N410AW
Service difficulty reports · 297
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 = 'N410AW' 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 = 'N410AW' 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 A6WA200840154Sill · corrodedSERVICE DOOR LOWER SILL PLATE CORRODED. BLENDED IAW SRM 51-21-06. (K)SDR A6WA200840166Diaphragm · missingRUDDER LOWER CLOSURE RIB IS MISSING CLOTH DIAPHRAGM. REPAIRED IAW CRJ 200 REO 601R-55-41-018 REV A. (M)SDR A6WA200840170Attach Fitting · crackedOUTBOARD CLIP AT FS 484 RBL 36 FOUND CRACKED. REPLACED IAW CRJ 200 REO 601R-53-41-059 REV A. (M)SDR A6WA200840167Strip · wornRIGHT NOSE COWL UPPER DOOR AFT STRIP FOUND WORN. REPAIRED IAW CRJ 200 CMM 71-14-01-300-815- A01. (M)SDR A6WA200840172Hinge · crackedPAX DOOR FOLDING STEP UPPER HINGE, REF P/N 601R31980-41, AND LOWER HINGE, REF P/N 601R31980-63, FOUND CRACKED. REPLACED PAX DOOR FOLDING STEP UPPER HINGE IAW SRM 51-42-02 AND REPLACED LOWER HINGE IAW SRM 51-41-02. (M)SDR A6WA200840169Stiffener · crackedON PAX DOOR, STIFFENER ANGLE FOUND CRACK. STIFFENER ON PAX DOOR FS 349. REPLACED IAW SRM 51-42-06. (M)SDR A6WA200840156Drag Angle · crackedPAX DOOR AFT DRAG ANGLE FOUND CRACK. REPAIRED IAW REO 601R-52-11-513 REV A. (K)SDR A6WA200840155Step · crackedPAX DOOR STAIR AFT WEB CRACK ON 1ST AND 2ND STEP CORNER AREA. REPAIRED IAW REO 601R-52-11-702 REV A. (K)SDR A6WA200840164Intercostal · crackedINTERCOSTAL AT FS 484 INBOARD CLIP AT RBL 27 IS CRACKED. REPLACED. (M)SDR A6WA200840161Floorbeam · crackedCROSSBEAM AT FS 280 RBL 9.0, WL 72 IS CRACKED IN RADIUS. (M) REPAIRED IAW REO 601R-53-11-171, REV B. (K)SDR A6WA200840248Handle · seizedFAILURE OF FUNCTIONAL TEST OF CREW ESCAPE HATCH, OUTER HANDLE SEIZED DUE TO CORROSION, DURING C-CHECK. CREW ESCAPE HATCH OUTER HANDLE REPLACED. (M)SDR A6WA200840171Bulkhead · crackedPRESSURE BULKHEAD WEB AT FS 621, LINTEL AREA, IS CRACKED. REPAIRED IAW CRJ 200 REO 601R-53-61-1230 REV D. (M)SDR A6WA200840008Anti-Ice System · malfunctionedGROUND LIFT DUMP UNSAFE CAUTION MESSAGE IN FLIGHT. QRH PROCEDURE CLEARED MESSAGE. COMPLIED WITH OPS CHECK OF SPOILER FLIGHT SYSTEM. IAW SYS IAW AMM 27-60-00 PARA 11. THIS MESSAGE IS CAUSED BY ANIT-SKID PROBLEM. REMOVED AND REPLACED IAW 32-44-06. OPS CHECK GSDR A6WA200740681Thermal Switch · inoperativeWING OVERHEAT WARNING MESSAGE ON CLIMBOUT SYNOPTIC PAGE SHOWS LT WING. COMPLIED WITH QRH, MESSAGE CLEARED. IN OFF, AND APPROXIMATELY 1 MINUTE LATER, REAPPEARED IN STANDBY. REMOVED AND REPLACED LT WING STANDBY THERMAL SWITCH IAW AMM 30, OPS CHECK GOOD. (K)SDR A6WA200740678Warning Message · illuminatedWING OVERHEAT WARNING