015013010490Warning Message · false activationLEFT SIDE WINDOW "OVERHEAT" L2, CAPTAINS SLIDING WINDOW. RAN QRH PROCEDURE "OVERHEAT" RETURNED. TURNED SWITCH OFF REMAINDER FLIGHT. ACFT GROUNDED. FOUND POWER C/B AT P6-12 B9 OPEN. INSPECTED C/B AND TERMINALS WITH NO DEFECTS FOUND. RESET C/B IAW AMM 20-60SDR ASAA2015013010496Fault Code · false activationWHILE PERFORMING T/C 78273000 FOUND ECONOMIC FAULT MESSAGE 73-31372, UPPER EGT SECTORS READING HIGH ON NR 2 ENGINE. ACFT GROUNDED. ACCOMPLISHED TC 78273000, FAULTS NOT PRESENT.SDR ASAA2015012910489Circuit Breaker · trippedLEFT SIDE WINDOW OVERHEAT CAUTION ILLUMINATED DURING CRUISE AT 37,000 FT. PERFORMED QRH PROCEDURE. LIGHT REMAINED ILLUMINATED. WINDOW WAS HOT TO THE TOUCH. ACFT GROUNDED. TROUBLESHOT SYS AND FOUND WINDOW HEAT POWER LT SIDE CIRCUIT BREAKER OPEN ON LOWER P6 SDR ASAA2015012810469Lamp · failedEXTERIOR L2 DOOR EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMP & TESTED GOOD IAW AMM 33-51-04-960-801.SDR ASAA2015012810468Lamp · failedRT FWD OVERWING EMERGENCY EXIT LIGHT HAS A LAMP INOPERATIVE. ACFT GROUNDED. OPENED BOTH RT SIDE OVERWING EXIT DOORS TO ACCESS LAMP CHANGE IAW AMM 52-22-00-508-801. REPLACED THE LAMP IAW AMM 33-51-04-960-801. REPAIRED LENS NUTPLATE REF SRM 51-40-10. CLOSEDSDR ASAA2015011810350Angle · corrodedFWD CARGO BAY BS 500I SEAL ANGLE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-12. REMOVED THE SEAL ANGLE IAW SRM 51-40-02. FABRICATED A NEW SEAL ANGLE IAW DWG 143A9873 AND INSTALLED IAW SRM 51-40-02.SDR ASAA2015011710349Plate · corrodedFWD CARGO BAY LT SIDEPLATE IS CORRODED BS 500H-500I. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW 53-00-53-1A-1. REPAIRED SIDEPLATE IAW SRM 53-00-53-2R-6.SDR ASAA2015011410272Strip · corrodedFWD CARGO BAY AFT RT CAPSTRIP IS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2 ORIGINAL MATERIAL THICKNESS WAS 0.063 IN IAW SRM 53-30-53-0I-1 MATERIAL THICKNESS REMOVED IS 0.009 IN MATERIAL THICKNESS REMASDR ASAA2014122010013Satcom · lockedSATCOM LOCKED UP ON GROUND. ACFT GROUNDED. ACCOMPLISHED QRH, PULLED SATCOM CIRCUIT BREAKER AND RESET. OPS NORMAL.SDR ASAA2014112409740Module · failedFLT ALT WINDOW ON PRESSURE CONTROLLER HAS NUMBER SCROLLING. ACFT GROUNDED. R & R PRESSURE CONTROL SELECTOR MODULE, OPS CK GOOD REF MM TASK 21-31-710-801 AND TASK 21-31-00-700-802. ALL TEST OPS CK GOOD.SDR ASAA2014112309736Fastener · looseDURING A NR 1 ENG INLET FAN BLADE DETAILED INSPECTION, FOUND NR 1 FAN DUCT PANEL AT 12 O'CLOCK POSITION HAS 