N466AW
Service difficulty reports · 169
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 = 'N466AW' 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 = 'N466AW' 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 A6WA2019080946783Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS 2 AREAS THAT HAVE MULTIPLE INDICATIONS NOTED. 1) BL0.0 WL112-106 6 INCHES LONG 90% FSH, 2) RBL 18.00 . 2 INCHES LONG 50% FSH. BOTH FAILED NDT INSPECTION.SDR A6WA2019061746660Warning Message · illuminatedMULTIPLE STEERING INOP CAUTION MESSAGES IN FLIGHT WITH GEAR UP. C/W'D QRH & MESSAGES PERSISTED. CYCLED STEERING AFTER LANDING, MESSAGE RETURNED AND PERSISTED. (CREW DECLARED EMERGENCY)SDR A6WA2019052846639Unknown · malfunctionedREF 315380/3,4 & 314381/1 ON APPROACH AFTER SELECTING GEAR HANDLE DOWN, RECEIVED NOSE DOOR OPEN, & GEAR DISAGREE WARNING MESSAGES AFTER APPROXIMATELY 15 SECONDS AFTER SELECTING GEAR HANDLE DOWN. LEFT & RIGHT GEAR SHOWED DOWN, NOSE GEAR SHOWED UP. RAN QRH & USESDR A6WA2019050246593Warning System · activatedRECEIVED WARNING GEAR DISAGREE TWICE AND MESSAGE DISAPPEARED WITH GEAR UP. MESSAGE APPEARED 3RD TIME AND WAS PERMANENT. DECLARED EMERGENCY AND PERFORMED MANUAL LANDING GEAR RELEASE PER QRH.SDR A6WA2019022546410Warning Message · false activationUPON GEAR EXTENSION THE CREW RECEIVED A GEAR DISAGREE ALONG WITH A NOSE DOOR CAUTION. THEY PERFORMED A GO-AROUND, DECLARED AN EMERGENCY AND RAN THE QRH. THE MESSAGE CLEARED AND THE EMERGENCY LANDING WAS CANCELED. THE FLIGHT LANDED WITHOUT INCIDENT. ARFF DID NOSDR A6WA2018040945762Wire Harness · damagedAFTER TAKEOFF, RECEIVED A GEAR DISAGREE AND NOSE DOOR WARNING, AFTER SELECTING THE GEAR UP. COMPLIED WITH QRH, PULLED THE EMERGENCY GEAR EXTENSION HANDLE, GEAR INDICATED DOWN, 3-GREEN AND MESSAGES CLEARED. LANDING WAS NORMAL. INSPECTED AND FOUND NLG CENSDR A6WA201745176Frame · corrodedFRAME 333 HAS CORROSION ON THE FWD SIDE BETWEEN STRINGER 23R AND 22R IN THE FWD E&E BAY.SDR A6WA201745159Skin · damagedLEFT INBD FLAP HAD AN OVERSIZED HOLE COMMON TO THE INBD SEAL AT AFT END.SDR A6WA201745171Stringer · crackedSTRINGER 20R CRACKED BETWEEN FS 333.00 AND 349.00. REPLACED STRINGER 20R IAW SRM 51-42-06, 51-42-21.SDR A6WA201745170Intercostal · crackedCORRODED INTERCOSTAL AT FS 333.00 TO 349.00, STR 20R IS CRACKED BETWEEN FASTENER HOLES. REPLACED INTERCOSTAL IAW SRM 51-42-06.SDR A6WA201745157Transition Panel · crackedTRANSITION PANEL 620ML IS CRACKED AT SCREW HOLE. REPAIRED PANEL 620ML IAW SUPP 13-141 DATED 12-16-2013.SDR A6WA201745158Bulkhead Web · crackedCRACKED REPAIR ON THE AFT PRESSURE BULKHEAD WEB, BS 621.00, LT SIDE. REPAIRED IAW REO 601R-53-61-1230, REV-F.SDR A6WA201745166Frame · corrodedFRAME BS 310 CORRODED BETWEEN STRINGERS 23L AND 26R. REPLACED THE FRAME IAW SRM 51-42-06, AND 51-42-21.SDR A6WA201745169Stringer · corrodedSTRINGER 24R CORRODED BETWEEN BS 280 AND 319.7. REPAIRED THE STRINGER IAW SRM 53-00-03.SDR A6WA201745167Plate · corrodedSPLICE ANGLE PLATE CORRODED JUST AFT OF FRAME 280, STRINGERS 22R TO 23R. REPLACED THE SPLICE ANGLE PLATE IAW IAW SRM 51-42-06.SDR A6WA201745165Frame · corrodedFRAME BS 295 CORRODED BETWEEN STRINGERS 23R AND 25R. REPLACED THE FRAME IAW SRM 51-42-06, AND 51-42-21.SDR A6WA201745161Skin · chafedLEFT AILERON LOWER SURFACE IS CHAFED ON L/E. REPLACED THE SKIN IAW SRM 51-42-21, AND 51-42-06.SDR A6WA201745160Vane · chafedLEFT INBD FLAP VANE IS CHAFED ON LE AT MULTIPLE AREAS. REPLACED THE INBD AND MID LEADING EDGES IAW SRM 51-42-13, OTBD LEADING EDGE IN LIMITS IAW REO 601R-57-52-004.SDR A6WA2017073145139Cargo Track · corrodedCARGO TRACK CORRODED FROM BS 559+112 TO 574, RBL 9. REPLACED THE CARGO TRACK IAW REO 601R-53-00-485, REV B, AND SRM 51-42-02.SDR A6WA2017073145140Bracket · corrodedPAX