MESSAGE ON CLIMBOUT, SYNOPTIC PAGE INDICATES LT WING. CORRECTIVE ACTION IN PROGRESS. (K)SDR A6WA200740501Fire Bottle · lowCARGO BOTTLE LOW MESSAGE. COMPLIED WITH QRH, MESSAGE CLEARED DESCENT. FIRE DEPARTMENT INSPECTION FOUND NO EVIDENCE OF HEAT. PLACED ON MEL. REMOVED AND REPLACED LT FIRE BOTTLE, OPS CHECK GOOD IAW 26-20-00 REMOVED OFF MEL.SDR A6WA200740187Unknown · warning lightLT WINDSHIELD HEAT MESSAGE ILLUMINATED IN FLIGHT. COMPLIED WITH QRH. [07-31-07] COMPLIED WITH CONNECTION OF SPARE TEMP SENSORS IAW AMM 30-41-06. OPS CHECK GOOD. (K)SDR A6WA200740094Service Door · malfunctionedSERVICE DOOR WILL NOT OPEN. CYCLED DOOR, OPENED NORMAL. (K)SDR A6WA200640313Connector · looseUNCOMMANDED ROLL FLAPS 45 AIRSPEED MANEUVERING OR GREATER, R-TURN 10-15 DEGREES BANK ANGLE AIRCRAFT CONTINUES TO ROLL INTO TURN. INSPECTED RIGHT SPOILER OUTBOARD PCU AND FOUND CANNON PLUG LOOSE. RESECURED AND PERFORMED OPS CHECK OF RT SPOILERON IAW AMM 27-60SDR A6WA200640227Windshield · crackedCRACKED RIGHT WINDSHIELD, HAPPENED DURING TAXI OUT. REMOVED AND REPLACED WINDSHIELD, OPS CHECK GOOD IAW AMM 56-11-01. (M)SDR A6WA200640089Connector · brokenFOUND FLOOR TRACK LIGHTING CONNECTOR AT LAV BROKE. REMOVED AND REPLACED CONNECTOR ON FLOOR TRACK LIGHTING AT LAV IAW CRJ WM 20-17-10. OPERATIONAL CHECK GOOD CRJ AMM 33-51-00-710-801. (M)SDR A6WA200640056Clip · crackedFS 280 CLIP AT RBL 9.0, IB, IS CRACKED NEAR RADIUS APPROX .90 INCH LONG. MAINTENANCE REMOVED AND REPLACED CLIP IAW SRM. RT IB FS 280 FRAME. (K)SDR A6WA200640055Clip · crackedFS 280 CLIP AT RBL 9.0, OB, IS CRACKED NEAR RADIUS APPROX .80 INCH LONG. MAINTENANCE REMOVED AND REPLACED ANGLE IAW SRM. RT OB FS280. (K)SDR A6WA200640054Clip · crackedFS 280 CLIP AT LBL 9.0, OB, IS CRACKED NEAR RADIUS APPROX .60 INCH LONG. MAINTENANCE REMOVED AND REPLACED ANGLE IAW SRM. LT OB FS 280. (K)SDR A6WA200640060Beam · corrodedJ-ANGLE ON TRANSVERSE BEAM FS 280 BETWEEN LBL 9.0 AND RBL9.0 HAS AREAS OF CORROSION AT CAMLOCK RECEPTICAL. LARGEST AREA MEASURES APPROX 1.5 INCH L X 1.0 INCH W X .009 INCH D. MAINTENANCE REMOVED DAMAGE ANGLE AND INSTALLED NEW ANGLE IAW SRM. (K)SDR A6WA200640058Beam · corrodedTRANSVERSE BEAM AT FS 280 BETWEEN LBL 9.0 AND RBL 9.0 HAS SEVERAL AREAS OF CORROSION. LARGEST AREA MEASURES APPROX 3.5 INC X .80 INCH W .007 INCH D. MAINTENANCE REMOVED DAMAGE SECTION OF TRANSVERSE BEAM (J ANGLE) AND INSTALLED REPLACED ANGLE IAW EO. (K)SDR A6WA200640057Clip · crackedFS 280 CLIP AT LBL 9.0, IB, IS CRACKED NEAR RADIUS APPROX .80 INCH LONG. MAINTENANCE REMOVED AND REPLACED CLIP AT IB LT FS 280 IAW SRM. (K)SDR A6WA200540174Display · malfunctionedCAPTAINS