Boeing 767-231
Service difficulty reports · 758
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 = '767231' 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 = '767231' 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 TWAA9818102Switch · wornTHE EXTERIOR EMERGENCY LIGHT TEST SWITCH WAS FOUND INOPERATIVE. REPLACED SWITCH. CHECK-C 9-16-98 LAX.SDR TWAA9818311Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND FUSELAGE STRINGER 39R CORRODED BETWEEN STA 610 AND 632. REMOVED S39R AT STA 600 TO 622 AND INSTALLED NEW FABRICATED PART PER SRM 53-00-03.SDR TWAA9901008Skin · corrodedDURING OP 15 MAINT CHECK, FOUND STA 1269, STRINGER 39R WITH CORROSION BETWEEN INBD SIDE OF STRINGER AND FUSELAGE SKIN, AND STRINGER 39L CORRODED BETWEEN STRINGER AND SKIN AT STA 1264. CUT OUT SKIN AND INSTALLED EXTERNAL DOUBLER REPAIR PER ARA 15766 AND SRM 5SDR TWAA9818206Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON LOWER SIDE OF STRINGER 38R, STA 565. CUT OUT CORROSION PER SRM 51-10-03 PAGE 16. INSTALLED SECTION OF STRINGER AT 38R STA 565 PER SRM 53-00-03, FIG 202.SDR TWAA9818205Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON STRINGER 39L BETWEEN STA 616 TO 632. REMOVED SECTION OF CORRODED STRINGER AND CLEANED STA 606 TO 632 PER SRM 51-10-00 PAGE 16. INSTALLED SPLICE BETWEEN STA 600 TO 632 PER SRM 53-00-03, PAGE 215 DETAIL III FIG 207SDR TWAA9818204Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND CORRODED STRINGER 38R BETWEEN STA 610 TO 632. CUT OUT SECTION OF STRINGER FROM STA 600 TO 627. REMOVED CORROSION PER SRM 51-10-00 PAGE 16. INSTALLED CRACK REPAIR PER SRM 53-00-03 PAGE 219 FIG 203 SHEET 3.SDR TWAA9818203Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND STRINGER 39L CORRODED AT STA 610 TO 632. REMOVED SECTION OF CORRODED STRINGER AND CLEANED STA 606 TO 632. INSTALLED SPLICE BETWEEN STA 600 TO 637 PER SRM 53-00-03, PAGE 215 DETAIL 14, FIG 207 SHEET A.SDR TWAA9818202Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION AT STA 580 STRINGER 39L ON THE STRINGER. SPLICED STRINGER AT STA 577 TO 600 PER SRM 53-00-03 PAGE 215, DETAIL III, FIG 207.SDR TWAA9818302Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND STRINGER 39R WITH EXFOLIATION CORROSION AT STA 561 TO 562, ON TOP INBD LIP APPROX 1 IN LONG. CORROSION REMOVED AND REPAIRED WITH J-ANGLE PER SRM 53-00-03, PAGE 218.SDR TWAA9818012Skin · corrodedDURING OP 15 MAINT CHECK, CENTER WING UPPER SKIN WAS CUT OUT FOR CORROSION TO SKIN STA 853 TO 855. RECTANGULAR SECT FRONT 71 RBL TO 84 RBL AND REAR 69 RBL TO 86 RBL. ACCOMP HIGH FREQ EDDY CURRENT OF AREA AND HOLES PER 51-00-03 PART 6 OF TWA NDT MANUAL AND NOSDR TWAA9818011Skin · corrodedDURING OP 15 MAINT CHECK, FOUND BELOW UPPER CENTER WING SKIN SUPPORT BEAM WITH EXIFOLIATION CORROSION THRU BEAM. CORROSION VISIBLE FROM STA 855 TO 853 RBL 75 TO RBL 86. ACCOMP HIGH FREQ EDDY CURRENT OF AREA AND HOLES PER TWA NDT MANUAL 51-10-03, PART 6 AND SDR TWAA9818010Skin · corrodedDURING