DOOR LOWER SILL FWD AND AFT CONNECTOR PLUG BRACKETS CORRODED.SDR A6WA201643974Strap · missingEMERGENCY ROPE RETAINING STRAP MISSING.SDR A6WA201643909Aileron · stiffABNORMAL RESISTANCE WITH AILERON CONTROLS. FELT ON BOTH SIDES. GREATER STIFFNESS WHEN TURNING RT.SDR A6WA201643688Latch · dirtyPILOT REPORTED SERVICE DOOR DIFFICULT TO OPEN. HANDLE WAS DIFFICULT TO MOVE. DOOR TRAVELED FREELY ONCE HANDLE RELEASED. CLEANED, LUBRICATED & ADJUSTED INNER HANDLE LATCH ASSEMBLY IAW AMM 52-41-00. OPERATIONS CHECKED GOOD.SDR A6WA201543078Link · wornFLIGHT 9368, AFTER TAKEOFF, ACCELERATED TO 200 KTS, AIRPLANE HAD A TENDENCY TO BANK RIGHT. ACCELERATED TO 250 KTS, ACFT TRIM PAST THE FIRST TRIM MARK ON AILERON TRIM INDICATOR WITH ZERO AILERON TRIM & NO PILOT INPUT, THE ACFT STARTED A CONTINUOUS ROLL TO THESDR A6WA201542962Skin · chafedCARGO DOOR OUTER SKIN IS GOUGED AT TOP CENTER.SDR A6WA201542947Bulkhead · damagedFORWARD FACE OF FS 621 BULKHEAD HAS MULTIPLE SCREW SHANK MARKS.SDR A6WA201542952Handle · crackedPASSENGER DOOR OUTER HANDLE CRACKED.SDR A6WA201542939Fitting · crackedBATHTUB FITTING CRACKED AT LBL 9 & FS 461.SDR A6WA201542955Mount Bracket · crackedNUMBER 1 HYDRAULIC SYSTEM PRESSURE FILTER MOUNT BRACKET HAS CRACK IN LOWER AFT CORNER.SDR A6WA201542941Fitting · crackedRIGHT SIDE WINDOW POST LOWER OUTBOARD CLIP CRACKED.SDR A6WA201542946Bulkhead · dentedFS 621 BULKHEAD WEB HAS SHARP DENT AT LBL 23, 2.5" ABOVE FLOOR.SDR A6WA201542940Fitting · crackedBATHTUB FITTING CRACKED RBL 9 AT FS 461.SDR A6WA201542954Housing · crackedCARGO DOOR HANDLE HOUSING CRACKED.SDR A6WA201542953Fitting · corrodedFS 280.00, RBL 9 & LBL 9, INBOARD & OUTBOARD CLIPS CRACKED.SDR A6WA201542956Skin · chafedRIGHT INBOARD FLAP VANE LEADING EDGE SKIN CHAFED THREE SPOTS. MID & INBOARD LOCATIONS BEYOND LIMITS.SDR A6WA201542945Angle · crackedPASSENGER DOOR ASSIST MOTOR MOUNT ANGLE CRACKED.SDR A6WA201542957Structure · crackedWING LEADING EDGE TRANSITION BETWEEN INBOARD & CENTER LEADING EDGES UNDER PANEL 620ML UPPER AFT CORNER CRACKED.SDR A6WA201542944Drag Angle · crackedRIGHT MAIN LANDING GEAR WHEEL WELL BATTERY RIB DRAG ANGLE CRACKED.SDR A6WA201542431Unknown · odorAFTER APU START, PACKS TURNED ON, BAD FUEL SMELL THROUGHOUT ACFT.SDR A6WA201441940Light · missingFIRST ORANGE FLOOR TRACK LIGHT STRIP MISSING. PLACARDED & PLACED ON MEL.SDR A6WA201309054149Cargo Track · corrodedCARGO TRACK CORRODED AROUND FASTENERS AT FS 559+110 - 566 RBL9. R & R WITH SERVICEABLE CARGO TRACK IAW AMM 53-01-11.SDR A6WA201309054148Cargo Track · corrodedCARGO TRACK IS CORRODED. REPLACE TRACK.SDR A6WA201309054146Sill · corrodedPAX DOOR LOWER SILL HAS CORROSION DAMAGE. R & R SILL.SDR A6WA201309054145Support Bracket · crackedEXTERNAL GROUND POST SUPPORT BRACKET IS CRACKED. R & R BRACKET.SDR A6WA201309044158Fairing · gougedLT JET PIPE FAIRING HAS GOUGE PUNCTURE HOLE ON L/E STIFFENER. REMOVED DAMAGED STIFFENER AND INSTALLED NEW, IAW CMM 20-23-00,20-42-06, 20-40-11, 20-42-20.SDR A6WA201309044154Intercostal · crackedAPU INLET DOOR INTERCOSTAL IS CRACKED. REMOVED DAMAGED INTERCOSTAL AND INSTALL NEW IAW SRM 51-42-06.SDR A6WA201309044150Tie Down · corrodedCARGO TRACK CORRODED ON LBL 27 AT FS 559+110, 559+112, 568. R & R CARGO TRACK IAW SRM 51-41-02.SDR A6WA201309034157Shield · crackedRT ENGINE JET PIPE FIRE DETECTOR LOOP SHIELD IS CRACKED. REPLACED WITH SERVICEABLE FIRE DETECTOR LOOP SHIELD.SDR A6WA201309034156Bracket · crackedRT ENGINE JET PIPE FIRE LOOP SHIELD FWD SUPPORT MOUNT BRACKET IS CRACKED. REPLACED WITH NEW SERVICEABLE BRACKET.SDR A6WA201309034155Bracket · crackedNR 2 HYD FILTER ASSY BRACKET IS CRACKED AT AFT LOWER CORNER. CUT OUT DAMAGE AND INSTALL ANGLE IAW REO 601R-53-62-031, REV A.
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