Boeing 767-322
Service difficulty reports · 11,768
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 = '767322' 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 = '767322' 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 2006UALA00448Bulkhead · crackedBS 1809 BULKHEAD RT SIDE, FWD OUTER CHORD, INBD FLANGE HAS A CRACK COMING OUT OF THE FASTENER HOLE. DAMAGE FOUND AS A RESULT OF ROUTINE INSPECTION, MANDATED PER AD 2005-11-02. REPAIRED PER AD REQUIREMENTS.SDR 2006UALA00569Pin · failedRT MAIN GEAR, LWR STRUT TO BOGIE ATTACH PIN SNAPPED.SDR 2006UALA00398Hinge Fitting · crackedLEFT INBD FLAP-CENTER HINGE FITTING CRACKED ON INBD AND OTBD FLANGES. THE SUBJECT HINGE FITTING WAS FOUND CRACKED ON THE INBOARD AND OUTBOARD FLANGE. REPAIRED PER 767-300 STRUCTURAL REPAIR MANUAL 57-53-02.SDR 2006UALA00397Seat Track · brokenMAIN SEAT TRACK OUTBD LT SIDE STA 786-808, LBL 88 INBD NODES BROKEN OFF FROM TRACK. DAMAGED SEAT TRACK REMOVED/REPLACED PER SRM.SDR 2006UALA00354Floorbeam · corrodedAFT PIT FLOORBEAM AT STA 1197+132 BETWEEN STR 33R TO 33L IS CORRODED AT 6 LOCATIONS. CORRODED FLOORBEAM REPAIRED PER SRM. DAMAGE FOUND BY ROUTINE INSPECTION.SDR 2006UALA00353Floorbeam · corrodedAFT PIT FLOORBEAM AT STA 1197 BTWN STR 33L- 33R IS CORRODED TOP AND BOTTOM OF T-CAP, SEVERAL LOCATIONS. CORRODED FLOORBEAM REPAIRED PER SRM. DAMAGE FOUND BY ROUTINE INSPECTION.SDR 2006UALA01158Latch · failedLT O/W LATCH SYS INTEGRATOR FAILS TORQUE CHECK. REPLACED LATCHES (LT) IAW 767 MM25-65-98.SDR 2006UALA00419Flap Track · shearedFRACTURE OF LT OTBD T/E FLAP DETECTION CONTROL TRACK. LT OTBD T/E FLAP DEFLECTION CONTROL TRACK IS COMPLETELY SHEARED JUST AFT OF TIE ROD SUPPORT LUG. PER BOEING, THIS TYPE OF INCIDENT IS UNUSUAL, BUT NOT UNCOMMON. BOEING HAS RELEASE SB 767-27-0184 TO EXAMISDR 2006UALA00541Track · separatedLEFT OUTBOARD FLAP DEFLECTION CONTROL TRACK HAS SEPARATED AT FWD END.SDR 2006UALA01157Housing · crackedLEFT OVERWING SLIDE DISCONNECT HOUSING CRACKED. REMOVE AND REPLACE DISCONNECT HOUSING IAW B767 MM25-65-98.SDR 2006UALA00257Bushing · migratedNR 2 ENG PYLON INBOARD MIDSPAR FITTING OUTBOARD LUG BUSHING MIGRATED. NR 2 ENG PYLON INBD MIDSPAR FITTING OUTBD LUG BUSHING WAS FOUND MIGRATED. 4 EACH MIDSPAR BUSHINGS WERE FABRICATED PER SRM 54-53-90, REPAIR 3 & REPLACED PER GN-MM 01-0- 01-013.SDR 2006UALA00256Attach Angle · crackedFLOORBEAM TO WEB ATTACH ANGLE AT BS 246 APPROX LBL 48, COCKPIT ENTRY STEP IS CRACKED. CRACKED ANGLE REPLACED PER SRM. ANGLE FOUND DURING ROUTINE INSPECTION PROGRAM PER BOEING SERVICE BULLETIN 767-53-0093.SDR 2006UALA00255Stiffener · gougedL-1 DOOR CABLE HAS RUBBED A DEEP GOUGE IN FRAME STIFFENER AFT SIDE OF BS 303 FRAME AT STR 1R. GOUGED SUPPORT MEMBER REPLACED AND INSTALLED PER