Boeing 767-277

Service difficulty reports · 253

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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 = '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.

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 INSPECTIApr 6, 2001 · Boeing 767277 · Wing, Nacelle/Pylon Attach FittingsSDR 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.Mar 23, 2001 · Boeing 767277 · Hydraulic System, AuxiliarySDR AUS20010774Valve · cracked(AUS) RAM AIR TURBINE (RAT) MODULE LEAKING DUE TO CRACKED CHECK VALVE.Mar 23, 2001 · Boeing 767277 · Hydraulic System, AuxiliarySDR AUS20010862Frame · cracked(AUS) RT BULKHEAD OUTER CHORD LOCATED AT BS1809.5 CRACKED IN AREA OFLOWER TWO FASTENERS IN INSPECTION AREA 1.Feb 1, 2001 · Boeing 767277 · Fuselage Main, FrameSDR AU010109Fitting · corroded(AUS) LT AND RT MAIN LANDING GEAR SIDE STRUT SWIVEL ASSEMBLY FITTINGS COORODED IN AREA BENEATH BUSHING FLANGE.Jan 23, 2001 · Boeing 767277 · Landing Gear Retraction/Extension SystemSDR 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.Sep 20, 2000 · Boeing 767277 · Fire DetectionSDR 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.Sep 16, 2000 · Boeing 767277 · Wheel/Ski/FloatSDR AU001066Pin · cracked(AUS) LT ENGINE PYLON MIDSPAR INBOARD FUSE PIN CRACKED. CRACK LENGTH APPROXIMATELY 14MM (0.55IN). FOUND DURING EDDY CURRENT INSPECTION.Sep 7, 2000 · Boeing 767277 · Nacelle/Pylon, Attach FittingsSDR 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).Sep 1, 2000 · Boeing 767277 · Landing Gear Retraction/Extension SystemSDR 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.Sep 1, 2000 · Boeing 767277 · Fuselage Main, Plate/SkinSDR AU000803Actuator · failed(AUS) RT MAIN LANDING GEAR DRAG BRACE ACTUATOR PISTON ROD PN 273T6034-1 FRACTURED IN THREADED END.Jul 31, 2000 · Boeing 767277 · Landing Gear ActuatorSDR AU000890Actuator · faulty(AUS) RUDDER TRIM ACTUATOR FAULTY. WORKSHOP INVESTIGATION COULD FIND NO FAULTS.Jul 24, 2000 · Boeing 767277 · Rudder Tab Control SystemSDR AU000801Actuator · corroded(AUS) NR 11 LEADING EDGE SLAT INBOARD ROTARY ACTUATOR INTERNALLY CORRODED. RING GEAR SEAL MISSING.Jul 15, 2000 · Boeing 767277 · Leading Edge Slat ActuatorSDR AU000579Pin · sheared(AUS) NOSE LANDING GEAR STEERING SYSTEM RT METERING VALVE INDEXING PINSHEARED. WORKSHOP FOUND EVIDENCE OF HEAVY CORROSION AROUND THEPIN LOCATION HOLE.Jul 7, 2000 · Boeing 767277 · Steering UnitSDR 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.Jun 21, 2000 · Boeing 767277 · Hydraulic System, MainSDR 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.Jun 4, 2000 · Boeing 767277 · Drag Control SystemSDR AU000517Web · cracked(AUS) PARK BRAKE INPUT CRANK ASSEMBLY SUPPORT WEB CRACKED. SUSPECTPARKING BRAKE MECHANISM INCORRECTLY RIGGED CAUSING FLEXING OF THE WEB.May 27, 2000 · Boeing 767277 · Fuselage Miscellaneous StructureSDR 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.May 20, 2000 · Boeing 767277 · Fuel Boost PumpSDR AU000386Gear · stripped(AUS) TRAILING EDGE FLAP DRIVE GEARBOX INPUT GEAR STRIPPED.Apr 20, 2000 · Boeing 767277 · Trailing Edge Flap ActuatorSDR 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.Mar 16, 2000 · Boeing 767277 · AC InverterSDR AU000987Circuit Board · burned(AUS) MASTER DIM AND TEST PRINTED CIRCUIT BOARD M2 IN PANEL P29 BURNED.Mar 10, 2000 · Boeing 767277 · Passenger Compartment LightingSDR AU000177Arm · corroded(AUS) DO 11 LEADING EDGE SLAT INBOARD ROTARY ACTUATOR CORRODED INTERNALLY BENEATH BEARING.Feb 23, 2000 · Boeing 767277 · Leading Edge Slat ActuatorSDR AU000072Bearing · seized(AUS) RT OUTBOARD AILERON POWER CONTROL ACTUATOR INPUT LINK BEARING SEIZED.Feb 2, 2000 · Boeing 767277 · Aileron Control SystemSDR 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.Jan 31, 2000 · Boeing 767277 · Wing SparSDR 