Boeing 767-201
Service difficulty reports · 660
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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 = '767201' 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 = '767201' 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 USAABB00078Clock · failedPHL - FLT 188 - EN ROUTE CLT/CDG, CREW EXPERIENCED A DUAL FMC FAILURE (EICAS MESSAGE ''L/R FMC FAIL''. FLIGHT DIVERTED TO PHL, AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED BOTH FMC''S AND THE CAPTAIN''S CLOCK. (X)SDR USAABB00074Fmc · faultyPHL - FLT 2 - EN ROUTE PHL/FCO, CREW NOTED THE LOSS OF BOTH FMC''S. CYCLING THE CIRCUIT BREAKERS BROUGHT THE FMC''S BACK ON-LINE, HOWEVER, THE CREW DECIDED NOT TO CONTINUE THE FLIGHT. FLIGHT RETURNED TO PHL, AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SDR USAABB00075Fmc · failedPHL - FLT 2 EN ROUTE PHL/FCO, CREW NOTED THE LOSS OF BOTH FMC''S. CYCLING THE CIRCUIT BREAKERS BROUGHT THE FMC''S BACK ON-LINE, HOWEVER, THE CREW DECIDED NOT TO CONTINUE THE FLIGHT. FLIGHT RETURNED TO PHL AND LANDED WITHOU FURTHER INCIDENT. (X)SDR USAABB00067Pump · failedCLT - FLT 855 - EN ROUTE TO JAX, WITH THE RIGHT FORWARD FUEL BOOST PUMP ON MEL, CREW RECEIVED INDICATIONS OF LOW PRESSURE ON THE LEFT FORWARD BOOST PUMP. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT FORWARD BOOSTSDR USAA000574Skin Panel · corrodedCLT - FOUND SKIN PANEL CORRODED 1 INCH BY 3 INCHES, STATION 953, WL 179, RBL 80. REPAIRED FILLER AND DOUBLER PER EA 67035, SRM 51-40-03 AND SRM 51-20-05. (M)SDR USAABB00053Computer · malfunctionedPHL - FLT 894 - EN ROUTE PHL-FRA, THE CREW RECEIVED THE EICAS MESSAGE R HYD SYSTEM MAINTENANCE. SUBSEQUENTLY, ALSO RECEIVED THE EICAS MESSAGED LDG GEAR MONITOR AND EICAS DISAGREE. THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RSDR USAABB00052Sensor · failedLGW - FLT 127 - AFTER TAKEOFF, CREW RECEIVED THE EICAS MESSAGE R HYD QTY AND THE ASSOCIATED LIGHT. THE HYDRAULIC QUANTITY READ 0, BUT THE PRESSURE WAS NORMAL. FLIGHT RETURNED TO LGW AND LANED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE HYDRAULIC QUANSDR USAABB00034Charger · inoperativeCLT - FOUND FLOOR TRACK LIGHT INOPERATIVE FROM SEAT ROW 21 AFT. MAINTENANCE REPLACED THE BATTERY CHARGER ASSEMBLY. (M)SDR USAABB00033Sensor · misalignedBOS - EN ROUTE PHL/MUC, CREW RECEIVED AN E/E ACCESS DOOR WARNING. ALTHOUGH NO PRESSURIZATION PROBLEMS EXISTED, THE CREW DECIDED TO DIVERT. FLIGHT DIVERTED TO BOS AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE SHIMMED THE E/E DOOR PROXIMITY SENSOR. (X)SDR USAABB00031Idg · leakingPIT - FLT 48 - AFTER TAKEOFF FROM PIT, CREW RECEIVED A FLICKERING E/M 'R GEN DRIVE' AND THE ASSOCIATED LIGHT. