Boeing 767-277
Service difficulty reports · 253
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 = '767277' 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 = '767277' 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 AU010297Fitting · cracked(AUS) RT WING PYLON ATTACHMENT FITTING OUTBOARD LUG CRACKED. CRACK PENETRATES THE FULL THICKNESS OF THE LUG AND EXTENDSAPPROXIMATELY 25.4MM (1IN) ALONG THE INBOARD FACE AND APPROXIMATELY 12.7MM (0.5IN) ALONG THE OUTBOARD FACE. FOUND USING EDDY CURRENT INSPECTISDR AUS20010865Valve · cracked(AUS) RAM AIR TURBINE (RAT) MODULE CHECK VALVE CRACKED. LOSS OF HYDRAULIC FLUID. INVESTIGATION FOUND THAT THE HEX HEAD SEPARATEDFROM THE CHECK VALVE BODY DUE TO A FRACTURE BETWEEN THE UPPER O' RING GROOVE AND THE INTERNAL BODY THREAD RELIEF.SDR AUS20010774Valve · cracked(AUS) RAM AIR TURBINE (RAT) MODULE LEAKING DUE TO CRACKED CHECK VALVE.SDR AUS20010862Frame · cracked(AUS) RT BULKHEAD OUTER CHORD LOCATED AT BS1809.5 CRACKED IN AREA OFLOWER TWO FASTENERS IN INSPECTION AREA 1.SDR AU010109Fitting · corroded(AUS) LT AND RT MAIN LANDING GEAR SIDE STRUT SWIVEL ASSEMBLY FITTINGS COORODED IN AREA BENEATH BUSHING FLANGE.SDR AU001023Warning System · faulty(AUS) LT ENGINE FIRE WARNING. A THOROUGH INVESTIGATION OF THE FIRE WARNING SYSTEM COULD FIND NO FAULTS AND THE SYSTEM HAS OPERATED CORRECTLY SINCE. DEFECT NOT CONFIRMED.SDR AU001073Bearing · collapsed(AUS) NR 7 MAIN WHEEL INNER BEARING COLLAPSED. INVESTIGATION FOUND THAT DURING THE LAST WHEEL CHANGE, THE INBOARD WHEEL SPACER WAS NOTREFITTED TO THE AXLE DUE TO THE SPACER COMING OFF WITH THE WHEEL. PERSONNEL/MAINTENANCE ERROR.SDR AU001066Pin · cracked(AUS) LT ENGINE PYLON MIDSPAR INBOARD FUSE PIN CRACKED. CRACK LENGTH APPROXIMATELY 14MM (0.55IN). FOUND DURING EDDY CURRENT INSPECTION.SDR AU000735Housing · corroded(AUS) RT MAIN LANDING GEAR SIDE STRUT SWIVEL HOUSING CORRODED IN THEAREA OF THE BUSHING FLANGE. DEPTH OF CORROSION 0.127MM (0.005IN).SDR AU000734Skin · corroded(AUS) AIRCRAFT SKIN CORRODED BENEATH PAINT LOCATED AFT OF STN 287 AND BELOW STRINGER NR 24. AREA OF CORROSION 50MM BY 50MM (1.968IN BY 1.968IN) AND 2.032MM (0.080IN) DEEP.SDR AU000803Actuator · failed(AUS) RT MAIN LANDING GEAR DRAG BRACE ACTUATOR PISTON ROD PN 273T6034-1 FRACTURED IN THREADED END.SDR AU000890Actuator · faulty(AUS) RUDDER TRIM ACTUATOR FAULTY. WORKSHOP INVESTIGATION COULD FIND NO FAULTS.SDR AU000801Actuator · corroded(AUS) NR 11 LEADING EDGE SLAT INBOARD ROTARY ACTUATOR INTERNALLY CORRODED. RING GEAR SEAL MISSING.SDR AU000579Pin · sheared(AUS) NOSE LANDING GEAR STEERING SYSTEM RT METERING VALVE INDEXING PINSHEARED. WORKSHOP FOUND EVIDENCE OF HEAVY CORROSION AROUND THEPIN LOCATION HOLE.SDR AU000804Fuse · cracked(AUS) OUTBOARD HYDRAULIC FUSE ON BRAKE MODULE CRACKED IN VALVE BODY. VALVE IS LOCATED AT THE WING TRAILING EDGE OUTBOARD OF THE LT MAIN LANDING GEAR. LOSS OF RT HYDRAULIC SYSTEM FLUID.SDR AU000516Controller · faulty(AUS) LT WING NR 3 SPOILER VIBRATING UP TO 52.8MM (2IN) FROM THE SELECTED POSITION. WORKSHOP INVESTIGATION