N431US, cancelled Mar 7, 2013
Service difficulty reports · 38
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 = 'N431US' AND deregistration_id = 'N431US-2013-03-07' 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 = 'N431US' AND deregistration_id = 'N431US-2013-03-07' 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 USAA001982Frame · crackedCLT - FOUND CHORD CRACKED 1.5 INCH, STATION 178, WL 207, RT FUSELAGE CHORD. REPAIRED DOUBLER PER EA 68417. (M)SDR USAA001983Angle · crackedCLT - FOUND SUPPORT ANGLE CRACKED .5 INCH, STATION 301 FORWARD OF FORWARD ENTRY DOOR UPPER HINGE AREA. REPAIRED DOUBLER PER SRM 51-10-02. (M)SDR USAA001984Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 460, BETWEEN STRINGER 8 AND 9R. REPAIRED DOUBLER PER TR 53-10-14. (M)SDR USAA001985Doubler · crackedCLT - FOUND ANTENNA DOUBLER 5 INCH CRACK, STATION 727D PLUS 6 INCH BL 0. FABRICATED NEW BRACKET PER SRM 51-10-02. (M)SDR USAA001986Frame · crackedCLT - FOUND FRAME CRACKED, BS 867, BETWEEN STRINGER 8/9L. REMOVED AND FABRICATED DOUBLER PER TR 53-10-14. (M)SDR USAASB00332Slat · lack of lubeIAD - FLT 1827 - CLIMBING OUT OF PHL THROUGH FL240, EN ROUTE TO CLT, THE NR 4 LEADING EDGE SLAT INTRANSIT LIGHT ILLUMINATED ON FORWARD AND OVERHEAD PANELS ALONG WITH A VIBRATION. CREW DESCENDED AND FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES. AT FL200, CREWSDR USAA001928Frame · crackedCLT - FOUND CHORD CRACKED 1.5 INCHES, STATION 178, WL 207, LT CHORD SIDE SKIN. REPAIRED DOUBLER PER EA 68426. (M)SDR USAA001929Bulkhead · crackedCLT - FOUND SKIN CRACKED 1 INCH IN TWO PLACES, BS 178, LBL 5.5, WL 201, 198 BBL 0, WL 190. DOUBLER REPLACED PER EA 68454. (M)SDR USAA001937Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 907, BETWEEN STRINGER 8 AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA001930Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 380, BETWEEN STRINGER 8 AND 9 R. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA001931Frame · crackedCLT - FOUND FRAME CRACKED BS 400, BETWEEN STRINGER 8 AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA001932Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, BS 747, BETWEEN STRINGER 8/9R. REMOVED DAMAGED AND FABRICATED DOUBLER PER TR 53-10-14. (M)SDR USAA001933Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, BS 827, BETWEEN STRINGER 8/9R. INSTALLED OUTSIDE REPAIR DOUBLER PER TR 53-10-14. (M)SDR USAA001934Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 827, BETWEEN STRINGER 8 AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA001935Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 867, BETWEEN STRINGER 8/9R. REPAIRED DOUBLER PER TR 53-10-14. (M)SDR USAA001936Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 907, BETWEEN STRINGER 8/9R. REPAIRED DOUBLER PER TR 53-10-14. (M)SDR USAA001918Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, STATION 986.5, LBL 7 - LBL 31. CORROSION LEVEL 1 C 53-107-02. REMOVED AND REPLACED T-CAP PER TR 53-60-01. (M)SDR USAA001919Channel · corrodedCLT - FOUND Z-CHANNEL CORRODED 1 INCH BY 2 INCH, LEFT AFT DOOR SILL. CORROSION LEVEL 1 C 53-107-02. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-02. (M)SDR USAA001909Seat Track · corrodedCLT - FOUND SEAT TRACK CORRODED .5 INCH BY .5 INCH BY .100 INCH DEEP, SEAT TRACK STATION 328-360, RBL 24. FABRICATED SEAT TRACK SECTION PER SRM 53-00-52 PAGE 202. (M)SDR USAA001882Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 727D BETWEEN STRINGER 8 AND 9R. FABRICATED NEW FRAME DOUBLER PER TR 53-10-14. (M)SDR USAA001883Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 3 INCHES, BL 0 STATION 312 CABIN FLOORBEAM LBL 18 - RBL 18. INSTALLED SPLICE ANGLES EPR SRM 52-10-51. (M)SDR