OP 15 MAINT CHECK, FOUND INTERGRANULAR CORROSION ON CENTER UPPER WING SKIN AT STA 954.5 TO 858, RBL 75 TO RBL 88. ACCOMP HIGH FREQ EDDY CURRENT OF AREA AND HOLES PER TWA NDT MANUAL 51-00-03, PART 6, AND NO CRACKS FOUND. REMOVED CORROSION AND APPLIED RSDR TWAA9818009Skin · corrodedDURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION ON UPPER SURFACE OF WING CENTER SECTION AT STA 860 BELOW EMERGENCY EXIT ON RT SIDE. CUT OUT CORRODED AREA PER SRM 51-10-00. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6 AND NO CRACKS FOUND. REMOVED CSDR TWAA9818008Skin · corrodedDURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION AT UPPER SKIN STA 830 TO 852, RBL 74 TO RBL 97. REMOVED CORROSION PER SRM 51-10-00. NDT HIGH FREQ EDY CURRENT PER 51-10-03, PART 6 AND NO CRACKS FOUND. REPAIRED PER TWA ARA 11596.SDR TWAA9818210Stringer · crackedDURING OP 15 MAINT CHECK, FOUND STRINGER 33L CRACKED AT STA 434. REPAIRED STRINGER PER SRM 53-00-03 PAGE 209 FIG 202.SDR TWAA9818209Stringer · crackedDURING OP 15 MAINT CHECK, FOUND FWD END OF STRINGER 33R CRACKED AT FORMER TIE FITTING, STA 1085. SPLICED IN NEW SECTION OF STRINGER PER 767-200 SRM 53-00-03 PAGE 209 TO 216 AND 51-40-03 PAGE 1.SDR TWAA9818208Stringer · crackedDURING OP 15 MAINT CHECK, FOUND STRINGER 33L CRACKED AT STA 434. REPAIRED STRINGER PER SRM 53-00-03 PG 209 FIG 202.SDR TWAA9818207Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND FORWARD END OF STRINGER 33R CRACKED AT FORMER TIE FITTING, STA 1085. SPLICED IN NEW SECTION OF STRINGER PER 767-200 SRM 53-00-03 PAGE 209 TO 216 AND 51-40-03 PAGE 1.SDR TWAA9818312Skin · gougedDURING OP 15 MAINT CHECK, FOUND LT ELEV HAD ONE INCH LONG GOUGE IN UPPER SURPACE, 29 IN OTBD FROM OTBD ACTUATOR, AND 15 IN AFT FROM THE LEADING EDGE. REMOVED DAMAGED AREA AND REPAIRED WITH 6 PLIES OF GRAPHITE OVERLAY PER SRM 55-20-01, PAR 3C, AND 51-10-17, PASDR TWAA9818007Skin · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION AT UPPER SKIN CENTER WING AT STA 850 TO 852.5, RBL 83.5 TO RBL 88.5, INTERGRANULAR CORROSION. SANDED CORROSION PER SRM 51-10-00, PAGE 16 PARA 6. ACCOMP HIGH FREQ EDDY CURRENT NDT PER 51-00-03, PART 6 AND NO CRACKS FOSDR TWAA9818006Skin · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON CENTER FUEL TANK UPPER SKIN AT STA 846, RBL 79 TO 83. SANDED CORROSION PER SRM 51-10-00, PAGE 16 PARA 6. NO CRACKS FOUND USING HIGH FREQ EDDY CURRENT NDT PER 51-00-03, PART 6. REPAIRED PER ARA 11596.SDR TWAA9817806Skin · corrodedDURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION ON UPPER SKIN, STA 830 TO 852, LBL 74 IN TO LBL 97 IN. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6 AND NO CRACKS FOUND. REPAIRED PER ARA 11596.SDR TWAA9817805Skin · corrodedDURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION ON UPPER SURFACE OF WING CENTER SECTION, STA 860 BELOW EMERGENCY EXIT ON LT SIDE. REMOVED CORROSION PER SRM 51-10-00. NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6, AND NO CRACKS FOUND. REPAIRED PER ARA 1159SDR TWAA9817804Skin · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON TOP WING AT FASTENERS STA 883 TO 911, LBL 74 IN TO 97 IN. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6, AND NO CRACKS FOUND. REMOVED CORROSION PER SRM 51-10-11. REPAIRED PER ARA 11596.SDR TWAA9817803Skin · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION AT TOP WING SKIN AT FASTENERS STA 911 TO 933, LBL 74 IN TO 97 IN. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6 AND NO CRACKS WERE FOUND. REMOVED CORROSION PER SRM 51-10-00. SPOT FACED AND BLENDED AS NEEDED SDR TWAA9817802Skin · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON TOP WING SKIN AT FASTENERS STA 933 TO 965, LBL 74 IN TO 97 IN. REMOVED CORROSION PER SRM 51-10-00. NDT EDDY CURRENT PER 51-00-03 PART 5, FOUND NO CRACKS. SPOT FACED AND BLENDED AS NEEDED PER MCI 98-0185RE. REPAISDR TWAA9817801Skin · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON TOP WING SKIN AT FASTENERS STA 859 TO 883, LBL 74 IN TO 97 IN. REMOVED CORROSION PER SRM 51-10-00. NDT HIGH FREQ EDDY CURRENT OF HOLES PER 51-00-03, PART 6, FOUND NO CRACKS. REPAIRED PER ARA 11596.SDR TWAA9818310Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON STRINGER 38R AT STA 615. CUT OUT CORRODED SECTION AND REPAIRED STRINGER 38R PER SRM 53-00-03, FIG 203.SDR TWAA9818309Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON STRINGER 34L AND STRINGER SPLICE AT STA 434. REMOVED DAMAGED PART OF STRINGER AND STRINGER SPLICE AND INSTALLED REPAIR PER SRM 53-00-03, FIG 202.SDR TWAA9818308Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND STRINGER 36L CORRODED AT STA 610 TO 632. SPLICED IN NEW 20 INCH SECTION AT STA 601 TO 621, PER SRM 53-00-03, PG 209 TO 215, FIG 202 SHEET 1 - 7.SDR TWAA9818307Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND STRINGER 39L HAD CORROSION IN CHANNEL AT STA 1395 TO 1417. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-00-03, FIG 202.SDR TWAA9818306Stringer · brokenDURING OP 15 MAINT CHECK, FOUND FUSELAGE STRINGER SPLICE AND STRINGER BROKEN AT STA 434, STRINGER 34R. REPLACED DAMAGED PARTS PER SRM 53-00-03.SDR TWAA9818303Structure · corrodedDURING OP 15 MAINT CHECK, FOUND FUSELAGE FORMER 434 STRINGER AND SPLICE CORRODED, STRINGER 39L. REPLACED S-39L AND SPLICE PER SRM 53-00-03, PAGE 209.SDR TWAA9818402Keel Beam · corrodedDURING CHECK-C MAINT, FOUND SURFACE CORROSION TO INTERGRANULAR CORROSION ON KEEL BEAM RT AND LT LOWER LEG, TOP AND BOTTOM OF I/B LEG FROM STA 933 THRU MAIN GEAR WHEEL WELL AREA. REMOVED CORROSION PER SRM 51-10-00 PG 1. TREATED WITH ALODINE AND PRIMED.SDR TWAA9818305Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND FUSELAGE STRINGER 39R WITH CORROSION AT STA 434 TO 460. REPLACED CORRODED STRINGER AND SPLICE 7075-T6 WITH BAC15CC6KC HI-LOCS.SDR TWAA9818304Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND FUSELAGE STRINGER 39L WITH CORROSION AT STA 434 TO 460. REPLACED