Boeing 767-222
Service difficulty reports · 956
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 = '767222' 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 = '767222' 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 2001UALA00189Splice · corrodedNR 1 PYLON INBOARD SIDE BETWEEN 2 SIDE PANELS, ATTACH SPLICE IS CORRODED. REPLACED SPLICE PER SRM 51-40-02.SDR 2001UALA00186Shear Tie · corrodedAFT PIT SHEAR TIE CORRODED BS 1480. REPLACED SHEAR TIE REF: BAC 140T2102 AND SRM 51-40-02.SDR 2001UALA00183Shear Tie · corrodedAFT PIT SHEAR TIE BETWEEN STR 39L AND 39R CORRODED. INSTALLED NEW SHEAR TIE PER BAC DRAWING 146T1206 AND SRM 51-40-2.SDR 2001UALA00182Seat Track · corrodedMAIN CABIN SEAT TRACK FITTING CORRODED AT STATION 1421 T0 1471, RBL 90, UNDER FLANGE. REPLACED FITTING PER BAC DWG 146T5204-2 AND INSTALLED FITTING PER SRM 51-40-2.SDR 2001UALA00117Light · malfunctionedEMERGENCY EXIT LIGHTS ON DURING CRUISE WITH COCKPIT SWITCH IN ARMED POSITION. RECYCLED SWITCH PER LHRLM.SUPPLEMENTAL DATA UPDATE ACCOMPLISHED EMERGENCY LIGHTS OP CHECK, OPS CHECK GOOD. OBSERVED LIGHTS FOR SEVERAL HOURS WITH NO PROBLEMS NOTEDSDR 2001UALA00134Stringer · corrodedAFT CARGO PIT AT BS 1395, STRINGER 39L END FITTING IS CORRODED BOTH SIDES OF STRINGER. REMOVED CORROSION FROM STRINGER PER GN-MM 5-0-6-1. REPLACED STRINGER SPLICE CLIPS PER BAC DWG 146T3006 STRINGER SPLICE CLIPS PER BAC DWG 146T3006 AND INSTALLED PER SRM 51-SDR 2001UALA00111Attach Angle · corrodedAFT CARGO PIT BS 1087 STRINGER 39R FRAME TO STRINGER ATTACH ANGLE CORRODED. *S/D* STRINGER ATTACH ANGLE WAS REPLACED BY OSV TIMCO, REFERENCE SRM 51-40-02 FOR FASTENER INSTALLATION PROCEDURES.SDR 2001UALA00112Apu · leakingAIRCRAFT DISPATCHED WITH NR 1 GENERATOR INOPERATIVE. CREW REPORTED THAT THE APU OIL QUANTITY WAS DROPPING. AIRCRAFT DIVERTED TO DEN.SDR 2001UALA00107Shear Tie · corrodedAFT CARGO PIT AT BS 1307 BETWEEN STRINGERS 36L AND 36R SHEAR TIE IS CORRODED. *S/D* SHEAR TIE WAS REPLACED BY OSV TIMCO, REFERENCE SRM 51-40-02 FOR FASTENER INSTALLATION PROCEDURES.SDR 2001UALA00093Frame · corrodedAFT CARGO PIT AT BS 1197 FROM RBL 13-19, FRAME CAP IS CORRODED. *S/D* FRAME T-CAP WAS REPLACED BY OSV TIMCO, REFRENCE 51-40-02 FOR FASTENER INSTALLATION PROCEDURES.SDR 2001UALA00091Battery Pack · dischargedRIGHT SIDE EEL LIGHTS ON WITH OVERHEAD SWITCH IN THE ARM POSITION. *S/D* ADJUSTED EMERGENCY LIGHT MICROSWITCH ON OVERHEAD PANEL. CHECKED 28VDC CHARGING VOLTAGE AND GROUNDS, ALL OK. REPLACED EMERGENCY LIGHT POWER SUPPLY. (NOTE - EEL LIGHT PROBLEMS IN 2 PRESDR 2001UALA00092Skin Panel · corrodedEXTERIOR FUSELAGE VHF RIGHT ANTENNA SKIN CUTOUT CORRODED STATION 510 BL 0. *S/D* SKIN REPAIRED PER SRM 53-30-01 AT OSV TIMCO.SDR 2001UALA00086Fseu · malfunctionedL/E SLAT ASSYM EICAS MSG AND ASSOC LIGHT ILLUM WHEN FLAP HANDLE PLACED TO ZERO. SLAT INDICATION STICKS BETWEEN 1 AND ZERO. PER FLT MANUAL IRREG 7-40 CYCLE FLAPS TO EXTEND, NO