1 LOOSE FASTENER WITH POSSIBLE FASTENER HOLE DAMAGE. ACFT GROUNDED. TIGHTENED FAN DUCT PANEL NR 1 12 O'CLOCK POSITION. PANEL SECURE, NO DAMAGE NOTED,SDR ASAA2014112309730Indicator · malfunctionedFLT WINDOW ON PRESSURE CONTROLLER HAS UNRELIABLE, UNSTABLE NR SCROLLING. FLIGHT ALT DESIRED IMPOSSIBLE TO INPUT. ACFT GROUNDED. CYCLED POWER FROM JET POWER TO APU AND PRESSURIZATION CONTROL MODULE READING CAME TO NORMAL. BOTH PRESSURIZATION CONTROLLERS BITSDR ASAA2014111509669Connector · brokenNR 2 ENGINE FIRE DETECTION SYS DOES NOT TEST PROPERLY. ACFT GROUNDED. T/S AND FOUND LUG BROKEN OFF OF RT SIDE FIRE DETECTOR ENGINE CORE. REPLACED LUG IAW SWPM REF 20-30-11. PERFORMED FIRE AND OVERHEAT DETECTION SYSTEM/OPS TEST IAW AMM REF 26-10-00-710-801, SDR ASAA2014111209648Fire Loop · inoperativeNR 2 FIRE LOOP B INOPERATIVE. ACFT GROUNDED. NO PREVIOUS HISTORY. UNABLE TO DUPLICATE. GROUND VERIFICATION TEST GOOD REF TASK 26-11-00-710-801.SDR ASAA2014110909622Circuit Breaker · trippedAFCS SYS A WARNING LIGHT CIRCUIT BREAKER FOUND EXTENDED. ACFT GROUNDED. RESET CIRCUIT BREAKERS IAW AMM 20-60-01, WDM 22-14-11 AND WDM 22-31-11. CIRCUIT BREAKERS REMAIN SET. ACCOMPLISHED DFCS BITE LIBRARY TEST NR 60 ,CHANNEL A DISENGAGE WARNING. ACCOMPLISHEDSDR ASAA2014110709604Start Valve · frozenPILOT REPORTED NR 1 ENGINE FAILED TO CRANK. ACFT GROUNDED. HEATED NR 1 ENGINE START VALVE OP'S NORMAL.SDR ASAA2014102109448Warning Light · false activationP5-13 TR UNIT ANNUNCIATOR LIGHT ILLUMINATED. WARNING HORN IN NOSE WHEEL WELL ON. ACFT GROUNDED. FOUND TRU2, TRU3, & EQUIPMENT COOLING EXHAUST FAN NORMAL. REF WDM 24-51-11, 24-51-21, 24-32-11, & 21-27-21. REMOVED TRU 1&2. GVI OF TR'S & ASSOCIATED WIRING. NO SDR ASAA2014100209295Shim · wornNR 1 ENGINE FAN BLADE SHIMS MOLYDAG COATING WORN. ACFT GROUNDED. R & R FAN BLADE SHIMS IAW T/C 78472002.SDR ASAA2014091709153Start Valve · stickingNR 1 ENGINE START VALVE OPEN LIGHT REMAINED ILLUMINATED AFTER ENGINE START. START SWITCH CUTOUT NORMALLY. START VALVE OPEN LIGHT EXTINGUISHED WHEN THE APU BLEED VALVE WAS CLOSED. ACFT GROUNDED. FOUND START VALVE NR 1 ENGINE STICKING OPEN. REPLACED START VSDR ASAA2014091209121Shim · wornNR 2 ENGINE, FAN BLADE SHIMS MOLYDAG COATING WORN. ACFT GROUNDED. R & R NR 2 ENGINE FAN BLADE SHIMS IAW T/C 78472002.SDR ASAA2014090209041Warning Message · false activationFMC DISAGREE LIGHT ON TAXI OUT OF PSP. ACFT GROUNDED. RAN QRH FMC DISAGREE NO LONGER DISPLAYED.SDR ASAA2014081808881Clamp · brokenDURING INSPECTION OF RT ENGINE