USAA001884Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .5 INCH BY 1 INCH, STATION 947 FROM LBL 12 THROUGH RBL 12 TOP SURFACE. INSTALLED NEW SECTION PER TR 53-60-02 REV A. (M)SDR USAA001885Floor Support · corrodedCLT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH, BETWEEN FLOORBEAM 947 AND 967 AT RBL 16. INSTALLED NEW PART PER SRM 51-10-2. (M)SDR USAA001872Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 747 BETWEEN STRINGER 8 AND 9L. DRILLED OUT DAMAGE AND FABRICATED DOUBLER PER TR 53-10-14. (M)SDR USAA001875Floorbeam · corrodedCLT - FOUND FLOORBEAM 2 INCH BY 3 INCH, STATION 328, BL 0 CABIN FLOORBEAM. CORROSION LEVEL 1. INSTALLED NEW T-CAP PER SRM 53-10-51 FIG 205. (M)SDR USAA001873Frame · crackedCLT - FOUND FRAME CRACKED .75 INCH, BS 787, BETWEEN STRINGER 8 AND 9L. DRILLED OUT DAMAGE AND FABRICATED DOUBLER PER TR 53-10-14. (M)SDR USAA001874Frame · crackedCLT - FOUND FRAME CRACKED .250 INCH, BS 727F BETWEEN STRINGER 8 AND 9L. FABRICATED DOUBLER DRILLED OUT DAMAGE PER TR 53-10-14. (M)SDR USAASB99186Warning · activatedDCA - FLT 8027 - AFTER TAKEOFF, THE FORWARD ENTRY DOOR WARNING LIGHT ILLUMINATED. FLIGHT RETURNED TO FIELD AT DCA AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. (M)SDR USAASB98231Gcu · failedRIC - FLT 811 - AFTER LEVEL OFF AT APPROXIMATELY FL 280, THE FLIGHT ATTENDANTS REPORTED AN UNUSUAL ODOR IN THE CABIN. SHORTLY THEREAFTER, ODOR WAS NOTICED IN THE COCKPIT. CREW DECLARED AN EMERGENCY AND DIVERTED TO RIC. FLIGHT LANDED WITHOUT INCIDENT AND TAXSDR USAASB96202Bleed Air Reg · failedPHX - FL 152 - AIRCRAFT WAS CLIMBING THROUGH 8,000 FEET WHEN THE FLIGHT EXPERIENCED NR 1 ENGINE BLEED VALVE FAILURE. CREW RECEIVED NO INDICATIONS BY WAY OF WARNING LIGHTS. CAPTAIN WENT THROUGH CHECKS AND PROCEDURES WITH NO HELP TO CORRECT THE PROBLEM. CAPTISDR USAA960497Skin · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK LOWER AFT CORNER OF PYLON SKIN ACCESS OPENING STRINGER 727 L. CUT OUT CRACK, INSTALLED FILLER AND DOUBLER. REPAIRED PER EA 41241. (M)SDR USAA960496Floor Beam · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER AREAS OF CORROSION STATION 328 FLOOR BEAM UPPER CHORD AT NUT PLATE HOLES RBL 13 TO RBL 58. CUT OUT DAMAGED CHORD AND SPLICED IN NEW SECTION PER TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSISDR USAA960495Floor Beam · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 344 LBL 21 THROUGH RBL 9. INSTALLED NEW SECTION OF T-CAP, REPAIRED PER TR 53-10-03. (M)SDR USAA960494Floor Beam · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 312 RBL 8 THROUGH LBL 8. INSTALLED NEW SECTION OF UPPER CHORD, REPAIRED PER SRM 53-10-51 FIG 205. (M)SDR USAA960493Frame · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH CORRSION AT FRAME AROUND AFT CARGO DOOR CUT OUT BS 787 PLUS 8 INCHES, STRINGER 25R. CUT OUT SECTION OF FRAME AND INSTALLED REPAIR. REPAIRED PER SRM 53-00-07 FIG 201. (M)SDR USAA960492Floor Beam · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 26 INCH CORROSION, STATION 947 FLOOR BEAM RBL 13 INCHES TO LBL 13 INCHES, WL 208. FABRICATED PER EA 41220. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)SDR USAA960491Floor Beam · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER AREAS OF CORROSION STATION 986.5 FLOOR BEAM UPPER CHORD LBL 45 TO RBL 45, WL 208. REPAIRED PER EA 41219. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)SDR USAA950158Cargo Strap · jammedMIA - FLT 2240 - AFT CARGO DOOR LIGHT ILLUMINATED ON TAKEOFF. FLIGHT RETURNED TO MIA WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND CARGO STRAP WEDGED BETWEEN ROLLER AND CAM. REMOVED STRAP AND CHECKED OPERATION OF DOOR WARNING SYSTEM. OPS CH
Back to N431US, cancelled Mar 7, 2013