SRM.SDR 2006UALA00254Frame · corrodedAFT PIT FLOOR FRAME UPPER CHORD AT BS 1153, LBL 24 TO RBL 18 CORRODED ON TOP AND BOTTOM SURFACES. CORRODED FRAME ASSY PIECES REPLACED AND SPLICED PER SRM.SDR 2006UALA00321Warning Horn · activatedFLIGHT DIVERTED DUE TO CONTINUOUS TAKEOFF CONFIGURATION WARNING HORN. RESET CB'S AND WEU PSU'S. ACCOMPLISHED CHECKS PER MM 31-51-00 FIG 103: NO FAULTS NOTED. FOUND CAUSE TO BE FLAT NOSE GEAR STRUT CAUSING NOSE AIR GROUND SENSORS/SWITCHES S266 & S244 TO REMAISDR 2006UALA00200Seat Track · corrodedSEAT TRACK IN MAIN CABIN HAS AREAS OF GOUGES AND CORROSION STA 1197 + 142 TO 1213, 88 RBL. GOUGED SECTIONS OF SEAT TRACK REPLACED WITH NEW, PER SRM.SDR 2006UALA00199Seat Track · corrodedMAIN CABIN STA 1087, SEAT TRACK RBL 88 IS CORRODED. A 20 INCH SECTION OF CORRODED SEAT TRACK REPLACED WITH NEW, PER SRM.SDR 2006UALA00182Seat Track · gougedAFT CABIN SEAT TRACK GOUGED STA 1302 - 1325 LBL 11. SECTION OF AFT CABIN SEAT TRACK GOUGED BY UNKNOWN ORIGIN. REPAIRED PER SRM.SDR 2006UALA01186Latch · wornNR 3 LATCH EDGE MARGIN BEYOND LIMITS. REMOVED AND REPLACED NR 3 LATCH IAW B767 MM 25-65-98.SDR 2006UALA00184Bearing · brokenBROKEN TIE BAR BEARINGS. BEARING FAILURES FREQUENTLY OCCUR. BROKEN BEARINGS WERE REPLACED.SDR 2006UALA00085Pump · failedRETURNED TO SFO DUE TO RIGHT ENGINE FUEL FILTER EICAS MESSAGE. REMOVED AND REPLACED NR 2 ENGINE DRIVEN FUEL PUMP. SHOP TEARDOWN REVEALED THAT THE PUMP HAD INTERNAL DAMAGE AS THE RESULT OF A MISSING THRUST WASHER. ALTHOUGH IT COULD NOT BE PROVEN CONCLUSIVELYSDR 2006UALA00063Bearing · brokenTUBE MISSING 7 BROKEN BEARINGS. THIS TYPE OF EVENT HAS OCCURRED PREVIOUSLY AND HAS BEEN REPORTED TO BOEING FOR RESOLUTION. BOEING IS WORKING TO DEVELOP A NEW, MORE RUGGED BEARING. STRESS OVERLOAD FROM UNKNOWN CAUSE. PACKBOARD REMOVED AND REPLACED.SDR 2006UALA01178Latch · failedRT OVERWING COMPT DOOR LATCHES FAILED TORQUE CHECK. REPLACED LATCHES. IAW B767, MM 25-65-98.SDR 2006UALA01185Latch · wornNR 3 LATCH EDGE MARGIN BEYOND LIMITS. REPLACED LATCH, IAW B767 MM 25-65-98.SDR 2006UALA00609Slat · malfunctionedDIVERTED TO HNL DUE TO LEADING EDGE SLAT ASYMMETRY PROBLEM. FAILURE DUE TO A CRACKED 90 DEGREE CONDUIT.SDR 2005UALA01501Wire · brokenDIVERTED DUE TO LEADING EDGE SLAT ASYMMETRY EICAS. FOUND SLAT SKEW SWITCH WIRING FAILED AT RT WING TIP, STA 1107. CAUSE OF WIRING FAILURE WAS BROKEN 90 DEG CONDUIT ELBOW.SDR 2005UALA01527Warning Light · illuminatedRETURNED TO FIELD DUE TO LEFT BLEED OVERHEAT INDICATION. THE WING DUCT LEAK DETECTORS TS211 & TS212 WERE REPLACED. DURING TROUBLESHOOTING THE SENSOR THAT WAS CAUSING THE FAULT COULD NOT BE DETERMINED SO BOTH WERE REPLACED. THE REMOVED PARTS ARE NON-STOCK, NO FSDR 2005UALA01526Sensor · dirtyFLIGHT RETURNED TO FIELD