Boeing 767-224
Service difficulty reports · 224
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '767224' 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 aircraft_model_key = '767224' 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 CALA0600023Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT BS 325, RBL 32 TO LBL 60. REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1.SDR CALA0600020Floorbeam · corrodedINSPECTION FOUND CABIN FLOORBEAM CORRODED AT BS 303, LBL 16 TO LBL 52. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1.SDR CALA0600018Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 303 TO 325, LBL 32. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02, PAGE 8 AND SRM 51-40-02.SDR CALA0600004Stiffener · crackedINSPECTION FOUND A 1 INCH CRACK IN LT PYLON NAC STA 285 AREA I/B STIFFENER AFTER FRAME CHORD REMOVAL. THE STIFFENER WAS REPLACED IAW ECRA 5420-01445.SDR CALA0600003Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN LT PYLON NAC STA 285.4 AREA I/B FRAME CHORD. THE FRAME CHORD WAS REPLACED IAW ECRA 5420-01445.SDR CALA0500461Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT BS 325, LBL 28 TO LBL 60. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1.SDR CALA0500459Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 303 - 325, LBL 32. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02.SDR CALA0500458Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT BS 303, LBL 19 TO LBL 32. REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1.SDR CALA0600014Stiffener · crackedINSPECTION FOUND A 1.5 INCH CRACK IN NR 1 PYLON O/B FRAME CHORD ATTACH SUPPORT -T- (STIFFENER) DURING FRAME CHORD REMOVAL AT NAC STA 285.45 TO NAC STA 295. THE STIFFENER WAS REPLACED IAW ECRA 5420-01444.SDR CALA0600013Stiffener · crackedINSPECTION FOUND A 4.5 INCH CRACK IN NR 1 PYLON I/B FRAME CHORD ATTACH SUPPORT -T- (STIFFENER) AT NAC STA 285.45 TO NAC STA 295. THE SUPPORT STIFFENER WAS REPLACED IAW ECRA 5420-01444.SDR CALA0600012Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 1 PYLON O/B FRAME CHORD DURING ATTACH CLIP REMOVAL AT UPPER CLIP ADJACENT AREA, NAC STA 285.45. THE FRAME CHORD WAS REPLACED IAW ECRA 5420-01444.SDR CALA0600011Clip · crackedINSPECTION FOUND A 1.5 INCH CRACK IN NR 1 PYLON LT NACELLE STRUT FRAME CLIP AT NAC STA 285.45. THE FRAME CLIP WAS REPLACED IAW ECRA 5420-01444.SDR CALA0600010Frame · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 2 PYLON NACELLE STRUT FRAME CHORD AT NAC STA 285.45, I/B AREA. THE FRAME CHORD WAS REPLACED IAW ECRA 5420-01444.SDR CALA0600009Stiffener · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 2 PYLON I/B FRAME CHORD ATTACH SUPPORT -T- (SUPPORT STIFFENER) DURING FRAME CHORD REMOVAL AT NAC STA 285.45 TO NAC STA 295. THE SUPPORT STIFFENER WAS REPLACED IAW ECRA 5420-01444.SDR CALA0500431Floorbeam · corrodedINSPECTION FOUND CABIN FLOORBEAM CORRODED AT BS 325, LBL 55. THE CORRODED SECTION OF FLOORBEAM WAS REPLACED IAW SRM 53-00-51 FIGURE 201, REPAIR 2.SDR CALA0500430Floorbeam · corrodedINSPECTION FOUND THE FLOORBEAM CORRODED AT BS 303, LBL 27 TO LBL 31. THE CORRODED SECTION OF FLOORBEAM WAS REPLACED IAW SRM 53-00-51, FIGURE 201, REPAIR 2.SDR CALA0500372Coffeemaker · inoperativeTHE FORWARD ESPRESSO COFFEEMAKER BEGAN TO SMOKE AND GAVE OFF A BURNED ELECTRICAL ODOR WHILE EN ROUTE FROM EWR TO FCO. THE CIRCUIT BREAKER WAS PULLED AND THE SMOKE CEASED. THE FLIGHT WAS CONTINUED TO FCO WHERE IT LANDED WITHOUT FURTHER INCIDENT. THE ESPRESSOSDR CALA050110Engine · failedON TAKEOFF, AT APPROXIMATELY 90 KNOTS, RT ENGINE FAILED. REPLACED ENGINE.SDR CALA0500002Cable · defectiveTHE LT OVERWING SLIDE WAS PARTIALLY DEPLOYED WHILE PERFORMING MAINTENANCE. THE DOOR OPENED BUT, THE SLIDE DID NOT INFLATE. INVESTIGATION FOUND THAT THE LT INFLATION CABLE WAS NOT OPERATING PROPERLY AND IT WOULD NOT ACTIVATE THE INFLATION BOTTLE FOR SLIDE DEPLSDR CALA0400703Entertain Sys · malfunctionedSTRONG FUMES WITH A BURNING WIRE-LIKE ODOR WERE NOTED IN THE FIRST CLASS CABIN (FORWARD IN AREA OF ENTERTAINMENT SECTION) AFTER APPROXIMATELY 3 HOURS OF FLIGHT WHILE EN ROUTE TO EWR. THE ENTERTAINMENT SYSTEMS WERE SECURED AND THE ODOR CLEARED. THE AIRCRAFT LSDR CALA0300688Fuse · blownAISLE LIGHT INOP AT ROW 29 THROUGH 37. REPLACED FUSE AT ROW 35 BATTERY CHARGER, OPS CHECK GOOD.SDR CALA0300329Fan · inoperativeAN ELECTRICAL SMOKE ODOR WAS DETECTED ON THE FLIGHT DECK AND IN THE VICINITY OF SEAT 3B OVERHEAD. THE UTILITY BUSSES AND RECIRCULATION FANS WERE TURNED OFF AND THE EQUIPMENT COOLING SELECTOR WAS TURNED TO STANDBY IAW CHECKLIST. THE ODOR DISSIPATED AND THE AIRCSDR CALA0300149Actuator · inoperativeTHE FORWARD AND AFT DOOR ACTUATORS FOR THE RT SIDE OFF-WING SLIDE DOOR WERE FOUND EXPENDED. THE DOOR ACTUATORS WERE REMOVED AND REPLACED IAW MM 25-65-10.SDR CALA0200441Battery · overheatedSMOKE AND BURNING ODOR ENTERED THE COCKPIT ON DESCENT INTO BRU. THE BATTERY CHARGER CIRCUIT BREAKER WAS PULLED AND THE SMOKE AND ODOR CEASED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE MAIN BATTERY HAD OVERHEATED AND BUBBLED OVER. THE MAIN
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