Boeing 767-201

Service difficulty reports · 660

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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.

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)Jun 8, 2000 · N647US · Boeing 767201 · Independent InstrumentsSDR 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 May 30, 2000 · N647US · Boeing 767201 · Flight Management Computing Hardware SystemSDR 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)May 30, 2000 · N647US · Boeing 767201 · Flight Management Computing Hardware SystemSDR 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 BOOSTMay 9, 2000 · N645US · Boeing 767201 · Fuel Boost PumpSDR 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)Apr 17, 2000 · N647US · Boeing 767201 · Fuselage Main, Plate/SkinSDR 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 RApr 16, 2000 · N647US · Boeing 767201 · Central WarningSDR 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 QUANApr 12, 2000 · N648US · Boeing 767201 · Hydraulic Quantity SensorSDR USAABB00034Charger · inoperativeCLT - FOUND FLOOR TRACK LIGHT INOPERATIVE FROM SEAT ROW 21 AFT. MAINTENANCE REPLACED THE BATTERY CHARGER ASSEMBLY. (M)Mar 12, 2000 · N647US · Boeing 767201 · Emergency LightingSDR 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)Mar 9, 2000 · N646US · Boeing 767201 · Door Warning SystemSDR 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)Mar 7, 2000 · N645US · Boeing 767201 · Directional Gyro and Indicating SystemSDR 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 FURTHERFeb 29, 2000 · N648US · Boeing 767201 · Flight Management Computing Hardware SystemSDR 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 INCIFeb 23, 2000 · N649US · Boeing 767201 · APU Cowling/ContainmentSDR 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 Feb 23, 2000 · N649US · Boeing 767201 · APU Cowling/ContainmentSDR 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)Feb 16, 2000 · N647US · Boeing 767201 · Emergency LightingSDR USAABB00017Power Supply · failedLGW - COULD NOT TURN EMERGENCY LIGHTS OFF. MAINTENANCE REPLACED THE TWO FORWARD AND TWO AFT POWER SUPPLIES. (M)Feb 10, 2000 · N647US · Boeing 767201 · Emergency LightingSDR 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 PANFeb 4, 2000 · N649US · Boeing 767201 · Hydraulic Power SystemSDR 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 OJan 18, 2000 · N650US · Boeing 767201 · Air Distribution SystemSDR 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 LDec 31, 1999 · N647US · Boeing 767201 · Hydraulic System, MainSDR USAABB99057Light Panel · malfunctionedPHL - CREW DISCOVERED A PROBLEM WITH THE EMERGENCY LIGHT PANEL. MAINTENANCE REPLACED THE PANEL. (X)Dec 20, 1999 · N649US · Boeing 767201 · Emergency LightingSDR 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 REPLANov 3, 1999 · N648US · Boeing 767201 · ATC Transponder SystemSDR 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)Oct 17, 1999 · N649US · Boeing 767201 · Electrical Power System WiringSDR 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)Sep 14, 1999 · N646US · Boeing 767201 · Door Warning SystemSDR 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 REJul 21, 1999 · N646US · Boeing 767201 · APU Engine Fuel and ControlSDR 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)May 18, 1999 · N650US · Boeing 767201 · Engine EGT/TIT Indicating SystemSDR 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 FLIGHTMay 18, 1999 · N650US · Boeing 767201 · Engine EGT/TIT Indicating SystemSDR 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)May 17, 1999 · N649US · Boeing 767201 · Fuselage Main, Floor BeamSDR 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)May 17, 1999 · N649US · Boeing 767201 · Fuselage Main, Floor BeamSDR 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)May 17, 1999 · N649US · Boeing 767201 · Fuselage Miscellaneous StructureSDR 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)May 17, 1999 · N649US · Boeing 767201 · Fuselage Main, Floor BeamSDR 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 May 15, 1999 · N648US · Boeing 767201 · Turbine Engine Oil SystemSDR 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)May 2, 1999 · N650US · Boeing 767201 · Engine StarterSDR 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)May 2, 1999 · N650US · Boeing 767201 · Engine Start Valves/ControlsSDR USAABB99021Battery Charger · inoperativePHL - FOUND LEFT FORWARD EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED BATTERY AND CHARGER. (M)Apr 30, 1999 · N648US · Boeing 767201 · Emergency LightingSDR 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)Apr 30, 1999 · N650US · Boeing 767201 · Fuselage Main, FrameSDR 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)Apr 30, 1999 · N650US · Boeing 767201 · Fuselage Main, Floor BeamSDR 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 EXMar 11, 1999 · N646US · Boeing 767201 · Landing Gear Position and WarningSDR 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 WFeb 3, 1999 · N650US · Boeing 767201 · Escape SlideSDR 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 BOTJan 26, 1999 · N649US · Boeing 767201 · Air Distribution SystemSDR 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)Jan 20, 1999 · N646US · Boeing 767201 · Fuselage, Seat/Cargo Attach FittingsSDR 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)Jan 20, 1999 · N646US · Boeing 767201 · Fuselage Miscellaneous StructureSDR 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)Jan 20, 1999 · N646US · Boeing 767201 · Fuselage Miscellaneous StructureSDR 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)Jan 20, 1999 · N646US · Boeing 767201 · Fuselage Main, Floor BeamSDR 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)Jan 20, 1999 · N646US · Boeing 767201 · Aerodynamic FairingsSDR 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)Jan 20, 1999 · N646US · Boeing 767201 · Fuselage, Seat/Cargo Attach FittingsSDR 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)Jan 20, 1999 · N646US · Boeing 767201 · Aerodynamic FairingsSDR 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)Jan 20, 1999 · N646US · Boeing 767201 · Fuselage Miscellaneous StructureSDR 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)Jan 20, 1999 · N646US · Boeing 767201 · Fuselage, Seat/Cargo Attach FittingsSDR 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)Jan 20, 1999 · N646US · Boeing 767201 · Fuselage Main, Longeron/StringerSDR 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)Jan 20, 1999 · N646US · Boeing 767201 · Fuselage, Seat/Cargo Attach FittingsSDR 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)Jan 20, 1999 · N646US · Boeing 767201 · Fuselage Main, Floor Beam
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