CORRODED STRINGER PER 53-00-3, FIG 202.SDR TWAA9815002Skin · delaminatedDURING CHECK-C MAINT, FOUND RT WING NR 11 LE SLAT REPAIR LOOSE IN CENTER AREA, 1.5 IN BY 2.5 IN. REMOVED OLD REPAIR. REMOVED 1 IN BY 3 IN DELAMINATION ON O/B END OF OLD REPAIR TO SKIN, AND REMOVED DAMAGED CORE. INSTALLED SKIN AND CORE REPLACEMENT WITH HOT BSDR TWAA9814703Battery Pack · dischargedESCAPE PATH LIGHTS IN RT AISLE ROWS 8 TO 45 ILLUMINATED INTERMITTENTLY. REPLACED RT EGRESS LIGHT BATTERY PACK. CHECK-C 8-1-98 LAX.SDR TWAA9814701Battery Pack · dischargedEGRESS LIGHTS WERE REPORTED AS FLASHING WITH SWITCH IN ARMED POSITION. REPLACED BATTERY PACK. CHECK-C 6-14-98 LAX.SDR TWAA9814903Te Wedge · crackedDURING CHECK-C MAINT, FOUND ON RT WING THE O/B TE FLAP, CENTER TE WEDGE LOWER SURFACE WITH A 4 INCH CRACK. DRESSED OUT DAMAGED AREA AND INSTALLED 3 SKIN HOT BOND REPAIRS 4 IN BY 6 IN PER SRM 51-70-07 FIG 4A.SDR TWAA9814304Connector · looseFOUND EGRESS LIGHT STRIP INOPERATIVE IN AFT GALLEY AREA DURING MAINTENANCE TEST. FOUND LOOSE CONNECTION. RESEATED FLEX JUMPER TO POWER FLEX CABLE AND SECURED. CHECK-C 6-14-98 LAX.SDR TWAA9814303Power Supply · inoperativeEGRESS LIGHT ON RT SIDE OF FWD CABIN ILLUMINATE INTERMITTENTLY. REPLACED EGRESS POWER SUPPLY. CHECK-C 6-14-98 LAX.SDR TWAA9813602Regulator · leakingCREW OXYGEN PRESSURE WENT TO ZERO, NOTICED AT TOP OF CLIMB. RETURNED TO JFK. FOUND CAPT OXY REGULATOR FAULTY. REPLACED REGULATOR AND OXY BOTTLE. CHECK-C 7-9-98 LAX.SDR TWAA9813501Light · malfunctionedFLOOR EGRESS LIGHTS ILLUMINATED ON LT SIDE, ROWS 12 THROUGH 13, AND ROWS 22 THROUGH 30, WHEN SWITCH PLACED IN ARM POSN. EGRESS LIGHT MALFUNCTIONS WERE DEFERRED PER MEL. AT THE NEXT STATION THE LIGHTS WERE FOUND TO OPERATE NORMALLY. CHECK-C 8-1-98 LAX.SDR TWAA9812503Skin · delaminatedDURING CHECK-C MAINT, FOUND ON RT WING THE LE PANEL UNDER NR 7 LE SLAT, APPROX 2/3 DISTANCE FROM INBD END OF STRUT, HAD .5 IN BY 2.5 IN LONG DELAMINATED LOOKING CRACK. INSTALLED REPAIR SIZE 2 IN BY 3 IN AND HOT BOND REPAIR PER SRM 51-70-17.SDR TWAA9812502Skin · delaminatedDURING CHECK-C MAINT, FOUND DELAMINATION ON LT WING UPPER LE 2.5 FEET BEHIND NR 6 LE SLAT, OTBD END, 5 INCHES LONG. REPAIRED SURFACE WITH A 3 IN BY 5 IN HOT BOND REPAIR PER SRM 51-70-08, PG 6 THRU 32.SDR TWAA9813702Skin · damagedDURING ROUTINE CHECK OF ACFT, FOUND RT O/B TE FLAP, I/B OF I/B CANOE, WITH LEADING EDGE DAMAGED 18 IN BY 8 IN. REPAIRED DAMAGE PER SRM 57-53-01 AND 57-70-17. CHECK-C 6-28-98 LAX.SDR TWAA9812114Strap · crackedSTRAP CRACKED AND TORN AT RIVET HOLES STA 456, BETWEEN S35 AND S36. REPAIRED PER ARA 11576.SDR TWAA9812113Splice · crackedDURING DAMAGE REPAIRS FOUND SPLICE PLATE CRACKED AT RIVET HOLE TO MATERIAL EDGE AT STA 434, STR 36. REPAIRED PER ARA 11576.SDR TWAA9812112Stringer · corrodedFOUND DURING DAMAGE REPAIRS STRINGER 33L HAD CORROSION AT STA 448. REPAIRED PER SRM 53-00-03 DETAIL III. CHECK-C 4-20-98 LAX.
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