WIRE HARNESS IAW TASK CARD N8420001. FOUND LT UPPER FIRE DETECTION HARNESS CLAMP BROKEN. ACFT GROUNDED. INSTALLED CLAMP IAW IPC REF 26-11-02-01.SDR ASAA2014081608846Hf Comm · malfunctionedHF1 & 2 INOPERATIVE. ACFT GROUNDED. ACCOMPLISHED RADIO TUNING PANEL-INOPERATIVE DISPLAY TOGGLE IAW AMM 23-12-41-800-802. VERIFIED HF 1, 2 & VHF 3 PLUS VHF 1 & 2 OPS NORMAL.SDR ASAA2014073108742Actuator · leakingFUEL PUDDLE UNDER NR 2 ENGINE. ACFT GROUNDED. PERFORMED NR 2 ENGINE VENT AND DRAIN INSPECTION IAW AMM 71-70-00-200-801-F00. FOUND RT VSV ACTUATOR LEAKING AT 9 DROPS A MINUTE. REPLACE RT VSV ACTUATOR WITHIN 75 CYCLES. ON DEFERRAL.SDR ASAA2014071808602Regulator · failedDURING CLIMB OUT, THE RT PACK INDICATED 8PSI AND THE LT PACK INDICATED 40 PSI. LEVELED OFF AT FL320 FOR SEVERAL MINUTES WITH NO CHANGE. OUT FINAL ALTITUDE WAS FLIGHT LEVEL 380, AND STILL NO CHANGE. ACFT PRESSURE PANEL INDICATED NORMAL DURING CLIMB AND AT SDR ASAA2014071608576Indicator · faultedACTIVE, CURRENT, FAULT 49-94300,OIL FILTER, START GENERATOR SHOWS SHORT CIRCUIT. APU DID NOT EXPERIENCE A START FAULT, ACFT GROUNDED. IAW FIM 49-90, TASK 810: DETERMINED MOST LIKELY DEFECT TO BE: START GENERATOR OIL FILTER INDICATOR, ELECTRIC SWITCH. R & R SDR ASAA2014070608469Pressure Switch · bypassingLEFT FUEL FILTER BYPASS LIGHT ILLUMINATED TAXING IN. ACFT GROUNDED. REPLACED NR 1 ENG FUEL FILTER DIFFERENTIAL PRESSURE SWITCH IAW AMM 73-34-01. REPLACED J8 HARNESS REF MM 73-21-06, GROUND VERIFICATION TEST PASSED.SDR ASAA2014070308449Bleed Valve · failedDURING CLIMBOUT WITH BOTH AC PACKS IN AUTO, LEFT BLEED DUCT READ 43PSI RT PACK 20 PSI. ACFT GROUNDED. PERFORMED NR 1 ENG & NR 2 ENG BLEED AIR HEALTH CHECK REF T/C NG-36WC-0001. FOUND NR 1 ENG PRSOV HAD INTERNAL LEAKAGE. REPLACED LT ENGINE PRSOV REF AMM 36-11SDR ASAA2014062408342Satcom · malfunctionedSAT COM NOT DISPLAYING ON ACARS APPLICATION PAGE. ACFT GROUNDED. PERFORMED FIM TASK 23-15/801. RESET SYSTEM PROMP <SAT> RETURNED. OK FOR SERVICE. NO HISTORY PAST 30 DAYS.SDR ASAA2014062208184Regulator Valve · failedDUCT SPLIT OF 23 PSI OBSERVED AT FL390 AT M785. RIGHT DUCT SHOWS 21 PSI AND LT SHOWS 44 PSI. THE DUCT SPLIT VARIES FROM 23 PSI-18 PSI AT DIFFERENT POWER SETTINGS WITH THE RT ALWAYS INDICATING LESS THEN THE LT DUCT. ACFT GROUNDED. PERFORMED TC NG-36WC-00001SDR ASAA2014062008297Warning Light · false activationFMC DISAGREE LIGHT ILLUMINATED ON GROUND. ACFT GROUNDED. PERFORMED CHECKLIST AND LIGHT EXTINGUISHED.SDR ASAA2014061408190Engine · unknownDURING