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).Jan 28, 2000 · Boeing 767277 · Wing, Plate/SkinSDR AU000076Wedge · contaminated(AUS) LEADING EDGE SLAT TRAILING EDGE WEDGES CORRODED INTERNALLY & CONTAMINATED WITH MOISTURE.Jan 14, 2000 · Boeing 767277 · Leading Edge DevicesSDR AU991092Bracket · broken(AUS) RIGHT ENGINE BLEED AIR DUCT SUPPORT BRACKET BROKEN. SUSPECT BROKEN BRACKET CAUSED BLEED AIR DUCT TO FAIL. SEE MDR AU991091.Sep 12, 1999 · Boeing 767277 · Engine Bleed Air SystemSDR AU991091Duct · burst(AUS) RIGHT ENGINE HP AIR DUCT ELBOW RUPTURED.Sep 12, 1999 · Boeing 767277 · Engine Bleed Air SystemSDR AU990844Sensor · out of adjust(AUS) RIGHT ENGINE THRUST REVERSER LOCK PROXIMITY SENSOR OUT OF ADJUSTMENT.Jul 31, 1999 · Boeing 767277 · Engine Thrust ReverserSDR AU991038Rod · out of adjust(AUS) OUTBOARD SLAT PDU INPUT ROD OUT OF ADJUSTMENT.Jun 22, 1999 · Boeing 767277 · Leading Edge Slat Control SystemSDR 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 May 24, 1999 · Boeing 767277 · Hydraulic System, MainSDR AU990471Valve · failed(AUS) RAM AIR TURBINE CHECKOUT MODULE CHECK VALVE FAILED. LOSS OF CENTER HYDRAULIC SYSTEM FLUID.May 9, 1999 · Boeing 767277 · Hydraulic System, AuxiliarySDR AU990293Pin · cracked(AUS) RIGHT INBOARD ENGINE PYLON MID-SPAR FUSE PIN CRACKED. CRACK LENGTH 11 MM (0.433 INCH). FOUND DURING EDDY CURRENT INSPECTION.Mar 24, 1999 · Boeing 767277 · Nacelle/Pylon, Attach FittingsSDR 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 DISBOOct 31, 1998 · Boeing 767277 · Leading Edge DevicesSDR 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 Oct 9, 1998 · Boeing 767277 · Hydraulic System, MainSDR 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.Jul 28, 1998 · Boeing 767277 · Wing, Control Surface Attach FittingsSDR 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) Jul 20, 1998 · Boeing 767277 · Nacelle/Pylon, Main FrameSDR 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 WIJul 20, 1998 · Boeing 767277 · Nacelle/Pylon, Main FrameSDR 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.Apr 22, 1998 · Boeing 767277 · Trailing Edge Flap Control SystemSDR AU980532Pdu · faulty(AUS) OUTBOARD LEADING EDGE SLAT POWER DRIVE UNIT (PDU), ELECTRIC MOTOR FAULTY.Mar 29, 1998 · Boeing 767277 · Leading Edge Slat ActuatorSDR 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.Mar 6, 1998 · Boeing 767277 · Nacelle/Pylon, Attach FittingsSDR AU971644Actuator · failed(AUS) LH MAIN LANDING GEAR LEFT HAND DRAG BRACE ACTUATOR PISTON ROD SHEARED IN THREADED AREA.Dec 26, 1997 · Boeing 767277 · Landing Gear Retraction/Extension SystemSDR 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 PREVENTINGOct 27, 1997 · Boeing 767277 · Landing Gear Door ActuatorSDR 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.Mar 7, 1997 · Boeing 767277 · Hydraulic System, MainSDR AU970481Hydraulic Fuse · faulty(AUS) RH MAIN LANDING GEAR TRUCK POSITIONER `UP' LINE HYDRAULIC FUSE FAULTYMar 7, 1997 · Boeing 767277 · Landing Gear Retraction/Extension SystemSDR AU970455Fuselage · corroded(AUS) FUSELAGE CONTAINED LEVEL 2 CORROSION - FOUND DURING INSPECTIONFeb 28, 1997 · Boeing 767277 · Fuselage Main, StructureSDR AU960897Cylinder · cracked(AUS) RH MAIN LANDING GEAR OUTER CYLINDER AFT TRUNNION CRACKED AND CORRODED IN AREA OF FILLET SEALMay 9, 1996 · Boeing 767277 · Main Landing Gear Strut/Axle/TruckSDR AU960898Cylinder · cracked(AUS) RH MAIN LANDING GEAR OUTER CYLINDER AFT TRUNNION CRACKED AND CORRODED IN AREA OF FILLET SEALApr 6, 1996 · Boeing 767277 · Main Landing Gear Strut/Axle/TruckSDR 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 CMar 16, 1996 · Boeing 767277 · Main Landing Gear Strut/Axle/TruckSDR 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 - ATAJan 31, 1996 · Boeing 767277 · Fuel System Wiring
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