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED A LEAKING IDG SERVICE FITTING. (M)SDR USAABB00030Fmc · failedPHL - FLT 894 - EN ROUTE PHL-FRA, APPROXIMATELY 35 MILE AFTER TAKEOFF, CREW NOTED THAT BOTH FMC''S WERE PROBLEMATIC. THE TIMES, MILEAGE AND FUEL DISAGREED, AND THE WAYPOINT AND TOTAL MILEAGE WAS NOT CHANGING. FLIGHT RETURNED TO PHL AND LANDED WITH NO FURTHERSDR USAABB00026Switch · failedKEF - FLT 893 - EN ROUTE FRA-PHL - CREW RECEIVED THE LEFT GENERATOR DRIVE LIGHT AND DISCONNECTED THE IDG. THE APU WAS STARTED AND RAN FOR APPROX 15 MINUTES, AFTER WHICH IT PERFORMED AN AUTO SHUTDOWN. THE FLIGHT DIVERTED TO KEF AND LANDED WITH NO FURTHER INCISDR USAABB00027Apu · malfunctionedBOS - FLT 893 - EN ROUTE KEF-PHL, WITH THE LEFT IDG ON MEL AND THE APU OPERATING, THE APU PERFORMED AN AUTO SHUTDOWN (AFTER APPROX 4.5 HOURS OF OPERATION). FLIGHT DIVERTED TO BOS. MAINTENANCE IN BOS REPLACED THE LEFT GENERATOR AND THE DE-OIL SOLENOID IN THE SDR USAABB00021Power Supply · inoperativeCDG - FORWARD AND AFT EXIT DOOR THRESHOLD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE SWAPPED POWER SUPPLIES M1208 AND 1210 WITH M735 AND M739, FERRIED THE AIRCRAFT, THEN REPLACED THE POWER SUPPLIES. (M)SDR USAABB00017Power Supply · failedLGW - COULD NOT TURN EMERGENCY LIGHTS OFF. MAINTENANCE REPLACED THE TWO FORWARD AND TWO AFT POWER SUPPLIES. (M)SDR USAABB00015Control Panel · failedLGW - FLT 127 - AFTER TAKEOFF FROM LGW, CREW NOTED A LOW HYDRAULIC PRESSURE INDICATION ON THE C SYSTEM AND REPORTED THAT THE GEAR WAS SLOW TO RETRACT. FLIGHT RETURNED TO LGW, AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE HYDRAULIC CONTROL PANSDR USAABB00001Unknown · odorPHL - FLT 893 - ON ARRIVAL TO PHL AT FL250, CRWE NOTED AN ACRID ODOR IN THE COCKPIT. CREW DESCENDED TO FL180 AND PERFORMED CHECKLIST PROCEDURE, INCLUDING SECURING THE RECIRC FANS, UTILITY BUS, APU BLEED AIR AND EACH AIR CONDITIONING PACK (ALTERNATELY). THE OSDR USAABB99062Seal · rupturedCDG - FLT 23 - AFTER TAKEOFF FROM CDG, CREW NOTED THE LEFT HYDRAULIC QUANTITY DECREASING TO ZERO, AND THE LEFT SYSTEM QUANTITY AND PRESSURE LIGHTS ILLUMINATING. CRWE ALSO RECEIVED THE EICAS MESSAGES L HYD QTY AND L HYD SYS PRESS. FLIGHT RETURNED TO CGD AND LSDR USAABB99057Light Panel · malfunctionedPHL - CREW DISCOVERED A PROBLEM WITH THE EMERGENCY LIGHT PANEL. MAINTENANCE REPLACED THE PANEL. (X)SDR USAABB99055Atc · failedPHL-LGW - FLT 126 - CREW RECEIVED THE EICAS MESSAGE 'ATC FAULT' AND THE ASSOCIATED LIGHT. BOTH TRANSPONDERS WERE REPORTED TO BE INOPERATIVE. AFTER CONFERRING WITH MAINTENANCE, THE FLIGHT RETURNED TO PHL AND LANDED WITH NO FURTHER PROBLEMS. MAINTENANCE REPLASDR USAABB99056Wire · arcedPIT - FLT 781 - CREW NOTED ELECTRICAL SMELL IN AFT GALLEY. (CIRCUIT BREAKER HAD TRIPPED.) MAINTENANCE FOUND THE CABLE ASSEMBLY FOR HEATED MEAL CART A201 ARCING AND REPLACED IT. (X)SDR USAABB99043Sensor · damagedBOS - FLT 894 - AFTER TAKEOFF FROM PHL, CREW RECEIVED THE BULK CARGO DOOR LIGHT. FLIGHT DIVERTED TO BOS AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE BULK CARGO DOOR LATCH SENSOR (S211) DAMAGED. AIRCRAFT WAS RELEASED ON MEL. (M)SDR USAABB99037Fuel Control · failedLGW - FLT 49 - EN ROUTE CDG/PIT, WITH RIGHT IDG ON MEL AND THE APU OPERATING, THE