FOUND THE SPOILER CONTROL MODULE FAULTY.SDR AU000517Web · cracked(AUS) PARK BRAKE INPUT CRANK ASSEMBLY SUPPORT WEB CRACKED. SUSPECTPARKING BRAKE MECHANISM INCORRECTLY RIGGED CAUSING FLEXING OF THE WEB.SDR AU000450Housing · eroded(AUS) MAIN FORWARD FUEL TANK LEFT BOOST PUMP FAILED. INVESTIGATION FOUND PIECES OF METAL SEPARATED FROM THE HOUSING INLET STRUTS JAMMING THE CHECK VALVE PARTIALLY OPEN.SDR AU000386Gear · stripped(AUS) TRAILING EDGE FLAP DRIVE GEARBOX INPUT GEAR STRIPPED.SDR AU000891Inverter · faulty(AUS) STANDBY STATIC INVERTER FAULTY. WORKSHOP INVESTIGATION FOUND THAT TRANSISTORS Q3 TO Q10 WERE SHORT CIRCUITED OR OPEN CIRCUITED WITH THE BASE BIAS RESISTORS BLOWN OPEN.SDR AU000987Circuit Board · burned(AUS) MASTER DIM AND TEST PRINTED CIRCUIT BOARD M2 IN PANEL P29 BURNED.SDR AU000177Arm · corroded(AUS) DO 11 LEADING EDGE SLAT INBOARD ROTARY ACTUATOR CORRODED INTERNALLY BENEATH BEARING.SDR AU000072Bearing · seized(AUS) RT OUTBOARD AILERON POWER CONTROL ACTUATOR INPUT LINK BEARING SEIZED.SDR AU000193Spar · corroded(AUS) RT WING CENTRE SECTION REAR SPAR WEB CORRODED IN THE AREA LOCATED BEHIND THE REAR SPAR BULKHEAD FITTING PNO 145T2521. AREA OF CORROSION APPROXIMATELY 215.9MM (8.5IN) BY 38.1MM (2.5IN) BY2.54MM (0.100IN) DEEP.SDR AU000079Skin · corroded(AUS) RT WING LOWER SKIN PANEL LOCATED AT WS391 CORRODED. AREA OF CORROSION 76.2MM BY 38.1MM (3IN BY 1.5IN). DEPTH OF CORROSION3.556MM (0.140IN).SDR AU000076Wedge · contaminated(AUS) LEADING EDGE SLAT TRAILING EDGE WEDGES CORRODED INTERNALLY & CONTAMINATED WITH MOISTURE.SDR AU991092Bracket · broken(AUS) RIGHT ENGINE BLEED AIR DUCT SUPPORT BRACKET BROKEN. SUSPECT BROKEN BRACKET CAUSED BLEED AIR DUCT TO FAIL. SEE MDR AU991091.SDR AU991091Duct · burst(AUS) RIGHT ENGINE HP AIR DUCT ELBOW RUPTURED.SDR AU990844Sensor · out of adjust(AUS) RIGHT ENGINE THRUST REVERSER LOCK PROXIMITY SENSOR OUT OF ADJUSTMENT.SDR AU991038Rod · out of adjust(AUS) OUTBOARD SLAT PDU INPUT ROD OUT OF ADJUSTMENT.SDR AU990494Cover · cracked(AUS) RT LATERAL CENTRAL CONTROL ACTUATOR FILTER COVER `O' RING SEAL DISPLACED. LOSS OF CENTER HYDRAULIC SYSTEM FLUID. INVESTIGATION FOUND THAT THE FILTER COVER CONTAINED A CIRCUMFERENTIAL CRACK INTHE THREADED PORTION EXPOSING THE SEAL TO HYDRAULIC PRESSURE SDR AU990471Valve · failed(AUS) RAM AIR TURBINE CHECKOUT MODULE CHECK VALVE FAILED. LOSS OF CENTER HYDRAULIC SYSTEM FLUID.SDR AU990293Pin · cracked(AUS) RIGHT INBOARD ENGINE PYLON MID-SPAR FUSE PIN CRACKED. CRACK LENGTH 11 MM (0.433 INCH). FOUND DURING EDDY CURRENT INSPECTION.SDR AU981610Wedge · disbonded(AUS) LEADING EDGE SLAT TRAILING EDGE WEDGES FOUND DISBONDED ON A TOTAL OF EIGHT SLATS: SLAT 3 - P/N 114T4103-25P, 8 DISBONDED AREAS. SLAT 4 - P/N 114T4104-21C, 1 DISBONDED AREA. SLAT 5 - P/N 114T4105-37, 1 DISBONDED AREA. SLAT 6 - P/N 114T3100-1A, 2 DISBOSDR AU981476Line · damaged(AUS) NOSE LANDING GEAR `DOWN' TITANIUM HYDRAULIC PIPE LOCATED AT FS 625 BETWEEN THE FORWARD CARGO HOLD LEFT SIDEWALL AND THE FUSELAGE SKIN DENTED AND CRACKED. LEAKING HYDRAULIC FLUID MIST IN