N260AU, cancelled Aug 16, 2004
Service difficulty reports · 93
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 = 'N260AU' AND deregistration_id = 'N260AU-2004-08-16' 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 = 'N260AU' AND deregistration_id = 'N260AU-2004-08-16' 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 USAASB01242Slide · inoperativeBOS - THE AFT RIGHT SERVICE DOOR EVACUATION SLIDE FAILED TO REMAIN INFLATED DURING TEST. MAINTENANCE REPLACED THE EVACUATION SLIDE. (M)SDR USAASB00208Light · failedPVD - MAINTENANCE FOUND THE FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)SDR USAASB00188Line · leakingMCO - FLT 2670 - UPON APPROACH INTO MCO, AFTER SETTING FLAPS, FLIGHT ENCOUNTERED SYSTEM A HYDRAULIC FLUID LOSS. BOTH A PUMP LOW PRESSURE LIGHTS ILLUMINATED. CREW ACCOMPLISHED ALTERNATE FLAP EXTENSION AND MANUAL GEAR EXTENSION. FLIGHT LANDED WITHOUT FURTHER SDR USAA000292Stringer · corrodedCLT - FOUND 3 INCH BY 1 INCH OF CORROSION AT BS 980 TO 988, STRINGER 27L. INSTALLED NEW STRINGER PIECE PLU SPLICE PER SRM 53-10-3 FIG 1. CORROSION LEVEL 1. (M)SDR USAA000287Bracket · corrodedCLT - CORROSION LEVEL 1, ANTENNA BRACKET CORRODED BETWEEN BS 500 AND 500B STRINGER 28L AND 28R. INSTALLED NEW PARTS PER SRM 51-10-01. (M)SDR USAA000288Frame · crackedCLT - FRAME CRACKED AT BS 663.75 STRINGER 3L. INSTALLED DOUBLER PER SRM 53-10-4 FIG 14. (M)SDR USAA000289Frame · crackedCLT - FRAME CRACKED AT BS 663.75, STRINGER 2L. INSTALLED DOUBLER PER SRM 53-10-4 FIG 14. (M)SDR USAA000290Frame · crackedFRAME CRACKED AT 663.75 STRINGER 2R. INSTALLED DOUBLER PER SRM 53-10-4 FIG 14. (M)SDR USAASB00056Packing · failedCLT - FLT 7900 - WHILE ON TEST HOP, APPROACHING CLT, THE A HYDRAULIC SYSTEM LIGHT BEGAN FLICKERING. CAPTAIN SHUT DOWN PUMPS AND STARTED GETTING THE B HYDRAULIC SYSTEM LIGHT FLICKERING. CAPTAIN DECLARED AN EMERGENCY AND LANDED AT CLT WITHOUT FURTHER INCIDENT.SDR USAA000275Floorbeam · crackedCLT - FOUND CRACK IN T-CAP, 2 INCHES, BL 0 AT STATION 663. INSTALLED REPAIR STRAPS AND ANGLES PER TR 57-10-04. (M)SDR USAA000276Web · crackedCLT - FOUND 4 CRACKS, .5 INCH, LBL 25, STATION 710 TO 714. INSTALLED DOUBLER PER EA 66602. (M)SDR USAA000277Tie Clip · crackedCLT - FOUND CRACK TIE CLIP .25 INCH, STATION 578, STRINGER 5L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)SDR USAA000278Frame · crackedCLT - FOUND 2 INCH CHORD ANGLE CRACK, STATION 1138, STRINGER 5AL. INSTALLED CHORD SECTION AND DOUBLER PER SRM 51-40-3 FIG 1. (M)SDR USAA000279Stringer · corrodedCLT - FOUND CORROSION LEVEL 1, 6 INCHES, STATION 1006 STRINGER 24L. INSTALLED NEW PART PER SRM 51-10-1 FIG 1. (M)SDR USAA000280Fitting · corrodedCLT - FOUND CORROSION LEVEL 1, .5 INCH, INBOARD STAB FITTING ON GEAR BEAM INSIDE FLANGES. INSTALLED NEW PART PER SRM 20-10-19. (M)SDR USAA000281Frame · corrodedCLT - FOUND CORROSION LEVEL 1, 1 INCH BY 2 INCH, STATION 500B ABOVE STRINGER 26R UNDER TRANSITION PANEL AND FRAME. INSTALLED REPAIR DOUBLER PER SRM 53-10-4. (M)SDR USAA000260Bulkhead · crackedBULKHEAD HAS A .25 INCH CRACK AT BS 663, LBL 25. SPLICED IN DOUBLER PER EA 66610 AND SB 737-53-1184. (M)SDR USAA000256Web · crackedCLT - FOUND WEB CRACKED 1 INCH, BS 950, STRINGER 10R. INSTALLED FILLER AND DOUBLER PER TR 53-30-07. (M)SDR USAA000229Skin · crackedCLT - SKIN AT BS 947 BETWEEN STRINGER 11R AND 12R HAS A .125 INCH CRACK. INSTALLED DOUBLER PER SRM 53-30-3. (M)SDR USAA000230Stringer Clip · crackedCLT - STRINGER CLIP CRACKED AT BS 727B STRINGER 7L. REPLACED TIE CLIP PER SRM 51-10-1. (M)SDR USAA000231Channel · crackedCLT - CHANNEL HAS A 2 INCH CRACK AT BS 520 RBL 25 WL 206. INSTALLED PIVOT LINK PER SB 737-53-1120. (M)SDR USAA000244Angle · crackedCLT - ANGLE CRACKED AT STATION 1138 ON HORIZ STABILIZER. REPAIRED PER SRM 51-40-3 FIG 1. (M)SDR USAA000206Stiffener · crackedCLT - FOUND CRACK IN STIFFENER 1.75 INCHES, STATION 178, LBL 5.5 LOWER AFT SIDE VERTICAL STIFFENER. INSTALLED DOUBLER PER TR 53-10-17 AND SRM 20-40-04. (M)SDR USAA0209Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 706, STRINGER 10L TIE CLIP. INSTALLED CLIP PER EO5393G227. (M)SDR USAA0210Web · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .750 INCH LONG CRACK AT BS 707 TO 710, RBL 25 WEB. INSTALLED DOUBLER PER EA 66602. (M)SDR