N13113
Service difficulty reports · 126
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 = 'N13113' 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 = 'N13113' 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 CALA2011092100616Charger · inoperativeEMERGENCY EXIT LIGHTS BETWEEN ROWS 7 & 14 LEFT INOP. FAULT TRACED TO INOP BATT CHARGER AT 9DEF. CHARGER REPLACED OPS CHECK OK IAW 33-51-07. SER NO OFF 36675 ON 41040 TAG NO GRN12374 9.SDR CALA2011032400172Skin · damagedLEFT WING NR 3 FLAP TRACK AFT FAIRING FWD I/B MOUNTING BRACKET HOLES IN FLAP ARE ELONGATED. REPAIRED MOUNTING HOLES IN FLAP AND REPLACED BRACKET PER EC/RA 5750-04368 STEPS 1 THRU 18. INITIATED DIP PER EC/RA 5750-04368 STEP 19.SDR CALA2011032100159Skin · dentedLOWER EXTERNAL FUSELAGE, DENT JUST AFT & TO THE LEFT OF FWD ACCESS DOOR STA 253 LBL 13 REPAIRED DENT REF EC/RA 5330-04113 PLACED ON DIP FOR DTA PER ECRA 5330-04113 ORIG, PART 1, STEP 9, ACCOMPLISH A PERMANENT REPAIR WITHIN 24 CALENDAR MONTHS OF MARCH, 16 2011.SDR CALA2011032100158Skin · dentedLT LOWER EXTERNAL FUSELAGE, 2 DENTS SIDE BY SIDE AT STA 430 AT 22L COMPLIED WITH ECRA 5330-04110 STEPS A, B AND C 1 THROUGH 8. INITIATED DIP TO ACCOMPLISH A PERMANENT REPAIR PER PART 3 WITHIN 24 MONTHS. PER ECRA 5330-04110 ORIG, PART 1, STEP C, 8, ACCOMPLISHSDR CALA2011032900227Structure · crackedDOOR HAS A .25 INCH CRACK AT EDGE OF LWR AFT LIGHTENING HOLE. TRIMMED OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER EC/RA 5210- 02238,STEPS 1 THRU 15.SDR CALA2011032400174Skin · dentedLT LOWER EXTERNAL FUSELAGE, DENT AT STA 459 STR 23 LT COMPLETED ALL STEPS OF REPAIR TO LOWER FUSELAGE SKIN AT STA 459 STR 23 LT REF SRM 53-00-01 REPAIR 2.SDR CALA0700181Support Bracket · unknownR1 DOOR WILL NOT CLOSE AND LATCH. REPAIRED IAW AMM 52-11-04.SDR CALA0500418Floorbeam · corrodedINSPECTION FOUND UPPER AND LOWER SURFACE OF FLOORBEAM CORRODED AT STA 1640, RBL 8. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51.SDR CALA0500417Stringer · corrodedINSPECTION FOUND FLOOR STRINGERS AT CROSS STRAP IN AFT BAG BIN CORRODED AT STA 1467, LBL 26. THE CORROSION WAS REMOVED AND ONE AREA WAS OUT OF LIMITS. A REPAIR WAS INSTALLED IAW SRM 51-70-11, FIGURE 1. THE OTHER AREAS WITHIN LIMITS WERE TREATED AND PRIMED ISDR CALA0500413Crease Beam · corrodedINSPECTION FOUND CREASE BEAM INNER CHORD CORRODED AT STA 1600, LBL 63. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-12 AND ECRA 5310-04501.SDR CALA0500412Pan · corrodedINSPECTION FOUND AFT LAV PAN CORRODED AT AFT SIDE, STA 1340-1620, RBL 2 TO RBL 20. THE CORRODED LAV SERVICE PAN DOUBLER WAS REMOVED AND A NEW PAN DOUBLER WAS INSTALLED IAW SRM 51-40-02 AND ENGINEERING DRAWING 146N3650.SDR CALA0500404Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 1640, RBL 57. THE CORROSION WAS BLENDED OUT AND REPAIRED IAW ECRA 5321-01316.SDR CALA0500143Floor Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 720, RBL 44 TO RBL 48. REPAIRED IAW SRM 