N57111
Service difficulty reports · 121
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 = 'N57111' 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 = 'N57111' 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 CALA2010110200518Socket · defectiveEMERGENCY SLIDE LIGHT (EXT) AT L4 DOOR WILL NOT TEST. CHANGED ATA 3300 TO 3350. RELAMPED, NO HELP. CHECKED FUSES, ALL OK. FOUND 6.5VDC AT LIGHT ASSY. REQ'S LIGHT ASSY, NSU LAX. PLACARD INOP PER MEL. REMOVED AND REPLACED SOCKET IAW AMM 35-51-09 OPS CHECKSDR CALA2009122800771Light · inoperativeFLOOR LEVEL EMERGENCY EXIT SIGN AT LEFT FWD EMERGENCY OVERWING EXIT HAS BULB INOPERATIVE. REMOVED AND REPLACED BULBS IN EXIT SIGN, OPS CHECK GOOD IAW AMM 33-51-10.SDR CALA2009112000685Gcu · malfunctionedLT AND RT UTILITY BUSES TRIPPED FOR ABOUT 3-4 SECONDS IN FLIGHT. ALSO LT AND RT UTILITY BUS MESSAGE APPEARED ON EICAS. UTILITY BUSES RESET THEMSELVES. GALLEY POWER AND VIDEO TURNED OFF. T/S PER MM 24-22-00, REMOVED AND REPLACED LT AND RT GCU AND BPCU AS PESDR CALA2009110900680Skin · crackedR-4 DOOR LIGHTENING HOLE NEAR VERTICAL ADJUSTMENT TORQUE TUBE HAS CRACK. ACCOMPLISHED REPAIR PER ECRA 5210-02105.SDR CALA2009101600630Floorbeam · misrepairedSTATION 720 FLOORBEAM APPROXIMATELY LBL 45 PREVIOUS REPAIR IMPROPERLY ACCOMPLISHED. REMOVED AND REPLACED REPAIR PER B757 SRM 53-00-51.SDR CALA2009101500625Floorbeam · corrodedSTATION 1640 T-CAP ON FLOORBEAM HAS CORROSION NEAR BUTTLINE 0 FOUND CORROSION OUT OF LIMITS. REPAIRED T-CAP PER SRM 53-00-51 REPAIR 3.SDR CALA2009062500331Fuse · blownL4 EXTERIOR EMERGENCY LIGHT NO POWER. T/S IAW WDM 33-51-22 & AMP; SSM 33-51-01. FOUND BAD FUSE ON M737. REPLACED FUSE & AMP; RELAMPED. ALL OPS NORMAL.SDR CALA0800474Control Panel · defectiveAT 23,000 FT, RT ENG FIRE AND OVERHEAT WARNING CAME ON. ACCOMPLISHED ENGINE FIRE / SHUTDOWN CHECKLIST. FIRE LIGHTS STAYED ON. BLEW BOTH BOTTLES. POSITIVE OIL PRESSURE ON SHUTDOWN, 15 MINUTE WINDMILL ON ENGINE. TROUBLESHOT PER FIM 26-11-00. FOUND NR 2 ENGSDR CALA0700328Skin · delaminatedTHE RUDDER TRAILING EDGE SKIN WAS FOUND DELAMINATED OVER AN AREA OF APPROXIMATELY 0.50 INCH BY 1.9 INCH AT RUDDER STA 175. THE DELAMINATION WENT THROUGH THE ENTIRE THICKNESS OF THE LT RUDDER PANEL AND APPROXIMATELY 20% OF THE THICKNESS OF THE RT RUDDER PANEL.SDR CALA0700307Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED UNDER RT AIRFONE ANTENNA AT STA 1510, RBL 10, S28R-29R. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-00-01, REPAIR NR 5.SDR CALA0600147Stringer Clip · corrodedINSPECTION FOUND STRINGER CLIP CORRODED AT STA 1140, S3R. THE STRINGER CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0500059Skin · delaminatedINSPECTION FOUND THE LT WING O/B FIXED LEADING EDGE SKIN TOP SURFACE DELAMINATED AT WS 380. REPAIRED IAW SRM 51-40-02, 51-70-07, 51-70-17 AND EA 5731-01010.SDR CALA0500055Intercostal · corrodedINSPECTION FOUND MAIN CABIN INTERCOSTAL CORRODED BETWEEN BS 680 AND 700, RBL 56, WL 208. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, PARA 4 AND 7.SDR CALA0500054Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER STRAP CORRODED AT BS 720 FROM LBL 60 TO RBL 60. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAE SRM 51-40-05.SDR CALA0500051Floorbeam · corrodedINSPECTION FOUND CORROSION ON FLOORBEAM IN L-2 DOOR AREA AT BS 720, LBL 65. REPAIRED IAW SRM 53-00-51, FIGURE 201.SDR CALA0500053Intercostal · corrodedINSPECTION FOUND GALLEY SUPPORT INTERCOSTAL CORRODED AT BS 680-700, RBL 15. THE GALLEY SUPPORT INTERCOSTAL WAS REPLACED IAW SRM 51-40-02, PARA 4 AND 7.SDR CALA0400599Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 215.25-223.5, S15R TO S16R, WL 188 JUST BELOW RT AOA VANE. THE SKIN WAS REPAIRED IAW ECRA 5310-04429. A DIP WAS ISSUED TO ACCOMPLISH AN INITIAL INSPECTION WITHIN 25,000 FLIGHT CYCLES AND TO PERFORM REPEAT INSPECTISDR CALA9900655Stringer · crackedINSPECTION FOUND A CRACK IN STRINGER 22L AT STA 1610-1640. A STRINGER SPLICE REPAIR WAS PERFORMED IAW SRM 53-00-03 AND ECRA 5331-01055.SDR CALA9900659Floorbeam · corrodedINSPECTION FOUND TOP CHORD OF FLOORBEAM CORRODED AT STA 324, RBL 42. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, PAGES 216-219 AND ECRA 5321-01049.SDR CALA9801353Panel · crackedINSPECTION FOUND A 10.5 INCH CRACK IN LT WING LEADING EDGE AT THE OUTBOARD END OF NR 1 LEADING EDGE SLAT. THE SURFACE WAS PREPARED IAW SRM 51-70-06. THE AREA WAS REPAIRED IAW ECRA 5720-01662. A DIP WAS ISSUED FOR FOLLOW-UP INSPECTION AND PERMANENT REPAIR PESDR CALA9801352Panel · crackedINSPECTION FOUND THE RT WING LEADING EDGE CRACKED IN TWO PLACES BETWEEN SLATS NR 7 AND NR 8. THE CRACKS WERE 5.5 AND 9.5 INCHES LONG. THE SURFACE WAS PREPARED IAW SRM 51-70-06. THE AREA WAS REPAIRED IAW ECRA 5720-01662. A DIP WAS ISSUED FOR FOLLOW-UP INSPE
Back to N57111