THE START OF NR 2 ENGINE, START VALVE OPENED AND THERE WAS LITTLE N1 AND N2. ACFT GROUNDED.SDR ASAA2014060208020Circuit Breaker · trippedMCP DC1 CIRCUIT BREAKER IS OUT. ACFT GROUNDED. VERIFIED CIRCUIT BREAKER IS OPEN. ACCESSED P18-1 AND ACCOMP G.V.I. OF CIRCUIT BREAKERS NO DEFECTS NOTED. CLOSED P18-1 AND CLOSED CIRCUIT BREAKER. ACCOMPLISHED MCP INST TEST, TEST PASSED IAW MM 22-11-34-740-80SDR ASAA2014052307904Sensing Element · failedR2 WINDOW OVERHEAT LIGHT IS ON. ACFT GROUNDED. PERFORMED WHCU BITE TEST, FOUND WINDOW SENSOR FAULT. SWAPPED R2 WINDOW SENSOR IAW FIM 30-41, TASK 811. R2 WINDOW OPS CHECK NORMAL REF AMM 30-41-00. SYS GROUND CHECK OK.SDR ASAA2014042807622Satcom · malfunctionedSATCOM LOCKED UP ON GROUND. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE TO RESTORE SATCOM. OPS NORMAL.SDR ASAA2014042307567Key Pad · failedCAPTAIN`S MCDU KEYPAD INOPERATIVE. ACFT GROUNDED. REPLACED CAPTAIN'S MCDU. RESET CIRCUIT BREAKERS, SYS TESTED GOOD IAW TASK 34-61-01-400-802. REMOVED SEAM C.SDR ASAA2014041107522Fmc · malfunctionedDURING CRUISE, NR 1 FMC KEYPAD LOCKED UP ON LEGS PAGE, UNABLE TO CHANGE FMC PAGES OR INPUT DATA VIA NUMERICAL KEYS, ALL LEGS PAGE DATA WAS NORMAL COMPARED TO NR 2 FMC AFTER 15 MIN, KEYPAD FUNCTIONALITY RETURNED TO NORMAL, NO OTHER ISSUES. ACFT GROUNDED. ACCOMSDR ASAA2014030607112Warning Message · illuminatedVTK FLAG DISPLAYED ON F/O'S NAV DISPLAY. FOLLOWED FMC QRH. NO BEARING/DISTANCE INFO DISPLAYED ON POS SHIFT. ACFT GROUNDED. RESET RT FMS AND BITE TESTS NORMAL IAW FIM 34-61, TASK 801. ETOPS SIGNIFICANT SYS, GROUND VERIFICATION SUCCESSFUL.SDR ASAA2014021206842Spinner · damagedWHILE ACCOMPLISHING ENGINE INLET INSPECTION ON NR 2 ENGINE, FOUND SPINNER FRONT CONE WITH MORE THAN 50 PERCENT MISSING ANODIZED COATING. ACFT GROUNDED. ON DEFERRAL.SDR ASAA2014021206839Strut · wornWHILE ACCOMPLISHING ENGINE INLET INSPECTION ON NR 2 ENGINE T/C 78472000. FOUND OTBD UPPER AND LOWER FASTENERS MISSING ON NR 4 FAN FRAM STRUT, 3 O`CLOCK LOOKING FORWARD, FAN DUCT PANEL NR 5 WITH A FASTENER THAT WILL NOT TIGHTEN, AND FAN DUCT PANELS NR 1 AND NSDR ASAA2014021206837Cdu · failedON PUSHBACK AND AFTER START AND POWER SWITCH TO ACFT GENERATORS LOST NR 1 CDU. ACFT GROUNDED. CYCLED C/B'S, NO HELP. R & R CAPT'S MCDU IAW AMM 34-61-01-400-802. OPS NORMAL. ETOPS PN VERIFICATION SEAMC ED.SDR ASAA2014012712503Sign · missingEXIT SIGN MISSING. ACFT GROUNDED. SECURED EXIT SIGN IN MID CABIN, OPS CHECKED GOOD.
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