Boeing 767-241
Service difficulty reports · 165
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 = '767241' 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 = '767241' 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 TAMF20090006SSkin · dentedDURING C3 CHECK INSPECTION FOUND RT AFT FUSELAGE BETWEEN STA 1906.80 TO STA 1915.15 WL 221.0 HAS DENT. REPAIRED ACCOMPLISHED IAW EWO 767 53-080 AND SRM 53-00-01 REPAIR 1.SDR TAMF20090011SKeelbeam · corrodedDURING C3 CHECK INSP, FOUND CORROSION ON HORIZONTAL WEB AT KEELBEAM STA 830. REPAIR ACCOMPLISHED IAW EWO 767 53-084 AND SR 1-1232023924.SDR TAMF20090014STorque Box · crackedDURING C3 CHECK INSPECTION, FOUND A CRACK ON ENGINE NR 1 T/R FIXED TORQUE BOX 6 O’CLOCK - RT. REPAIR ACCOMPLISHED IAW EWO 767 54-050 AND MRA 8CQT090317-BH REPAIR. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20090013SRib · damagedDURING ROUTINE C3 CHECK INSPECTION OF THRUST REVERSER, FOUND LT ENGINE RT T/R WITH ONE ZEE RIB DAMAGE DUE TO INTERFERENCE WITH ENGINE HARDWARE. REPAIR ACCOMPLISHED IAW EWO 767 78-019 AND MRAS CMM 78-32-02 REPAIR 033.SDR TAMF20090002SSkin · crackedDURING "C3" CHECK INSP, CRACKS FOUND ON UPPER SKIN ON SLAT NR 5 AT STA OSS 424.097 REPAIR SLAT IAW EWO 767 57-049 AND SR 1-1230186572. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20090008SFrame · chafedDURING C3 CHECK INSPECTION FOUND ENG NR2 RH CORE COWL NAC STA 303.75 FRAME AND STRAP WITH CHAFING. REPAIRED ACCOMPLISHED IAW EWO 767 54-048 AND ROHR CV 09-0629-01.SDR TAMF20090007SFrame · crackedDURING C3 CHECK INSPECTION FOUND ENG NR 2 RT CORE COWL NAC STA 275 FRAME CRACKED. REPAIR ACCOMPLISHED IAW EWO 767 54-049 AND ROHR CV 09-0629-01.SDR TAMF20090005SSkin · dentedDURING C3 CHECK INSPECTION FOUND RT AFT FUSELAGE BETWEEN STA 1923.50, STA 1933.50 UPPER SIDE WL 241.10 HAS DENT. REPAIRED ACCOMPLISHED IAW EWO 767 53-079 AND SRM 53-00-01 REPAIR 6.SDR TAMF20090004SSplice Plate · corrodedDURING C3 CHECK INSPECTION, FOUND CORROSION ON THE LOWER SURFACE OF THE UPPER SPLICE PLATE AT STA OSS 460 RH. CORROSION REMOVED AND REPAIRED IAW EWO 767 57-051 AND SR 1-1230329934.SDR TAMF20090003SSkin · dentedDURING C3 CHECK WAS FOUND AFTER CARGO COMPARTMENT DOOR LOWER EDGE OUTER SKIN HAS TWO DENTS. ACCOMPLISHED REPAIR IAW EWO 767 52-012 AND SR 1-1232057632.SDR TAMF20090001SStructure · chafedDURING C3 CHECK, FOUND RT AILERON INBOARD WITH CHAFING IN CORNER RT PART UPPER SIDE. REMOVED INBD AILERON IAW AMM 27-11-01 PAGE 401 TO 408 ACCOMPLISHED EWO 767 57-048 AILERON FITTING THICKNESS FOUND MIN 0.055 INCH IAW 767 NDT MANUAL D634T301 PART 4 SUB 51-00-SDR 2008FA0000428Light · illuminatedCABIN ALT AND CABIN ALTITUDE LIGHTS ILLUM, EICAS MSG CABIN ALTITUDE WAS DISPLAYED. UNABLE TO RESTORE CABIN PRESS USING MANUAL MODE. AIRPLANE RETURNED TO DEPARTURE. IAW FIM 21-31-00, FIG 103 BLOCKS 1,2,22,23,23A, 24, 44, PLN U3 IN CONNECTOR D2712A WAS REPAIREDSDR 2008FA0000427Transmitter · faultyLT FLAP DID NOT MOVE FROM 1 TO UP POSITION. FLIGHT RETURNED TO DEPARTURE. REMOVED AND REPLACED PROXIMITY SENSORS S282 AND S283 IAW SWPM 20-30-12 AND AMM 27-88-01, BITE TEST PSEU WAS PERFORMED AND IT WAS FOUND NORMAL IAW FIM 32-09-03, FIG 103. FLAP POSITION TRSDR TAMF20080018SRib · corrodedCORROSION ON LT WING OB L/E RIB LOWER OUTER SHROUD AT STA 933.73 AND 938.73. (2) RIBS WERE FABRICATED AND INSTALLED IAW MFG AUTHORIZATION PO214294 AND PO214297, DRAWINGS 117T2224 AND 114T2223 AND SRM 51-40-02/1-3 AND 7.SDR TAMF20080017SRib · corrodedCORROSION ON LT WING OB L/E RIB LOWER CHORD STA 779.44 AND 784.44. (2) RIBS WERE FABRICATED AND INSTALLED IAW P0214296 AND P0214326, AND DRAWINGS 114T2217 AND 114T2218 AND SRM 51-40-02 PG 1-7.
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