N268AU, cancelled Dec 9, 2003
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 = 'N268AU' AND deregistration_id = 'N268AU-2003-12-09' 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 = 'N268AU' AND deregistration_id = 'N268AU-2003-12-09' 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 USAASB01321Wire · brokenPVD - THE EMERGENCY LIGHT AT SEAT 12 WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. (M)SDR USAA010622Skin · crackedCLT - FOUND FUSELAGE SKIN HAS APPROXIMATELY .5 INCH CRACK, BS 380, FUSELAGE BELLY S-28L, COOLING DUCT CUTOUT. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-30-04. (M)SDR USAASB0279Fuel Control · failedBWI - FLT 2797 - ON CLIMB-OUT FROM BWI, AT FL080, THE NR 2 ENGINE FLAMED OUT. N1, N2 AND OIL PRESSURE WAS PRESENT. CREW TRIED TO RESTART/RELIGHT NR 2 ENGINE, BUT COULD NOT. AN EMERGENCY WAS DECLARED AND THE PASSENGERS WRE BRIEFED ON EMERGENCY PROCEDURES. FSDR USAA001138Frame · corrodedTPA - FOUND FRAME WEB CORRODED 4 INCHES BY 3 INCHES, FRAME STATION 277, LT LOWER LOBE. REPLACED SECTION PER SRM 51-40-2 FIG 1, SRM 53-10-4 FIG 9A EA 66638. (M)SDR USAASB00190Structure · vibrationPVD - FLT 2851 - ON CLIMB-OUT FROM BOS, AIRCRAFT EXPERIENCED A CONTINUOUS AIRFRAME VIBRATION OF UNKNOWN SOURCE. ATTEMPTS TO ISOLATE THE NATURE OF THE SOURCE WERE NO HELP. THE ONLY IMPROVEMENT WAS WHEN THE AIRCRAFT SLOWED TO 250 KNOTS. CAPTAIN THOUGHT OF DIVSDR USAASB00153Flap · jammedTPA - FLT 2797 - AS AIRCRAFT WAS BEING CONFIGURED FOR FINAL APPROACH TO TPA, THE RIGHT INBOARD TRAILING EDGE FLAP BECAME JAMMED WHEN THEY WERE MOVED FROM 10-15 DEGREES. CREW ACCOMPLISHED PROCEDURES AND A GO-AROUND AND DECLARED AN EMERGENCY. FLIGHT LANDED WITSDR USAASB00134Hose · failedIAD - FLT 2755 - DURING CLIMB-OUT FROM IAD, THE NOSE LANDING GEAR WOULD NOT RETRACT. CREW NOTICED A DROP IN HYDRAULIC PRESSURE. THE NOSE LANDING GEAR NEVER UNLOCKED AS A STEADY NOSE GEAR GREEN LIGHT REMAINED ILLUMINATED. FLIGHT RETURNED TO FIELD AT IAD AND SDR USAASB00131Start Valve · failedTPA - FLT 2999 - CLIMBING THROUGH 7,000 FEET OUT OF TPA, THE NR 1 ENGINE START VALVE LIGHT ILLUMINATED. CAPTAIN WENT THROUGH PROCEDURES, DECLARED AN EMEREGNCY AND SHUT DOWN THE NR 1 ENGINE PER PROCEDURES. FLIGHT RETURNED TO FIELD AT TPA AND LANDED WITHOUT FUSDR USAASB00121Actuator · failedATL - FLT 2967 - ON DESCENT INTO ATL, WHILE EXTENDING FLAPS, CAPTAIN VISUALLY CONFIRMED THE NR 1 SLAT WAS NOT FULLY EXTENDED. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND DECLARED AND EMERGENCY. FLIGHT LANDED WITHOUT INCIDENT AT ATL. MAINTENANCE RESDR USAASB99199Compressor · stalledBOS - FLT 2851 - AT ROTATION, CREW HEARD AND FELT A LOUD BANG. ALL ENGINE INDICATIONS WERE NORMAL. FLAMES OR A FLASH WERE LATER REPORTED BY A PASSENGER OFF THE RIGHT SIDE OF THE AIRCRAFT. AT APPROXIMATELY 5,000 FT. CAPTAIN DECLARED AN EMERGENCY AND PREPPEDSDR USAASB99150Wire Harness · failedRDU - FLT 2826 - EN ROUTE FROM MCO TO BOS, DURING CRUISE, CAPT REPORTED PROBLEMS WITH THE NR 2 FUEL GAUGE. GAUGE WAS UNRELIABLE WITH ITS READINGS AND THE NR 1 FUEL GAUGE WAS ALREADY ON MEL. CREW TRIED RESETTING CIRCUIT BREAKER WITH NO HELP. THE NR 2 FUEL GASDR USAASB98304Battery Pack · dischargedPHL - MAINTENANCE FOUND THE AFT CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)SDR USAA980554Skin · creasedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CREASE APU DOOR AFT LATCH CUTOUT AT STATION 1146 ON SKIN. INSTALLED DOUBLER PER EA 62761. (M)SDR USAA980553Skin · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AFT ENTRY DOORWAY AT LOWER HINGE CUTOUT ON FUSELAGE SKIN. INSTALLED REPAIR DOUBLER AND TRIPLER PER SRM 53-30-3 FIG 34 AND