N534AU, cancelled Apr 25, 2003
Service difficulty reports · 27
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 = 'N534AU' AND deregistration_id = 'N534AU-2003-04-25' 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 = 'N534AU' AND deregistration_id = 'N534AU-2003-04-25' 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 USA2002F00043Seal · tornENROUTE, THE AIRCRAFT LOST CABIN PRESSURIZATION AS MASTER CAUTION WARNING LIGHT ILLUMINATED. AUTO, STANDBY AND MANUAL PRESSURIZATION MODES WOULD NOT STOP CABIN FROM CLIMBING. CREW DONNED OXYGEN MASKS, ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND DECESDR USAA980418Frame · dentedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH DENT STATION 747 AND STRINGER 24L, 727E AND STRINGER 25L AND 767 AND STRINGER 21L FRAME. INSTALLED REPAIR ANGLES STATION 727E, STATION 747 STRINGER 24L AND STATION 767 STRINGER 21L PER EA 6239SDR USAA980417Skin · damagedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH HOLE IN FORWARD FUSELAGE STATION 189, 2 FT FORWARD AND 1 FT DOWN FROM 1ST OFFICERS WINDOW ON SKIN. REPAIRED EXISTING INTERMI REPAIR TO PERMANENT REV A PER EA 58180A. (M)SDR USAA980416Housing · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AFT INBOARD FLANGE OF UPPER HINGE HOUSING FOR FORWARD SERVICE DOOR FRAME 294.5. INSTALLED DOUBLER PER TR 53-10-11. (M)SDR USAA980391Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION STATION 1006 LBL 2 BEAM INST PASS FLOOR. CORROSION TASK NR C53-107-02. INSTALLED REPAIR ANGLES PER SRM 53-30-51. (M)SDR USAA980388Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH BY 14 INCH AREA OF CORROSION STATION 328 LBL 51 TO RBL 65 FLOORBEAM UPPER CHORD. CORROSION TASK NR C63-107-02. SPLICED IN NEW T-CAP SECTION PER SRM 53-10-51. (M)SDR USAA980387Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH BY 50 INCH AREA OF CORROSION STATION 344 BLO TO LBL 50 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. SPLICED IN NEW T-CAP SECTION PER SRM 53-10-51. (M)SDR USAA980386Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH BY 72 INCH AREA OF CORROSION CLIPNUT HOLES STATION 312 LBL 36 TO RBL 36 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. SPLICED IN NEW T-CAP SECTION PER SRM 53-10-51. (M)SDR USAA980385Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH BY 10 INCH AREA OF CORROSION STATION 967 LBL 5 TO RBL 5 FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED REPAIR ANGLES PER SRM 53-30-51. (M)SDR USAASB98121Battery · dischargedIND - MAINTENANCE FOUND THE FORWARD CABIN EMERGENCY EXIT SIGNS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY IN CHARGER UNIT. OPS CHECK GOOD. (M)SDR USAA950406Adc · failedCLT - FLT 1157 - CAPTAIN'S FLIGHT INSTRUMENTS, AIRSPEED, ALTIMETER FAILED AND GPWS WARNING CAME ON. FLIGHT RETURNED TO CLT WHERE AN OVERWEIGHT LANDING WAS MADE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 ADC. OPS CHECK OK. PERFORMED OVERWEIGHT LANDSDR USAA950623Stringer · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STRINGER 16L BS 500 C PLUS 4 INCHES. REPAIRED PER EO 5393X228. (M)SDR USAA950253Stringer · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK IN STRINGER S-16 R BS 500 C PLUS 4 INCHES. REPAIRED PER EO 5393X228. (W)SDR USAA950268Floor Beam · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 60 INCH STATION 986.5 ENTIRE LENGTH. REPAIRED PER TR 53-10-5. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W)SDR USAA950263Floor Beam · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FLOOR BEAM CORRODED 2 INCH BY 72 INCH AREA (CLIP NUT HOLES) BS 328. REPAIRED PER SRM 51-70-12 AND TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W)SDR USAA950275Intercostal · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FOUR .5 INCH BY 1 INCH CORRODED AREA (ABOUT .050 INCH DEEP), BS 312-328 RBBL 12 (CABIN FLOOR SUPPORT). REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W)SDR USAA950274Angle · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND ANGLE CORROSION AT CLIP NUT HOLES BS 320-344 LBBL 12. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W)SDR USAA950273Angle · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 20 INCH BY 1 INCH BY 6 INCH EQUALS 1 INCH BY 36 T, BS 277-BS 328 FORWARD SERVICE DOOR ANGLE. REPAIRED PER SRM 51-10-4. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)SDR USAA950272Angle · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND ANGLE CORROSION 1 INCH BY 15 INCH AND 1 INCH BY 3 INCH FOR TOTAL OF 1 INCH BY 18 INCH, BS 300 THROUGH BS 344 AT FORWARD CABIN (LEFT SIDE) ENTRY DOOR. REPAIRED PER SRM 51-10-4. CORROSION TASK NR C53-107-02. CORSDR USAA950271Angle · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AT CLIP NUT HOLES, BS 312-328 LBBL 12. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)SDR USAA950270Intercostal · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 .5 INCH BY 1 INCH CORRODED AREAS (ABOUT .050 INCH DEEP), BS 328-344 RBBL 12 (CABIN FLOOR SUPPORT). REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W)SDR USAA950264Floor Beam · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FLOOR BEAM CORROSION AT CHIP NUT HOLES BS 312 RBBL 24 TO LBBL 30. REPAIRED PER TR 53-10-03. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)SDR USAA950269Floor Beam · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FLOOR BEAM (2) 1 INCH BY 1 INCH CORRODED AREAS (ABOUT .060 INCH DEEP), LBL 6 AND RBL 6 AT BS 947. REPAIRED PER SRM 53-00-51 FIG 202. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)SDR USAA950267Seat Track · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND SEAT TRACK 2 INCH BY 12 INCH CORRODED AREA BS 277-294 RBL 24 INBOARD SIDE OF NR 1 GALLEY. REPAIRED PER SRM 53-00-52 FIG 202. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)SDR USAA950266Seat Track · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND SEAT TRACK 2 INCH BY 24 INCH CORRODED AREA BS 340-364 RBL 24. REPAIRED PER SRM 53-00-52 FIG 201. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)SDR USAA950265Seat Track · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION ,FOUND SEAT TRACK 1 INCH BY 8 INCH CORRODED AREA BS 340 RBL 44. REPAIRED PER SRM 52-00-52 FIG 201. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)SDR USAA950276Angle · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND ANGLE CORRODED SEVERAL NUT PLATES BS 947 BS 1006. REPAIRED PER SRM 51-10-02 PG 16. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W)
Back to N534AU, cancelled Apr 25, 2003