N426AW
Service difficulty reports · 233
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 = 'N426AW' 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 = 'N426AW' 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 A6WA200740609Track · crackedRIGHT ENGINE THRUST REVERSER MAIN TRACK AT 7 O’CLOCK FOUND CRACKED. REPLACED IAW CRJ 200 AMM 78-34-11-801. OP CHECK OF T/R TRANSFERRED TO MWC 115431-208. (M)SDR A6WA200740608Bulkhead · crackedBRACKET CRACK AT JUNCTION OF NET POST AND AFT PRESSURE BULKHEAD FORWARD FACE, FS 621, CARGO BAY AREA. BRACKET FABRIATED IAW CRJ SRM 53-61-23 AND SRM 51-24-16, AND INSTALLED IAW CRJ 20 SRM 51-42-20. (M)SDR A6WA200740604Floorbeam · crackedFOUND CRACK EXIST ON FLOORBEAM AT FUSELAGE STATION 280 RBL 9. REPAIR PERFORMED IAW REO 601R-53-11-171 REV D. (M)SDR A6WA200740261Pump · failedENROUTE FROM DCA T 1252Z HYD2 LOW PRESSURE MESSAGE COMPLIED WITH QRH DIVERTED. HYD QTY NR 2 SYSTEM READS ZERO. PRESSED FDR EVENT BUTTON. LANDING WEIGHT 46900, BRAKE TEMP READS 4,5,4,4. REMOVED AND REPLACED ENGINE DRIVEN HYDRAULIC PUMP NR 2. OPERATIONAL ANSDR A6WA200640376Warning Message · activatedLEFT THRUST REVERSER UNLOCK MESSAGE DURING CRUISE FLIGHT. CWM ACTION REF 154290/4 FOR MEL. DEACTIVATED TR IAW AMM IAW AMM 78-30-00. REMOVED AND REPLACED LT ENGINE POWER DRIVE UNIT IAW AMM 78-32-03. OPERATIONAL CHECK GOOD. (M)SDR A6WA200640361Track · lack of lubeLEFT THRUST REVERSER UNLOCKED CAUTION MESSAGE. COMPLIED WITH QRH. AIR RETURN BACK TO PHL. LUBED LT T/R TRACKS. CLEANED STOW SWITCH. OPS CHECK GOOD IAW 78-30-00. REMOVED FROM MEL. (M)SDR A6WA200640162Skin · lightning strikeFUSELAGE SKIN SUSTAINED LIGHTNING STRIKE DAMAGE AT FS 559, STRINGER 13R AT FASTENER HOLE. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE LIGHTNING STRIKE DAMAGE FUSELAGE SKIN AT RT SIDE FS 559 PLUS 13 BY CUTTING OUT THE DAMAGED SKIN SECTION AND FABRICATING REPAISDR A6WA200640159Engine · power lossREQUEST INSPECTION FOR POSSIBLE LIGHTNING STRIKE. ALTITUDE WAS 5000 FEET GEAR RETRACTED, FLAPS UP. ENGINE NR 2 POWER ROLLED BACK TO 29 PERCENT, N1 FOR TWO MINUTES, ENGINE POWER RECOVERED. NO OTHER INSTRUMENTATION MALFUNCTIONS NOTED. COMPLIED WITH INSPECTIOSDR A6WA200640007Apu · unknownUPON POST FLIGHT INOPERATIVE NOTED SMOKE COMING FROM APU INLET DOOR. INSPECTED APU INLET AND COMPARTMENT FOUND NO EVIDENCE OF OIL LEAK OR SMOKE. RAN APU FOR SEVERAL MINUTES, SHUTDOWN OPS CHECK NORMAL AT THIS TIME. (K)SDR A6WA200540348Handle · corrodedMWC 258 CREW ESCAPE HATCH OUTER HANDLE SHAFT HAS PITTING, CORROSION. REMOVED OUTER HANDLE ASSY AND INSTALLED NEW HANDLE ASSY, PN H341937, IAW AMM. (K)SDR A6WA200540346Floor Support · crackedRT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED. PERFORMED REPAIR TO RT FS 621.00 FLOOR SUPPORT ANGLE IAW REO. (K)SDR A6WA200540345Skin · damagedTHE FUSELAGE 5 KM BETWEEN VS 55.625 PERCENT AND VS 67.5 PERCENT. SPAR DATUM BETWEEN STRINGER 2R AND 4R HAS A DENT 1.5 INCH LONG X 1.875 INCH WIDE X .109 INCH DEEP. REPAIRED DAMAGE TO FUSELAGE SKIN BETWEEN VS 55.625 AND VS 67.5 SPAR DATUM BETWEEN STRINGERS 2RSDR A6WA200540339Skin · nickedNUMEROUS NICKS IN PAIR AND/OR SKIN ON AFT FUSELAGE RT SIDE FS 589 TO 605 BETWEEN STRINGERS 21R TO 26R. REPAIRED DAMAGED AREA IAW EO BY CUTTING AWAY DAMAGE AND INSTALLING FILLERS AND EXTERNAL DOUBLERS. (K)SDR A6WA200540326Floor Support · crackedRT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED. MAINTENANCE PERFORMED REPAIR TO RT FS 621.00 FLOOR SUPPORT ANGLE IAW REO. (K)SDR A6WA200540325Support Angle · crackedLT FS621 FLOOR SUPPORT ANGLE IS CRACKED MAINTENANCE PERFORMED REPAIR TO LT FS 