HELP. L/E ASSYM RETURNED UPON RETRACT SELECTION. PER FLT MANUAL DID NOT SELECT ALSDR 2001UALA00089Switch · stuckON CLIMBOUT OF JFK, EMERGENCY SIGN LIGHTS ON, ON RIGHT SIDE OF FIRST AND BUSINESS CLASS. *S/D* FOUND FLIGHT ATTENDANT EMERGENCY LIGHT TEST SWITCH STUCK. CYCLED SWITCH, OPS CHECK GOOD.SDR 2001UALA00087Light · intermittentRIGHT HAND FORWARD CABIN EEL LIGHTS COMES ON INTERMITTENTLY WITH SWITCH IN ARM POSITION.SDR 2001UALA00081Cart · shortedENTRY CART 300 IN MID-GALLEY SPARKED WHEN PLUGGED IN AND THE 60 AMP AC CB POPPED. OK AT FIRST SERVICE OF FLIGHT. LEFT UNPLUGGED AND DID NOT RESET. *S/D* CART CONTROL PANEL HAD SHORT TO GROUND. TAGGED CART AND NOTIFIED DOBBS FOOD SERVICE. RESET 15 AMP CIRCSDR 2001UALA00053Oven · contaminatedSMALL FLAME AND SMOKE IN FORWARD CABIN OVEN FROM PAPER WRAPPER. CIRCUIT BREAKER PULLED AND FIRE EXTINGUISHER USED.SDR 2001UALA00045Warning Light · illuminatedGEAR DISAGREE AND GEAR DOORS CAUTION MESSAGE AND LIGHTS ILLUMINATED AFTER GEAR UP AND HANDLE MOVED TO OFF.SDR 2001UALA00054Circuit Board · failedGOT FIRE OVERHEAT MESSAGE AND ASSOCIATED RIGHT ENGINE FIRE LOOP 1 AND 2 STATUS MESSAGE. RESET FIRE-OVERHEAT SWITCH. LIGHT STAYED OUT DIVERTED TO DEN. *S/D* CAUSE OF THE RIGHT ENGINE LOOP 1 AND LOOP 2 STATUS MESSAGE WAS RIGHT ENGINE AFOLTS CARD M10274 (MR26SDR 2000UALA00814Structure · damagedACFT SUSTAINED STRUCTURAL DAMAGE, APPROX 6 FT BELOW DOOR 1L AND RUNS AFT 28 FT. INITIAL EVAL SHOWS DMG STARTS AT LT FS 303 AND RUNS TO STA 570 THRU BOTH STATIC PORTS IN CRITICAL AREA ALONG STRINGER S28 & S29. *S/D* DAMAGE WAS DUE TO ACFT CONTACT WITH A JSDR 2000UALA00730Warning Light · illuminatedTRAILING EDGE FLAP DISAGREE EICAS ILLUM WITH FLAPS SELECTED 15 LOCKED AT 5 DEG ALT DROVE TO 15 DEG FOR LANDING. LANDED UNDER AMBER ALERT.SDR 2000UALA00718Gear · wornL/E SLAT ASYM DURING FLAP EXTENTION ON APPROACH. *S/D* THE RIGHT WING SLATS DID NOT MOVE TO THE COMMANDED POSITION DUE TO A SEVERELY WORN OUTBOARD LEADING EDGE SLAT DRIVE TORQUE TUBE. WHEN THE LEFT WING L/E SLAT POSITION DOES NOT MATCH THE RIGHT WING L/E SLSDR 2000UALA00701Harness · burnedSMOKE IN MID CABIN REPORTED BY FLIGHT ATTENDANT. DISCONNECTED PIG TAIL AND ISOLATED. SMOKE AND ORDER DISSIPATED. SUPPLEMENTAL DATA UPDATE CART HEATER PIG TAIL OVERHEATED WITH EVIDENCE OF BLACK CHARRING. CART HEATER PIG TAIL WAS REPLACED, CART HEATER OPERATIONSDR 2000UALA00635Light · intermittentEXIT PATH LIGHTING BETWEEN ROWS 15 - 25 RT SIDE ARE FLASHING ON INTERMITTENTLY PER CREW. REPLACED EEL BATTERY PACK, OPS CK GOOD.SDR 2000UALA00625Fuel Control · malfunctionedNR 2 ENGINE EPR AND N1 PARAMETERS REMAINED AT IDLE POWER UPON APPLICATION OF T/O POWER. RTB. *S/D* CAUSED BY THE FUEL CONTROL OR THE FUEL PUMP. BOTH UNITS WERE REPLACED. THE FUEL CONTROL UNIT FAILED THE AS RECEIVED TEST BENCH CHECK. THERE WAS NO PS4 ACTUSDR 2000UALA00624Aileron · jammedAT FL370 SAT-60C, AUTOPILOT EICAS MESSAGE AND LIGHT SHOWN. A/P