53-00-51, REPAIR 3.SDR CALA0500142Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 720, LBL 45.50 TO 51.50. REPAIRED IAW SRM 53-00-51, REPAIR 3.SDR CALA0200522SealNOISE FROM L1 DOOR. INSTALLED SEAL IN TRACK TOP FORWARD DOORSDR CALA0200502Slat · delaminatedINSPECTION FOUND #6 SLAT WEDGE SKIN DELAMINATED. THE #6 SLAT WAS REMOVED AND REPLACED IAW MM 27-81-01.SDR CALA0200497Fuse · blownTHE EMERGENCY ESCAPE PATH LIGHTING ON SEATS FROM ROW 15ABC TO 25ABC WERE FOUND INOPERATIVE. MAINTENANCE FOUND THAT THE LOAD FUSE HAD RUPTURED AT BATTERY PACK M10699. THE LOAD FUSE WAS REPLACED AND EMERGENCY ESCAPE PATH LIGHTING TEST WAS GOOD IAW MM 33-51-00.SDR CALA9901438Panel · crackedINSPECTION FOUND A 6 AND 7 INCH CRACK IN RT WING FIXED L/E PANEL AT WS 421-471. REPAIRED IAW ECRA 5720-01668. A DIP WAS INITIATED TO REINSPECT THE AREAS EVERY 1000 HOURS AND ACCOMPLISH A PERMANENT REPAIR WITHIN 18 MONTHS OR NEXT C-CHECK.SDR CALA9901437Panel · crackedINSPECTION FOUND A 10 AND 6 INCH CRACK IN LT WING FIXED LEADING EDGE PANEL AFT OF NR 4 L/E SLAT, WS 421-471. A FIBERGLASS REPAIR WAS INSTALLED IAW ECRA 5720-01668. A DIP WAS ISSUED TO ACCOMPLISH A PERMANENT REPAIR WITHIN 18 MONTHS OR NEXT C-CHECK.SDR CALA9901424Intercostal · corrodedINSPECTION FOUND INTERCOSTAL ON FLOOR STRUCTURE CORRODED AT BS 1620-1640. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW BOEING DRAWINGS 146N5300 AND 143N5554-6.SDR CALA9901423Seat Track · corrodedINSPECTION FOUND I/B SEAT TRACK CORRODED AT BS 377-400, LBL 25 AND O/B SEAT TRACK WAS CORRODED AT BS 377-440, LBL 45. THE SEAT TRACKS WERE REPLACED IAW SRM 53-10-00 AND BOEING DRAWING 141N5130.SDR CALA9901370Skin · dentedIMPACT DAMAGE (1)ON LEFT SIDE FUSELAGE STATION 610 BETWEEN STRINGERS 15 AND 16 LEFT. REPAIRED PER SRM 53-00-01 FIG 208.SDR CALA9801172Compressor · failedTHE NR 2 ENGINE EXPERIENCED COMPRESSOR STALL ACCOMPANIED BY HIGH EGT JUST AFTER TAKEOFF FROM LAS. THE AIRCRAFT WAS RETURNED TO LAS WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WILL BE REMOVED AND REPLACED. THE HIGH PRESSURE COMPRESSOR DAMAGE REPORTED DSDR CALA9701798Engine · failedTHE NR 2 ENGINE FAILED ON FINAL APPROACH TO LAX. THE ENGINE SHUT DOWN WITH NO FIRE WARNING. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED DUE TO SUBSEQUENT ENGINE PROBLEMS. REVEALED DURING ENGINE INSPECTION.SDR CALA9700354Transmission · inoperativeTHE TRAILING EDGE FLAP DISAGREE EICAS APPEARED WHILE GOING FROM UP TO FIVE DEGREES. THE FLAPS WERE LOWERED ALTERNATELY IAW THE TRAILING EDGE FLAP DISAGREE CHECKLIST AND A 20 DEGREE FLAP LANDING WAS MADE AT EWR. MAINTENANCE FOUND THE NR 8 FLAP TRANSMISSION TOSDR CALA9601381Brake · leakingTHE EICAS MESSAGE LEFT HYDRAULIC QUANTITY STATUS PAGE SHOWED .46RF DURING GEAR EXTENSION FOR LANDING. THE RIGHT HYDRAULIC QUANTITY LOW CAME ON SHOWING .73RF DURING TAXI IN. MAINTENANCE FOUND THE NR 8 BRAKE LEAKING. THE NR 8 BRAKE WAS REMOVED AND REPLACED.
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