DUE TO A DOOR 1-R ARMING INDICATION. FOUND DEBRIS AROUND SENSOR CLEANED AREA AND CYCLED DOOR, NO DEFECTS NOTED.SDR 2005UALA01495Bushing · corrodedNR 1 PYLON UPPER LINK FITTING, OUTBOARD LUG REQUIRES REWORK DUE TO INBOARD LUG REWORKED. BUSHING REPLACEMENT DUE CORRODED BUSHING. BOTH LUGS MUST BE REWORKED AS A PAIR. REWORKED AND BUSHINGS WERE REPLACED DUE TO CORROSION. BUSHINGS WERE REPLACED PER SRM 54SDR 2005UALA01494Skin · crackedNR 1 PYLON INBOARD FWD STRUT SKIN CRACKED AT PANEL 416BR CUTOUT RADIUS. IT WAS PROBABLY CAUSED BY FATIGUE. THE SKIN WAS REPAIRED PER SRM 54-53-01 WITH -1 AND -2 DOUBLERS.SDR 2005UALA01450Bushing · wornNR 1 PYLON UPPER LINK FITTING, INBOARD LUG, OUTBOARD BUSHING LIP FRETTED. NR 1 PYLON UPPER LINK FITTING, INBD LUG, OUTBD BUSHING LIP FRETTED. IT WAS PROBABLY CAUSED BY TOLERANCE BUILD UP. BUSHING WAS REPLACED PER SRM 54-51-93.SDR 2005UALA01449Bushing · rotatedNR 1 PYLON DIAGONAL BRACE FITTING AT STRUT ATTACH, FWD INBOARD AND OUTBOARD BUSHINGS HAS EVIDENCE OF ROTATION IN THE BORE. NR 1 PYLON DIAGONAL BRACE FITTING AT STRUT ATTACH, FWD INBD AND OUTBD BUSHINGS HAVE EVIDENCE OF ROTATION IN THE BORE. MIGRATION CAUSE IS SDR 2005UALA01448Bushing · looseNR 2 PYLON OUTBOARD MIDSPAR FITTING, INBOARD LUG BUSHING MOVES IN BORE. NR 2 PYLON OUTBD MIDSPAR FITTING, INBD LUG BUSHING MOVED IN THE BORE. BUSHING MIGRATION CAUSE IS UNKNOWN. IT WAS REPLACED WITH AN OVERSIZED BUSHING PER SRM 54-53-90SDR 2005UALA01430Skin · gougedFUSELAGE DENTED AND GOUGED FWD OF AFT CARGO PIT CONTROL PANEL DOOR. FUSELAGE SKIN REPAIRED PER SRM. SUPPLEMENTAL INSPECTIONS REQUIRED BY 37,500 CYCLES ARE MONITORED BY AMIS CF9010.SDR 2005UALA01423Bushing · migratedNR 2 PYLON DIAGONAL BRACE FITTING FWD-STRUT ATTACH, INBD SIDE BUSHING IS MIGRATED. NR 2 PYLON DIAGONAL BRACE FITTING FWD-STRUT ATTACH, INBD SIDE BUSHING WAS MIGRATED. BUSHING MIGRATION CAUSE IS UNKNOWN. THE BUSHING WERE REPLACED PER SRM 54-53-90.SDR 2005UALA01422Bushing · migratedNR 1 PYLON OUTBD MIDSPAR FITTING OUTBD LUG, BUSHING IS MIGRATED. NR 1 PYLON OUTBD MIDSPAR FITTING OUTBD LUG, BUSHING WAS MIGRATED. THE BUSHING MIGRATION IS UNKNOWN. IT WAS REPLACED PER SRM 54-53-90.SDR 2005UALA01421Bushing · migratedNR 1 PYLON INBD MIDSPAR FITTING, INBD AND OUTBD LUG BUSHINGS MIGRATED. NR 1 PYLON INBD MIDSPAR FITTING, INBD AND OUTBD LUG BUSHINGS WERE MIGRATED. CAUSE OF BUSHING MIGRATIONS IS UNKNOWN. BUSHINGS WERE REPLACED PER MM 54-53-90.SDR 2005UALA01420Frame · corrodedFRAME TOP CAP CORRODED AT BS 654+121, LBL42, FWD CARGO PIT. MAJOR REPAIR TO FRAME TOP CAP PER SRM AS PERMANENT REPAIR.SDR 2005UALA01409Bracket · crackedLT WING KRUEGER FLAP INBD OF NR 1 PYLON, ROTARY ACTUATOR OUTBD SUPPORT BRACKET IS BUCKLED AND CRACKED. BRACKET FAILURE WAS DUE TO FATIGUE. PART