CABIN. PIPE HAD BEEN DAMAGED DUE TO PREVIOUS MAINTENANCE. PART SDR AU981210Fitting · cracked(AUS) LEFT WING DEFLECTION CONTROL SUPPORT FITTING LOWER ATTACHMENT LUG FRACTURED THROUGH THE BEARING HOUSING. FITTING IS LOCATED AT WS 906.20. PART TC: 41,421.SDR AU981209Fitting · corroded(AUS) LEFT PYLON CONTAINED EXFOLIATION CORROSION ON THE UPPER SURFACES OF THE UPPER WEB OF THE TORQUE BOX ADJACENT TO THE UPPER LINK ATTACHMENT BEAM OUTBOARD OF AND RUNNING UNDER THE STRUT FITTING. CORROSION HAD PENETRATED TO A DEPTH OF 1.778 MM (0.070 INCH) SDR AU981208Fitting · corroded(AUS) RIGHT PYLON CONTAINED EXFOLIATION CORROSION ON THE UPPER SURFACES OF THE UPPER WEB OF THE TORQUE BOX ADJACENT TO THE UPPER LINK ATTACHMENT BEAM EITHER SIDE OF AND RUNNING UNDER THE FORWARD UPPER STRUT FITTING. CORROSION HAD PENETRATED THROUGH THE WEB WISDR AU980787Collar · cracked(AUS) LEFT INBOARD FLAP INBOARD TORQUE TUBE COLLAR CRACKED AND TORQUE TUBE HEAVILY CORRODED. RIGHT SIDE FLAP COLLARS AND TORQUE TUBE ALSO CORRODED. PART TOTAL CYCLES: 39,633.SDR AU980532Pdu · faulty(AUS) OUTBOARD LEADING EDGE SLAT POWER DRIVE UNIT (PDU), ELECTRIC MOTOR FAULTY.SDR AU980821Pin · cracked(AUS) LT ENGINE MID SPAR INBOARD FUSE PIN INNER BORE CONTAINED TWO LONGITUDINAL CRACKS. TOTAL CRACK LENGTH 8.89 MM (0.35 INCHES). FOUND DURING EDDY CURRENT INSPECTION IAW ER B76-54-40-4I.SDR AU971644Actuator · failed(AUS) LH MAIN LANDING GEAR LEFT HAND DRAG BRACE ACTUATOR PISTON ROD SHEARED IN THREADED AREA.SDR AU971566Piston Seat · fractured(AUS) AFTER TAKE-OFF, THE GEAR DOOR DISAGREE MESSAGE WARNING DISPLAYED AND EXCESSIVE NOSE GEAR VIBRATIONS WERE FELT DURING GEAR RETRACTION. GROUND INVESTIGATION FOUND THAT THE NLG PRIORITY VALVE'S PISTON SEAT ASSEMBLY PNO 01715201B2-1 HAD FRACTURED PREVENTINGSDR AU971595Spring · fractured(AUS) HYDRAULIC SYSTEM RH FUSE PNO V2-4360-2 SPRING PNO 33582 FAILED. SPLIT RING PNO 33581 DAMAGED AND RESET PISTON PNO 33589 JAMMED INSIDE ADAPTER PNO 33590.SDR AU970481Hydraulic Fuse · faulty(AUS) RH MAIN LANDING GEAR TRUCK POSITIONER `UP' LINE HYDRAULIC FUSE FAULTYSDR AU970455Fuselage · corroded(AUS) FUSELAGE CONTAINED LEVEL 2 CORROSION - FOUND DURING INSPECTIONSDR AU960897Cylinder · cracked(AUS) RH MAIN LANDING GEAR OUTER CYLINDER AFT TRUNNION CRACKED AND CORRODED IN AREA OF FILLET SEALSDR AU960898Cylinder · cracked(AUS) RH MAIN LANDING GEAR OUTER CYLINDER AFT TRUNNION CRACKED AND CORRODED IN AREA OF FILLET SEALSDR AU960570Trunnion · corroded(AUS) LH AND RH MAIN LANDING GEAR OUTER CYLINDER AFT TRUNNIONS CONTAINED UNACCEPTABLE CORROSION DURING ULTRASONIC AND EDDY CURRENT INSPECTIONS IAW ER B76-32-10-24 - RH OUTER CYLINDER CORRODED IN AREA OF JOURNAL CHAMFER AT THE 2 O'CLOCK POSITION -LH TRUNNION CSDR AU960177Wire · damaged(AUS) WIRES DAMAGED IN AREA BEHIND FLIGHT ENGINEERS PANEL - WIRES DAMAGED WERE:- 1. SINGLE TWISTED WIRE WITH TWO WIRES SEVERED - P61 RH SIDE PANEL WIRE NO W062-209R18 - FUEL TEMPERATURE INDICATOR - ATA 28 WIRE NOW062-209R18 - FUEL TEMPERATURE INDICATOR - ATA
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