APU 'FAULT' LIGHT ILLUMINATED AND THE EICAS MESSAGE 'APU FAULT' APPEARED. THE APU WAS SHUT DOWN. THE FLIGHT DIVERTED TO LGW AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE RESDR USAABB99025Connector · loosePHL - FLT 126 - AFTER A PREVIOUS RETF DUE TO FLUCTUATING RIGHT EGT AND SUBSEQUENT MAINTENANCE, FLIGHT 126 AGAIN RETURNED TO PHL FOR THE SAME PROBLEM. MAINTENANCE REPLACED THE NR 17 AND 18 PINS AND SOCKETS INPLUG D4208P. (M)SDR USAABB99024Harness · frayedPHL - FLT 126 - AFTER TAKEOFF FROM PHL, CREW NOTED THAT THE RIGHT EGT INDICATION AND STANDBY INDICATION WERE FLUCTUATING. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE UPPER EGT HARNESS FRAYED AND REPLACED IT. TEST FLIGHTSDR USAA990479Floorbeam · corrodedCLT - DURING C-4 CHECK, FOUND 2 INCH BY 1 INCH CORRODED AREA AT FLOORBEAM STATION 344 RBL 88, CORROSION LEVEL 1. REPLACED T-CAP PER SRM 53-00-51. (M)SDR USAA990473Floorbeam · corrodedCLT - DURING C-4 CHECK, FOUND 2 INCH CORRODED AREA OF FLOORBEAM AT STATION 287 RBL 79. CORROSION LEVEL 1. SPLICED SECTION T-CAP, INSTALLED REPAIR ANGLES EPR SRM 51-10. (M)SDR USAA990472Beam · corrodedCLT - DURING C-4 CHECK, FOUND 3 INCH CORROSION AT SCREW HOLE ON T-CAP AT STATION 355 APPROX RBL 47. CORROSION LEVEL 2. INSTALLED REPAIR ANGLES PER SRM 53-00-51. (M)SDR USAA990471Floorbeam · corrodedCLT - DURING C-4 CHECK, FOUND 2 INCH CORROSION ON FLOORBEAM AT STATION 303 RBL 53, CORROSION LEVEL 1. CUT SECTION OF T-CAP, INSTALLED NEW SECTION AND REPAIR ANGLES PER SRM 53-00-51. (M)SDR USAABB99023O-Ring · rupturedPHL - FLT 12 - EN ROUTE PHL-MAD, AT APPROXIMATELY 50W LONGITUDE, THE CREW NOTED THAT THE LEFT ENGINE OIL PRESSURE WAS LOW AND THAT THE QTY WAS FLUCTUATING BETWEEN 13 AND 14. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A BAD SDR USAABB99022Starter · failedPHL - FL126 - CREW RECEIVED EICAS MESSAGE 'L STARTER CUTOUT' ON CLIMB-OUT FROM PHL. FLIGHT RETURNED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE STARTER AND START VALVE. (M)SDR 99ZZZM357Start Valve · failedPHL - FL126 - CREW RECEIVED EICAS MESSAGE 'L STARTER CUTOUT' ON CLIMB-OUT FROM PHL. FLIGHT RETURNED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE STARTER AND START VALVE. (M)SDR USAABB99021Battery Charger · inoperativePHL - FOUND LEFT FORWARD EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED BATTERY AND CHARGER. (M)SDR USAA990463Frame · corrodedCLT - DURING C-4 CHECK, FOUND 3 INCH CORRODED AREAS AROUND NUTPLATE HOLES AT T-CAP FRAME AT STATION 287 RBL 63, CORROSION LEVEL 2. REPAIRED T-CAP PER SRM 53-00-51. (M)SDR USAA990422Floorbeam · corrodedCLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 4 INCH AREA OF CORROSION AT STATION 346 FLOORBEAM. INSTALLED REPAIR ANGLE PER EA 64434. (M)SDR USAABB99013Sensor · out of adjustPIT - FLT 48 - DURING CLIMB OUT OF PIT, CREW RECEIVED THE EICAS MESSAGE 'GEAR DOORS'. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. AIRCRAFT WAS FERRIED TO CLT. MAINTENANCE FOUND THE SYSTEM 1 RIGHT NOSE GEAR DOOR P2 CLOSED SENSOR (S235) GAP EXSDR USAABB99006Shear Pin · shearedAMS - FLT 42 - ON TOUCH DOWN AT AMS, THE RIGHT OVERWING SIDE DEPLOYED. MAINTENANCE FOUND THE OVERWIG DOOR LATCH ACTUATOR SQUIBS HAD NOT FIRED, BUT THE PIN THAT SHEARS WHEN THE ACTUATOR SQUIB FIRES (ALLOWING THE LATCHES TO OPEN) HAD SHEARED. IT IS NOT KNOWN WSDR USAABB99004Air Dist · odorPHL - FLT 15 - CREW REPORTED STRONG BURNING ODOR APPROXIMATELY TEN MINUTES PRIOR TO LANDING. FLIGHT CONTINUED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED THE COCKPIT, GALLEY, E/E BAY AND BOTH PACK BAYS. THE PACKS WERE OPERATED FROM BOTSDR USAA990060Seat Track · crackedCLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK STATION 1065 RBL 10 SEAT TRACK. INSTALLED SECTION SEAT TRACK PER EA 63457. (M)SDR USAA990059Clip · crackedCLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK STATION 1702 AND STRINGER 39 LT AT TIE CLIP. INSTALLED STRINGER TIE CLIP PER SRM 51-10-00. (M)SDR USAA990058Clip · crackedCLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 1702 AND STRINGER 30R AT TIE CLIP. INSTALLED STRINGER TIE CLIP PER SRM 51-10-00. (M)SDR USAA990038Floorbeam · crackedCLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK ON STIFFENER ANGLE STA 246 FLOORBEAM FORWARD FACE AT LBBL 17.0. REPAIRED FLOORBEAM ANGLE PER SRM 51-10-00. (X)SDR USAA990037Fairing · corrodedCLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION STA 980 RT SIDE KEEL BEAM FAIRING FLANGE NEAR SCREW HOLE. REPAIRED PER SRM 53-50-12 AND E.O. 5195T055, PART 2, STEPS 2, 4. (X)SDR USAA990036Seat Track · corrodedCLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION, 1 INCH BY 2 INCHES, BS 347 LBL 54.75 SEAT TRACK. REMOVED AND INSTALLED SEAT TRACK PER SRM 53-00-52. (X)SDR USAA990035Fairing · corrodedCLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION STA 1000 LEFT OF KEEL BEAM OF FAIRING FLANGE. REPAIRED PER SRM 53-50-12, PAGE 107. (X)SDR USAA990034Clip · crackedCLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK STA 1654.5 AND STR 30L AT TIE CLIP. REPAIRED PER SRM 51-10-00. (X)SDR USAA990033Seat Track · corrodedCLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION LT OUTBOARD SEAT TRACK STA 625 THROUGH STA 754. REPAIRED PER SRM 53-00-52, FIG 101, AND SRM 51-20-01 AND SRM 51-21-01. (X)SDR USAA990032Stringer · corrodedCLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION, 1 INCH, AT BS 1564 STR 37L. REPLACED STRINGER SECTION PER SRM 53-00-03 FIG 202. (X)SDR USAA990031Seat Track · corrodedCLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON SEAT TRACK STA'S 764, 777, 780, 795, 806, AND 814. REPLACED SEAT TRACK FROM STA 764 TO STA 814 PER SRM 51-10-00. REF: OPERATOR CONTROL NR 99ZZZX566 THROUGH 99ZZZX570. (X)SDR USAA990030Floorbeam · corrodedCLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM 1 INCH BY 79 INCHES AT STA 325 RBL 23 TO RBL 56. INSTALLED DOUBLER PER SRM 53-00-51 FIG 201. (X)
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