TR 53-30-11. (M)SDR USAA980552Stringer · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 6 INCH CORRODED AREA STATION 907, STRINGER 26L. CORROSION TASK NR C53-208-01. INSTALLED NEW STRINGER AND STRINGER SPLICES PER SRM 53-10-3. (M)SDR USAA980551Angle · crackedDURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH STATION 727 WL 200 LBL 45 CHORD ANGLE. INSTALLED REPAIR ANGLE PER TR 53-10-03A. (M)SDR USAA980550Sill · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 6 INCH AREA OF CORROSION BS 300-306 WL 208.10, RBBL 54 FORWARD SERVICE DOOR INNER CHORD. CORROSION TASK NR C53-107-01. INSTALLED NEW 'Z' ANGLE PER SRM 51-10-1 AND SRM 51-30-2. (M)SDR USAA980546Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .03125 INCH CRACK AT LOWER AFT CORNERS FORWARD ENTRY DOOR STATION 342 WL 208.1 SKIN FUSELAGE. CUT OUT CRACKED AREA FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER AND TRIPLER PER BOEING DRAWING 65C27257 AND EASDR USAA980545Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727B STRINGER 7R TIE CLIP. INSTALLED NEW STRINGER TIE CLIP PER PCI 1093, EO 5393G227. (M)SDR USAA980544Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION FOUND A .25 INCH CRACK BS 727A STRINGER 7R TIE CLIP. INSTALLED NEW TIE CLIP PER PCI 1093, EO 5393G227. (M)SDR USAA980543Web · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION VERIFIED BY EDDY CURRENT, FOUND A CRACK BL 0 BS 706, .6 INCH CRACK BS 708 .25 INCH CRACK BS 709 .6 INCH CRACK BS 710 .2 INCH CRACK BS 712 .15 INCH CRACK ON WEB. INSTALLED DOUBELR PER EA 62724A. (M)SDR USAA980534Skin · crackedCLT - DURING Q-CHECK VISUAL INSPECTION, FOUND A .20 INCH CRACK LEFT AFT ENTRY DOORWAY FORWARD LOWER CORNER BS 961, 2 INCHES ABOVE STRINGER 17L OF SKIN. INSTALLED TRIPLER PER REPAIR DOCUMENT 53-30-3 FIG 24. (M)SDR USAA980524Floorbeam · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 11 CORRODED AREAS BS 986.5 LBL 18 TO RBL 43 WL 208.1 OF FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED REPAIR T-CAP PER SRM 53-10-9 FIG 2. (M)SDR USAA980518Stringer · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 927 STRINGER 25L. REPAIRED AREA PER SRM 53-10-1. (M)SDR USAA980517Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 616 STRINGER 1R TIE CLIP. REMOVED AND REPLACED PER EO 5393G227 REV 'A'. (M)SDR USAA980516Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 807 STRINGER 9R TIE CLIP. INSTALLED IDENTICAL PART PER EO 5393G227 REV 'A'. (M)SDR USAA980515Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 616 STRINGER 2R TIE CLIP. INSTALLED IDENTICAL PART PER EO 5393G227 REV 'A'. (M)SDR USAA980513Sill · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BS 294.5 WL 208.10 RBBL 53 FORWARD SERVICE ENTRY DOOR LOWER SILL INBOARD CHORD DOUBLER ANGLE. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (M)SDR USAA980512Skin · dentedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 3 INCH BY 1.5 INCH BY .062 INCH DENT 11 INCH AFT OF REAR ENTRY AND 18 INCH ABOVE LOWER DOOR SILL OF SKIN. INSTALLED DOUBLER PER SERM 53-30-3. (M)SDR USAA980511Skin · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK STATION 767 STRINGER 19R OF SKIN. INSTALLED DOUBLER PER SRM 53-30-3. (M)SDR USAA980510Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 597 STRINGER 9R. INSTALLED MODIFIED PART PAR EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)SDR USAA980509Clip · crackedCLT - DURIGN Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727B STRINGER 8R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)SDR USAA980508Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 616 STRINGER 5R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)SDR