USAA0211Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 616, STRINGER 5R CLIP. REPAIRED PER EO 5393G227. (M)SDR USAA0212Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 727B, STRINGER 2L TIE CLIP. REPLACED TIE CLIP PER EO 5393G227. (M)SDR USAA0213Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 747, STRINGER 4R TIE CLIP. REPLACED TIE CLIP PER EO 5393G227. (M)SDR USAA0214Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 807, STRINGER 11R TIE CLIP. REPLACED TIE CLIP PER EO 5393G227. (M)SDR USAA0215Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 578, STRINGER 5L TIE CLIP. REPAIRED PER EO 5393G227. (M)SDR USAA0216Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 639, STRINGER 4L TIE CLIP. REPAIRED PER EO 5393G227. (M)SDR USAA0217Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 578, STRINGER 5L TIE CLIP. REPAIRED PER EO 5393G227. (M)SDR USAA0218Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT STATION 344, LBL 9 FLOORBEAM. CORROSION LEVEL 1. INSTALLED FILLER AND REPAIR ANGLE PER SRM 53-10-9. (M)SDR USAA0219Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND SCREW HOLES STATION 947.5 FROM LBL 17 - RBL 17 FLOORBEAM. CORROSION LEVEL 1. INSTALLED NEW T-CAP PER SRM 53-10-9, TR 53-10-05A, AND EA 66592. (M)SDR USAA0220Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION STATION 312, LBL 11 AND BL 0 FLOORBEAM T-CAP. CORROSION LEVEL 2. REPLACED T-CAP PER SRM 53-10-0 FIG 5 AND IAW 51-10-9 FIG 5. (M)SDR USAA0221Frame · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AREA OF CORROSION STATION 500B ABOVE STRINGER 26R FRAME. CORROSION LEVEL 1. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-4. (M)SDR USAA0222Beam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 2 INCH AREA OF CORROSION BS 234, WL 190, RBL 6 ON NG TRAVERSE BEAM. CORROSION LEVEL 2. TASK NR C53-202-01. REPLACED PART PER SRM 51-10-1. (M)SDR USAA0223Stringer · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AREA OF CORROSION STATION 1006, STRINGER 24R. CORROSION LEVEL 2. TASK NR C53-202-01. REPLACED PART PER SRM 51-10-1. (M)SDR USAA0224Angle · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 40 INCH AREA OF CORROSION STATION 957-1006, RBL 54 FLOOR LEVEL Z-ANGLE. CORROSION LEVEL 1. TASK NR C553-107-02. REPLACED PART PER BOEING DWG 65-45855 AND SRM 51-10-1. (M)SDR USAA0225Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 46 INCH AREA OF CORROSION FLOORBEAM 986.5 BETWEEN BBL 0 - RBL 46. CORROSION LEVEL 1. TASK NR C53-107-02. REPLACED T-CAP PER TR 53-60-01 REV A. (M)SDR USAA0226Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION FLOORBEAM 986.5 LBL 17. CORROSION LEVEL 1. TASK NR C53-107-02. REPLACED T-CAP PER TR 53-60-01 REV A. (M)SDR USAA0227Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND PATCHES OF CORROSION WITHIN 34 INCHES STATION 986.5 BETWEEN LBL 17 AND RBL 17 FLOORBEAM. CORROSION LEVEL 1. TASK NR C53-107-02. REPLACED T-CAP PER TR 53-60-01 REV A. (M)SDR USAA0228Angle · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 24 INCH AREA OF CORROSION LEFT AFT ENTRY Z-ANGLE. CORROSION LEVEL 1. TASK NR C53-107-02. FAB REPAIR DOUBLERS AND FILLER PER SRM 51-40-03 FIG 1. (M)SDR USAA0208Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727B, STR 5L TIE CLIP. REMOVED AND REPLACED CLIP PER EO 5393G227. (M)SDR USAA000200Skin · crackedCLT - FOUND LOWER FORWARD CORNER OF AFT SERVICE DOOR CUTOUT SKIN HAS A 2 INCH CRACK. INSTALLED REPAIR PLATES PER SRM 53-30-3. (M)SDR USAA000201Stringer Clip · crackedCLT - STRINGER CLIP HAS A .25 INCH CRACK AT BS 727B STRINGER 7L. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-00. (M)SDR USAA000202Stringer · crackedCLT - STRINGER 18A HAS A 1.5 INCH CRACK AT BS 727. REPAIRED PER SRM 51-10-01. (M)SDR USAA0203Gusset · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK IN RADIUS OF GUSSET AT BS 259, BBL 0, WL 193 TOP OF NG W/W. REPLACED GUSSET PER SRM 51-10-01. (M)SDR USAA0204Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 727A STRINGER 5L TIE CLIP. REMOVED AND REPLACED CLIP PER EO 5393G227. (M)SDR USAA0205Floorbeam · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SIX .5 INCH CRACKS BL 0 LONGITUDINAL FLOORBEAM WEB LOWER FASTENERS STATION 707 TO 715. REPAIRED NEW SECTION PER TR 57-10-05. (M)
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