N282AU, cancelled Sep 10, 2002
Service difficulty reports · 56
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 = 'N282AU' AND deregistration_id = 'N282AU-2002-09-10' 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 = 'N282AU' AND deregistration_id = 'N282AU-2002-09-10' 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 USAASB01322Battery · dischargedTPA - THE EMERGENCY EXIT LIGHT ABOVE THE FORWARD ENTRY DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)SDR USAASB01312Battery · dischargedLGA - MAINTENANCE FOUND THE FORWARD SERVICE DOOR AND FORWARD ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES. OPERATIONAL CHECK GOOD. (M)SDR USAA010780Splice · corrodedCLT - FOUND STRINGER SPLICE CORRODED 1 INCH BY 4 INCHES, BS 986.5, STRINGER 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM 53-10-3 FIG 1. (M)SDR USAA010797Support Fitting · corrodedPIT - FOUND SUPPORT FITTING CORRODED .020 INCH - .010 INCH, NOSE GEAR RIGHT TRUNNION SUPPORT FITTING BORE. REAMED BORE, INSTALLED SLEEVE PER EA 71444. (M)SDR USAASB00296Duct · crackedTPA-LGA - FLT 2676 - AFTER TAKEOFF, THE RIGHT ENGINE START VALVE LIGHT AND THE RIGHT ENGINE OVERHEAT LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. 15 MINUTES SINGLE ENGINE TIME. MAINTENANCE FSDR USAASB00284Actuator · leakingEWR - FLT 2636 - EN ROUTE FROM PBI TO LGA, CAPTAIN NOTICED THAT SYSTEM A HYDRAULIC QUANTITY HAD DECREASED FROM 2.2 GALLONS TO 1.2 GALLONS. ON DESCENT TO LGA, AS AIRCRAFT SLOWED AND FLAPS WERE EXTENDED, HYDRAULIC QUANTITY WENT TO .5 GALLONS. CREW WAS ABLE TO SDR USAA001316Stringer · crackedCLT - FOUND SHELF CRACKED .5 INCH, STRINGER 18A RIGHT, BS 727 SHELF. REPLACED WITH NEW SHELF PER SRM 51-10-02. (M)SDR USAA001318Pressure Panel · crackedCLT - FOUND PRESSURE DECK WEB CRACKED .5 INCH, STATION 670, RBL 12. INSTALLED FILLER AND DOUBLER PER EA 67747. (M)SDR USAA001317Stringer · crackedCLT - FOUND SHELF CRACKED .5 INCH, STRINGER 18A LEFT, BS 727 SHELF. REPLACED WITH NEW SHELF PER SRM 51-10-1. (M)SDR USAA001299Clevis · corrodedCLT - FOUND CLEVIS CORRODED .008 INCH BY .008 INCH, VERT FIN, AFT SPAR, AFT OUTBOARD CLEVIS RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M)SDR USAA001298Clevis · corrodedCLT - FOUND CLEVIS CORRODED .008 INCH BY .008 INCH, VERT FIN, FWD SPAR, FRONT CLEVIS, RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M)SDR USAA001297Clevis · corrodedCLT - FOUND CLEVIS CORRODED .008 INCH BY .008 INCH, VERT FIN, FWD SPAR, AFT CLEVIS RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M)SDR USAA001296Clevis · corrodedCLT - FOUND AFT SPAR CLEVIS CORRODED .013 INCH BY .028 INCH, VERT FIN, AFT SAPR, AFT OUTBOARD CLEVIS, RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M)SDR USAA001281Skin · crackedCLT - FOUND SKIN CRACKED .250 INCH, AFT SERVICE DOOR LOWER HINGE. INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-03 AND EA 67849. (M)SDR USAA001254Gusset · crackedCLT - FOUND GUSSETT CRACKED .5 INCH, NLG ACTUATOR ATTACH BEAM GUSSETT, STATION 259.5, BL 0. INSTALLED NEW PART PER SRM 51-30-00. (M)SDR USAA001236Torque Box · crackedCLT - FOUND TORQUE BOX CRACKED .25 INCH, STATION 1112, LEFT SIDE JUST BELOW UPPER TORQUE BOX. INSTALLED DOUBLER AND FILLER PER EA 67773 AND SRM 51-40-3. (M)SDR USAA001237Strap · crackedCLT - FOUND STRINGER STRAP CRACKED .75 INCHES LONG, 2 INCHES AFT OF STATION 1138, RT SIDE. INSTALLED REPAIR PER EA 67733, AND SRM 53-00-01 FIG 221. (M)SDR USAA001207Clip · crackedCLT - FOUND ATTACH CLIP CRACKED .5 INCH, STATION 380, STRINGER 26L ON BAFFLE ATTACH CLIP. REPLACED PER SRM 51-10-01. (M)SDR USAA001206Shim · crackedCLT - FOUND SHIM CRACKED .25 INCH, STATION 440 BETWEEN STRINGER 22R AND STRINGER 23R. REPLACED ATTACH CLIP SHIM PER SRM 51-10-01. (M)SDR USAA001157Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 440, STRINGER 22R. REMOVED AND REPLACED ANGLE PER SRM 51-10-1. (M)SDR USAA001149Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 2 INCHES, BS 663, BL 0. INSTALLED STIFFENER FILLER AND DOUBLER PER EA 67727. (M)SDR USAA001141Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, BS 907, STRINGER 21R FUSELAGE FRAME UPPER LEG. INSTALLED DOUBLER PER SRM 51-40-3. (M)SDR USAA001140Skin · crackedCLT - FOUND SKIN CRACKED 3 INCHES, BS 328 AFT LOWER CORNER FS 0 CUTOUT. INSTALLED DOUBLER PER TR 53-10-19A. (M)SDR USAA001139Stringer Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED .5 INCH, STRINGER 13 STATION 1138. INSTALLED NEW TIE CLIP PER SRM 51-10-01. (M)SDR USAA001112Frame · crackedCLT - FOUND 1 INCH CRACK, STATION 951 FRAME WL 254 RT SIDE. FABRICATED REPAIR AND INSTALLED PER TR 53-30-07A. (M)SDR USAA001111Frame · crackedCLT - FOUND 1 INCH CRACK, STATION 951 FRAME, WL 254 LT SIDE. FABRICATED AND INSTALLED REPAIR PER TR 53-30-07A. (M)SDR USAA001110Cap · corrodedCLT - FOUND T-CAP CORRODED 2 INCHES, FS 312, RBL 35. CUTOUT DAMAGED FABRICATED REPAIR AND INSTALLED PER 53-10-9 FIG 5. (M)SDR USAA001109Clip · crackedCLT - FOUND CLIP CRACKED .125 INCH, STATION 727B, STRINGER 3. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)SDR USAA001108Clip · crackedCLT - FOUND CLIP CRACKED .125 INCH, STATION 685, STRINGER 4. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)SDR USAA001107Clip · crackedCLT - FOUND CLIP CRACKED .250 INCH, STATION 685, STRINGER 3. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)SDR USAA001106Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, FS 663, STRINGER 10L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)SDR USAA001105Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 616, STRINGER 3R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)SDR USAA001104Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, FRAME 597 AT STRINGER 8L TIE CLIP. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)SDR USAA001066Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, FS 727B, STRINGER 5L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)SDR USAA001065Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 727A, STRINGER 4L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)SDR USAA001064Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, FS 727A, STRINGER 4L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)SDR USAA001063Clip · crackedCLT - FOUND CLIP CRACKED .125 INCH, STATION 685, STRINGER 2. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)SDR USAA001062Tie Clip · crackedCLT - TIE CLIP CRACKED .125 INCH, STRINGER 9L, AT FRAME 597. INSTALLED STRINGER TIE CLIP PER EO 5393G227. (M)SDR USAA000803Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .250 INCH BY .250 INCH, BS 312, RBL 11-36. INSTALLED NEW T-CAP PER SRM 53-10-9. INSTALLED NEW T-CAP PER SRM 53-10-9. (M)SDR USAASB99052Pcu · malfunctionedBWI - FLT 2710 - EN ROUTE FROM MCO-BDL, AT FL330 AND .74 MACH, FLIGHT WAS APPROACH SBY ON 'A' AUTOPILOT WHEN THE A/C STARTED PITCHING UP AND ROLLING TO RIGHT 80 DEGRES. CAPT USED FULL POWER AND FULL AILERON TO GET THE AIRCRAFT LEVEL. CAPT STATED THAT WHEN HESDR USAASB98309Mechanism · out of adjustBWI - FLT 2608 - FLIGHT WAS CLEARED FOR APPROACH AT BWI FOR RUNWAY 28. AS CAPTAIN SELECTED FLAPS 1, THE LEADING EDGE TRANSIT LIGHT AND THE NR 4 SLAT TRANSIT LIGHT ON THE OVERHEAD PANEL ILLUMINATED. CREW RECYCLED THE FLAPS AND DISCONTINUED THE APPROACH. CREWSDR USAA980176Stringer · corrosionROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 1.333 INCH BY 2.5 INCH CORROSION BS 967 STRINGER 25 LEFT. REMOVED CORROSION AND INSTALLED STRINGER SPLICE. REPAIRED PER SRM 53-10-3 FIG 9. (M)SDR USAASB98055Light · failedCLT - MAINTENANCE FOUND THE EMERGENCY LIGHT OVER THE FORWARD SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD. (M)SDR USAASB97332Battery Pack · dischargedCLT - MAINTENANCE FOUND THE AFT LEFT AND RIGHT EXTERIOR EMERGENCY ESCAPE SLIDE LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)SDR USAASB97073Garlock Seal · leakingBWI - FL 8028 - ON CLIMB-OUT OF BWI, AT FL 250, CAPTAIN SHUT DOWN THE NR 1 ENGINE DUE TO LOW OIL PRESSURE LIGHT ILLUMINATING WHICH WAS VERIFIED BY OIL PRESSURE GAUGE AND LOSS OF OIL QUANTITY. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD AT BWI ASDR USAA960918Beam · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACKED BEAM RBL 24.5 BS 674. INSTALLED STIFFENER AND NEW CHANNEL, REPAIRED PER EO 5791G632. (M)SDR USAA960622Floor Beam · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 20 INCH AREA OF HEAVY SURFACE CORROSION FLOOR BEAM STATION 360, RBL 12 TO RBL 56. INSTALLED REPAIR ANGLES, REPAIRED PER TR 53-10-05 C. CORROSION TASK NR C53-107-01, CORROSION LEVEL 1. (SDR USAA960621Web · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO .5 INCH CRACKED WEBS RBL 24.5 BS 707. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2, FIG 1. (M)SDR USAA960620Web · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND THREE .25 INCH CRACKED WEBS LBL 24.5 BS 707. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2 FIG 1. (M)SDR USAA960619Web · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND FOUR .5 INCH CRACKED WEBS BL 0 BS 707. INSTALLED WEB REPAIR AND FILLERS. REPAIRED PER SRM 51-40-2. (M)
Back to N282AU, cancelled Sep 10, 2002