MFD FAILED INFLIGHT, UNABLE TO USE REVISIONARY FUNCTION F/O PFD ERRATIC AND STAB TRIM 1 AND 2 AND MACH TRIM DISENGAGES. INTERROGATED MDC, NO CURRENT FAULTS FOUND, RE-SET CAPTS MFD CB FOR FAILED CAPTS MFD, CND. FAULT PERFORMED NR 1 AND NR 2 ENGINE RUSDR A6WA200540085Screen · dirtyDISPLAY COOL CAUTION MESSAGE INFLIGHT. MESSAGE WAS INTERMITTENT REGARDLESS OF FAN SELECTION. INSPECTED DISPLAY COOLING DUCTING, NO LEAKS NOTED. AIR FILTER GETTING DIRTY HOWEVER NOT CLOGGED. CLEANED AIR SCREEN BEHIND PFD2. ALL THREE FANS BLOW NORMALLY. NOSDR A6WA200440220Control System · bindingFIRST OFFICER REPORTED RT AILERON BINDING ON APPROACH WITH AUTO PILOT SELECTED OFF. INSPECTED AILERON CONTROL SYSTEM IAW SL. FOUND NO EVIDENCE OF MOISTURE OR PULLEY BINDING. NO FAULTS IN MDC. PERFORMED OPS CHECK OF AUTOPILOT, OPS CHECK GOOD IAW 27-11-00.SDR A6WA200440153Duct · separatedMESSAGE IN FLIGHT, QRH COMPLIED WITH. DISPLAY COOL MESSAGE INTERMITTENT IN FLIGHT. ALT POSITION WENT TO STANDBY POSITION THEN EXTINGUISHED THRU FL270 THEN WENT OFF (AIR RETURN). UPON INSPECTION FOUND DUCT ABOVE CAPTAINS RUDDER PEDAL OFF. RESECURED DUCT. OSDR A6WA200440095Sill · crackedFOUND FLOOR SILL PLATE AT CARGO DOOR ENTRANCE IS CRACKED. CUT OUT DAMAGED SECTION OF FLOOR SILL SECTION AND INSTALLED FABRICATED REPAIR SECTION OF FLOOR SILL AND INSTALLED FABRICATED SPLICE DOUBLER IAW BRAS EO 601R-53-5095. (M)SDR A6WA200440092Skin · dentedDENT IN LEFT HORIZONTAL STABILIZER BOTTOM SKIN APPROXIMATELY 74 INCHES FROM VISOR AND 9 INCHES FROM 4E. PERFORMED A MAJOR REPAIR IAW BRAS EO 601R-55-5102 BY DRILLING NR 30 HOLE IN DAMAGE AREA AND PULLING DENT TO ORIGINAL CONTOUR. PERFORMED EDDY CURRENT INSPESDR A6WA200440090Bushing · looseRIGHT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .062 INCH. PERFORMED A MAJOR REPAIR TO MIGRATED RIGHT MLG AFT TRUNNION BUSHING BY REMOVING BUSHING AND INSTALLING 1ST OVERSIZE BUSHING P/N 601R-57-21-003-21 IAW BOMBARDIER REO 601R-57-21-003 REV B. (M)SDR A6WA200440093Airstair · crackedPASSENGER DOOR STAIR STRUCTURE AFT ANGLE IS CRACKED .80 INCH LONG IN AREA OF DOOR ASSIST CABLE PULLEY BRACKET LOCATED IN RADIUS OF ANGLE. CUT AWAY DAMAGED SECTION OF DRAG ANGLE, FABRICATED REPLACEMENT DRAG ANGLE FROM 5773 EXTRUSION AND SPLICE ANGLES FROM $614SDR A6WA200440088Angle · crackedPASSENGER DOOR STAIR STRUCTURE AFT ANGLE, P/N 601R31907-303 IS CRACKED .8 INCH LONG AREA OF DOOR ASSIST CABLE PULLEY BRACKET LOCATED IN RADIUS OF ANGLE. (M)SDR A6W2004F00000Angle · crackedPAX DOOR STAIR STRUCTURE AFT ANGLE, PN 601R31907-303, IS CRACKED .8 INCHES LONG AREA OF DOOR ASSIST CABLE PULLEY BRACKET LOCATED