WAS REPLACED.SDR 2006UALA00570Pin · failedLEFT MAIN GEAR STRUT PIVOT PIN TO BOGIE SNAPPED.SDR 2005UALA01405Spacer · burnedBURNED SPACER BLOCKS BETWEEN APU GENERATOR 3 CABLES. FAILING SPLICE INSTALLATIONS REVEALED A MISMATCH BETWEEN THE SPLICE AND CRIMPER USED. MANUFACTURERS' SPLICES AND CRIMPER DIES MUST BE USED AS A MATCHED SET; IF NOT, AN INCOMPLETE SWAGE WILL RESULT IN HEAT GSDR 2005UALA01318Slide · unserviceableDAMAGED BEARINGS. THIS TYPE OF EVENT HAS HAPPENED BEFORE AND BOEING IS WORKING ON IMPROVED FABRICATION MATERIALS TO ADDRESS THIS CONDITION. SLIDE WAS REMOVED FROM THE AIRCRAFT AND SENT TO THE COMPONENT SHOP WHERE BEARINGS WERE REPLACED.SDR 2005UALA01276Light · brokenFOUND SEAT MOUNTED EMERGENCY AISLE LIGHTS BROKEN AT SEATS 28AB AND 29HJ. REPLACED EMERGENCY LIGHT ASSY.SDR 2005UALA01257Skin · lightning strikeLIGHTNING STRIKE AT LEFT FUSELAGE STA 1587 JUST AFT OF PRESSURE BULKHEAD. *S/D* LIGHTNING STRIKE DAMAGE CUT OUT AND REPAIRED PER SRM.SDR 2005UALA01247Spar · crackedLEFT WING FRONT SPAR IS CRACKED, PUNCTURED AT NR 1 LEADING EDGE SLAT, INBD AUX TRACK. DETERMINED SLAT SENSOR TARGET WAS PREVIOUSLY INSTALLED 180 DEGREES OUT, CAUSING DAMAGE. LEFT WING FRONT SPAR WAS FOUND CRACKED, PUNCTURED AT THE NR 1 LEADING EDGE SLAT, INBSDR 2005UALA01238Angle · crackedNR 1 PYLON MID SPAR AT STA 233.120 RT SIDE, ANGLE IS CRACKED AT THE 2ND FROM INBOARD ATTACH FASTENER. NR 1 PYLON MID SPAR P/N 311T3157-1 AT STA 233.120 RT SIDE, ANGLE IS CRACKED AT THE 2ND FROM INBOARD ATTACH FASTENER, VERIFIED WITH HFEC. THIS IS THE CLOSE-OSDR 2005UALA01239Angle · crackedLEFT WING, LEFT PYLON, AFT BULKHEAD, LOWER OUTBOARD ANGLE CRACKED. *S/D* THE LEFT WING LEFT PYLON, AFT BULKHEAD LOWER OUTBOARD ANGLE WAS FOUND CRACKED ON A/C 6768 DURING A C-CHECK VISIT. CRACK IS DUE TO FATIGUE. CRACKED ANGLE WAS REPLACED AND INSTALLED PERSDR 2005UALA01245Wire · burnedEMPENNAGE INSIDE AT BS 1809 RT SIDE BELOW CENTER HORIZONTAL STAB FEEDER WIRE BUNDLES, INSULATION NOT SECURE, LOOSE ON APU FEEDER SPLICES AND FEEDER WIRES FOUND BURNT. *S/D* THE FEEDER WIRE, SPLICE AND CONNECTOR WERE REPLACED.SDR 2005UALA01243Switch · failedFLIGHT DIVERTED DUE TO LOST RIGHT PACK. FOUR UNITS WERE REMOVED DUE TO THIS EVENT: HIGH PRESSURE SHUTOFF VALVE AND PRESSURE REGULATING VALVE (HPSOV/PRV, P/N: 790270-4/-14), HIGH PRESSURE CONTROLLER (HPC, P/N: 773289-15) AND PRESSURE REGULATING VALVE CONTROLLSDR 2005UALA01244Wire Harness · burnedWIRE BUNDLE W1402 HAS BURNT WIRES IN FORWARD PIT AT STA 654 -PDU WIRE BUNDLE. DAMAGED CARGO LOADING SYSTEM WIRES REPAIRED PER SWPM 20-10-13 AND OPS CHECK GOOD PER MM 25-53-01. CAUSE SUSPECTED TO BE METAL SHAVINGS PRODUCING AN ELECTRICAL SHORT AT BURN LOCATIO
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