USAA980507Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 685 STRINGER 4R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)SDR USAA980506Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 747 STRINGER 9L TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)SDR USAA980505Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 639 STRINGER 4L TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)SDR USAA980504Clip · crackedCLT - DURING Q-5 CHECK VIAUL INSPECTION, FOUND A .25 INCH CRACK STATION 616 STRINGER 2R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)SDR USAA980503Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 616 STRINGER 1R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)SDR USAA980502Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 807 STRINGER 9R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)SDR USAASB98214Battery Pack · dischargedCMH - PILOT REPORTED THE LEFT AFT SERVICE DOOR EMERGENCY EXIT LIGHT FLICKERS. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAASB98170Anti-Ice Duct · blownPHL - FLT 993 - AFTER TAKEOFF FROM PHL, CREW OBSERVED A RAPID RISE IN THE NR 2 ENGINE CSD OIL TEMPERATURE FOLLOWED BY A NR 2 ENGINE OVERHEAT LIGHT. CREW REDUCED THRUST ON ENGINE AND OVERHEAT LIGHT WENT OUT. AIRCRAFT WAS AT FL 080 WHEN CREW MADE DECISION TO RSDR USAASB98091Fuel Pump · defectiveBWI - FL 2197 - AFTER TAKEOFF AT 1,000 FEET, CAPTAIN THOUGHT HE HAD AN ENGINE FAILURE. THE NR 1 ENGINE FAILED TO RESPOND TO THRUST LEVER MOVEMENT. CAPTAIN SHUT DOWN THE NR 1 ENGINE AND RETURNED TO FIELD AT BWI WHERE THE FLIGHT LANDED WITHOUT INCIDENT. AN ESDR 98ZZZX1641Fuel Control · defectiveBWI - FL 2197 - AFTER TAKEOFF AT 1,000 FEET, CAPTAIN THOUGHT HE HAD AN ENGINE FAILURE. THE NR 1 ENGINE FAILED TO RESPOND TO THRUST LEVER MOVEMENT. CAPTAIN SHUT DOWN THE NR 1 ENGINE AND RETURNED TO FIELD AT BWI WHERE THE FLIGHT LANDED WITHOUT INCIDENT. AN ESDR USAASB97281Battery Pack · dischargedSYR - MAINTENANCE FOUND THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT PANEL FAILS TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK NORMAL. (X)SDR USAASB97195Battery Pack · dischargedPHL - MAINTENANCE FOUND THE AFT ROW OF EMERGENCY ESCAPE PATH LIGHTING INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)SDR 97ZZZM769Battery Pack · dischargedPHL - MAINTENANCE FOUND THE AFT ROW OF EMERGENCY ESCAPE PATH LIGHTING INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)SDR USAASB97193Rod Assy · failedPHL - FL244 - DURING CLIMB-OUT FROM PHL AT APPROXIMATELY 21,000 FT, THE CABIN WAS AT 4 PSI DIFFERENTIAL WHEN THE AFT ENTRY DOOR WARNING LIGHT ILLUMINATED. FLIGHT ATTENDANT REPORTED THE AFT ENTRY DOOR HANDLE HAD POPPED UP. TRIED TO STOW IT BUT HANDLE WOULD NOSDR USAASB97085Battery Pack · dischargedCLT - FL 1499 - DURING FLIGHT, THE CENTER AISLE CEILING EMERGENCY LIGHTS IN THE MID CABIN FLICKER OFF AND ON. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND BATTERY CHARGER FOR THE CENTER AISLE CEILING EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD. (M)SDR 97ZZZM475Battery Charger · failedCLT - FL 1499 - DURING FLIGHT, THE CENTER AISLE CEILING EMERGENCY LIGHTS IN THE MID CABIN FLICKER OFF AND ON. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND BATTERY CHARGER FOR THE CENTER AISLE CEILING EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD. (M)SDR USAASB96259Battery Pack · dischargedROA - MAINTENANCE FOUND THE AFT LEFT AND RIGHT EXTERIOR EMERGENCY EXIT LGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT BATTERY PACKS LOCATED IN THE AFT CARGO COMPT. OPS CHECK GOOD. (M)
Back to N268AU, cancelled Dec 9, 2003