621.00 FLOOR SUPPORT ANGLE IAW REO. (K)SDR A6WA200540344Skin · crackedLT FS640 BONDED SKIN CRACKED. REPAIRED LT BONDED DOUBLER AT FS 640 BY FABRICATING ANGLE AND INSTALLING BETWEEN STR6L AND 14L. (K)SDR A6WA200540343Angle · crackedWO 87925, MWC 213, FS484, RBL36 IB ANGLE OF INTERCOSTAL IS CRACKED .5 INCH LONG. REPAIRED CRACKED ANGLE AT FS 484, RBL36 BY REMOVING AND REPLACING ANGLE WITH FABRICATED ANGLE IAW REO. (K)SDR A6WA200540342Angle · crackedWO 87925, MWC 214, FS484, LBL 36 IB ANGLE OF INTERCOSTAL IS CRACKED .5 INCH LONG. REPAIRED CRACKED ANGLE AT FS 484, LBL 36 BY REMOVING AND REPAIRING ANGLE WITH FABRICATED ANGLE IAW REO. (K)SDR A6WA200540341Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED APPROX 1.0 INCH LONG AT DOOR SUPPORT CABLE PULLEY. CUT AWAY DAMAGED SECTION OF DRAG ANGLE AND INSTALLED REPAIR ANGLE AND SPLICES IAW REO. (K)SDR A6WA200540338Angle · crackedOB CLIP AT FS 280, LBL 9.0 IS CRACKED IN RADIUS AT TOP CLIP, CRACK APPROX .50 INCH LONG. REMOVED AND REPLACED FS 280, LBL 9.0 FLOORBEAM TO BULKHEAD ANGLE IAW SRM (OB CLIP). (K)SDR A6WA200540337Attach Angle · crackedOB CLIP AT FS 280, RBL 9.0 IS CRACKED IN RADIUS AT TOP OF CUP, APPROX .50 INCH LONG. REMOVED AND REPLACED FS 280, RBL 9.0 FLOORBEAM TO BULKHEAD ATTACHMENT ANGLE IAW BRAS SRM (OB CLIP). (K)SDR A6WA200540336Attach Angle · crackedOB CUP AT FS280, RBL 9.0 IS CRACKED IN RADIUS AT TOP OF CUP, APPROX .50 INCH LONG. REMOVED AND REPLACED FS280, RBL 9.0 FLOORBEAM TO BULKHEAD ATTACHMENT ANGLE IAW SRM (OB CLIP). (K)SDR A6WA200540320Intercostal · crackedFS 484, LBL 36, IB ANGLE OF INTERCOSTAL IS CRACKED .5 INCH LONG. (K)SDR A6WA200540319Intercostal · crackedFS484, RBL 36 IB ANGLE OF INTERCOSTAL IS CRACKED .5 INCHES LONG. (K)SDR A6WA200540322Angle · crackedIB CLIP AT FS280, RBL 9.0, IS CRACKED IN RADIUS AT TOP OF CLIP, APPROX .5 INCH LONG. REMOVED AND REPLACED FS 280, RBL 9.0 FLOORBEAM TO BULKHEAD IB ATTACHMENT ANGLE IAW SRM. (K)SDR A6WA200540321Angle · crackedOB CLIP AT FS 280, LBL 9.0, IS CRACKED IN RADIUS AT TOP OF CLIP CRACK APPROX .5 INCH LONG. REMOVED AND REPLACED FS 280, LBL 9.0 FLOORBEAM TO BULKHEAD ATTACHMENT ANGLE IAW SRM (OB CLIP). (K)SDR A6WA200540318Intercostal · crackedFS 621 TO FS 625 TOP RT INTERCOSTAL ANGLE IS CRACKED 1.5 INCH LONG IN AFT RADIUS. (K)SDR A6WA200540317Intercostal · crackedMWC 22, FS 621 TO FS 625 TOP LT INTERCOSTAL ANGLE CRACKED 1.5 INCH LONG IN AFT RADIUS. C/A IN PROGRESS. (K)SDR A6WA200540260Bpsu · inoperativeFLAPS FAIL CAS APPROACH, MYR FLAPS SELECTED NOT MOVE QAR C/W FLAPS ZERO LANDING. ACCOMPLISHED -30 DEGREES. REMOVED AND REPLACED LT BPSU IAW AMM. OPS CHECK GOOD. (K)SDR A6WA200540115Unknown · malfunctionedDURING APPROACH, WHEN SELECTING FLAPS FROM 30 TO 45 AIRCRAFT STARTED ROLLING LT, REQUIRED HALF AVAILABLE AILERON TRIM AND RT CONTROL WHEEL INPUT TO KEEP WINGS LEVEL. FLAP TRAVEL APPEARS UNEVEN. PERFORMED FLAP RIG CHECK, OPS CHECK GOOD. SPOILER SYSTEMS OPS CSDR A6WA200440076Indicator · inoperativeSTANDBY AIRSPEED INOPERATIVE DURING TAKEOFF ROLL AT 80-90 KNOTS. ABORTED TAKEOFF. COMPLIED WITH ABORTED TAKEOFF INSPECTION, NO DEFECTS. PERFORMED P3 CONTAMINATION REMOVAL PER TASK 34-11-00-100-806, AND LEAK TESTED. NO LEAKS DETECTED. (M)SDR A6WA200340084Line · crackedWHILE TAXIING AIRCRAFT LOST NR 3 HYD FLUID LEAKING AROUND NLG. REMOVED AND REPLACD RIGHT INBOARD BRAKE LINE IN NOSE COMPARTMENT. (M)SDR A6WA200340075Line · leakingWHILE TAXIING AIRCRAFT LOST NR 3 HYDRAULIC. FLUID LEAKING AROUND NOSE LANDING GEAR. REMOVED AND REPLACED RIGHT INBOARD LINE IN NOSE COMPARTMENT. (M)
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