IN RADIUS OF ANGLE. REMOVED CRACKED ANGLE AND INSTALLED A NEW ANGLE PN 601R311719 IAW REO 601R53-41-059.SDR A6WA200440089Access Door · corrodedRIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUT OT AT WS 54.897 HAS FRETTING DAMAGE IN TWO AREAS, INBOARD AND FORWARD .004 IN CHES DEEP AT WORST AREA. REMOVED FRETTING CORROSION ON LOWER WING PLANK FUEL ACCESS DOOR IN THREE PLACES (.004 DEEP) WS 54.897 PANEL SDR A6WA200440083Floor Support · crackedFOUND FLOOR SUPPORT ANGLE BRACKET IS CRACKED AT FS 484, LEFT SIDE, LBL 36. REMOVED CRACKED ATTACHMENT FLANGE AND FABRICATED NEW REPAIR ANGLE, P/N 1 FORM 6144-14 AND INSTALLED IAW BOMBARDIER REO 601R-53-41-059 AND BRAS EO 601R-53-0030. (M)SDR A6WA200440081Angle · crackedFOUND RIGHT SIDE FS 621/FS 625 OBLIQUE ANGLE AT STRINGER 14R IS CRACKED IN RADIUS APPROXIMATELY 1 INCH. REPLACED CRACKED ANGLE WITH NE ANGLE P/N 601-35012-52 IAW CRJ SRM 51-42-06. (M)SDR A6WA200440085Floor Support · crackedFOUND FLOOR SUPPORT ANGLE CRACKED AT FS 484 RBL 27. (M)SDR A6WA200440087Attach Angle · crackedATTACHMENT ANGLES AT FS 621 CRACKED AT LEFT/RIGHT SIDES. PERFORMED A MAJOR REPAIR TO CRACKED UNDER FLOOR SUPPORT ANGLE AT FS 621 LEFT SIDE AND RT SIDE BY REMOVING CRACKED SECTION OF ANGLE AND INSTALLING REPAIR IAW BOMBARDIER REO 601R-53-61-117 REV B. (M)SDR A6WA200440086Floor Support · crackedFLOOR SUPPORT ANGLE AT FS 484 RBL 36 IS CRACKED. REMOVED CRACKED ATTACHMENT FLANGE, FABRICATED NEW REPAIR ANGLE,P/N 2 FROM 6144-14 AND INSTALLED IAW BOMBARDIER REO 601R-53-41-059 AND BRAS EO 601R-53-0030. (M)SDR A6WA200440082Angle · crackedFOUND LEFT SIDE FS 621/FS 625, OBLIQUE ANGLE AT STRINGER 14L IS CRACKED IN RADIUS APPROXIMATELY 1.1 INCH LONG, 1.1 INCHES. REPLACED CRACKED ANGLE WITH NEW ANGLE, P/N 601-35012-51, IAW CRJ SRM 51-42-06. (M)SDR A6WA200340118Acm · failedON TAXI, CABIN BEGAN TO FILL WITH SMOKE. PLACED RT PACK ON MEL. RT PACK MAKING LOUD GRINDING NOISE AND EXCESSIVE VIBRATION. RAN RIGHT ENGINE, CHECKED NR 2 BLEED AND APU BLEED ON NR 1 PACK. NO SMOKE NOTED. REMOVED AND REPLACED AIR CYCLE MACHINE IAW AMM. OSDR A6WA200340074Actuator · malfunctionedYAW DAMPER NR 2 WILL NOT STAY ENGAGED WHEN MOVING AIRCRAFT. YAW DAMP INOPERATIVE STATUS MESSAGE. REMOVED AND REPLACED NR 2 YAW DAMPER ACTUATOR. CHECKS OK. (M)SDR A6WA200240002Odor · detectedAPU AUTO SHUTDOWN IN FLIGHT, CREW RESTARTED INFLIGHT, STRONG FUEL SMELL IN CABIN AFTER APU BLEED AIR SELECTED ON TO FEED PACKS, FUEL ON TAIL OF AIRCRAFT ON GROUND. MAINTENANCE INSPECTED APU WITH APU RUNNING, NO FUEL LEAKS, CHECKED APU OIL LEVEL OK. OPERATED
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