DISCONNECTED, AILERONS APPEARED JAMMED. AILERONS REGAINED BY APPLICATION OF 50 - 75 POUND FORCE. FLIGHT CONTINUED AND LANDED UNEVENTFULLY.SDR 2000UALA00626Landing Gear · malfunctionedAFTER TAKEOFF JFK RIGHT MAIN GEAR REMAINED EXTENDED WITH RT GEAR DOWN GREEN LIGHT ILLUMINATED. RIGHT GEAR RETRACTED AFTER 11 MINUTES. JFK TOWER CONFIRMED VISUALLY RT GEAR EXTENDED WITH OTHER GEARS RETRACTED. CTR HYD PRESS NORMAL. HAD EICAS MSG''S GEAR DISASDR 2000UALA00610Duct · crackedLOUD HISS HEARD SEAT 30A FLOOR LEVEL WHEN THROTTLES ARE RETARDED DURING DESCENT. RUBBER SMELL COMING FROM ROW 30 FLOOR VENTS. *S/D* THERE IS NO AMIS HISTORY FROM 12/1/00 TO 10/24/00 OF A RUBBER SMELL COMING FROM ROW 30 FLOOR VENTS. HOWEVER, THE LOUD HISS HSDR 2000UALA00606Apu · failedSPARKS COMING FROM APU EXHAUST. FLIGHT CREW DISCHARGED 1 FIRE BOTLE. RETURNED TO BLOCKS.SDR 2000UALA00596Strut · crackedFOUND ONE QUARTER INCH CRACK IN OUTER CYLINDER OF RIGHT MAIN LANDING GEAR REQUIRES REPLACEMANT OF OUTER CYLINDER SUPPLEMENTAL DATA UPDATE CAUSE CURRENTLY UNKNOWN. OUTER CYLINDER WAS REPLACED.SDR 2000UALA00592Fan · faultyON CLIMB CREW NOTICED ACRID SMELL IN THE FLIGHT DECK. FLIGHT CONTINUED TO SFO. LIGHTING TURNED OFF AND SMELL DISSIPATED. REPLACED FWD EQUIP FAN.SDR 2000UALA00553Switch · damagedAFT LAVATORY SMOKE DETECTOR ANNOUNCES IN FLIGHT. *S/D* CHECK OF THE DETECTOR FOUND THAT THE TEST SWITCH HAD BEEN DAMAGED (NO DETENT) AND COULD VIBRATE TO THE ''TEST'' POSITION AND SOUND THE ALARM. A SERVICEABLE DETECTOR WAS INSTALLED IN THE AIRCRAFT AND OPESDR 2000UALA00529Module · faultyLEFT AND RIGHT RUDDER TRIM INOP. RTF. REPLACED AILERON AND RUDDER TRIM CONTROL MODULE, OPS CHECK OK.SDR 2000UALA00499Light · inoperativeOUTSIDE EEL LIGHT OUT BY DOOR 2L. CLEANED LIGHT SOCKET, OPS CHECKS OK.SDR 2000UALA00503Warning Light · illuminatedSTAB TRIM EICAS AND OVERLIGHT CAME ON WHILE LEVELING AT FL 330, UNABLE TO DETERMINE TRIM RATE.SDR 2000UALA00493Engine · malfunctionedLEFT ENGINE DID NOT COME UP TO SPEED ON TAKEOFF ROLL. LARGESPLIT ON POWER LEVER DEVELOPED, ABORTED AT 100 KNOTS. *S/D* FOUND BROKEN PT7 (EPR) LINE. REPLACED EPR LINE PER MAINTENANCE MANUAL.SDR 2000UALA00470Fan · contaminatedSTRONG METALLIC ODOR AFTER T/O IN FLIGHT DECK. ALSO SMELLED IN CENTER CABIN BY F/A. THE SMELL STARTED APPROX 1 MIN AFTER GEAR UP AND LASTED APPROX 2 MINS. *S/D* FAILED PRESSURE LINE IN CENTER HYD SYSTEM IN THE RECIRCULATION FAN AREA IN THE FWD CARGO PIT. SDR 2000UALA00435Valve · leakingCHRONIC CENTER TANK FUEL TRANSFER. *S/D* THE TRANSFER WAS FOUND TO BE THE RESULT OF LEAKAGE FROM THE LEFT MAIN TANK AND THE FOLLOWING REPAIRS WERE MADE. THE CENTER TANK REFUEL VALVES WERE REPLACED DUE TO LEAKAGE WHEN CLOSED. THE LEFT SURGE TANK DRAIN LINE SDR 2000UALA00430Oven · shortedRETURNED TO BLOCKS. BURNING ODOR IN AFT GALLEY. *S/D* FOUND OVEN (P/N: 8800-01-0000) 2 CIRCUIT BREAKER B PHASE OPEN. REPLACED CB AND OVEN CHECKED GOOD. NO ODORS NOTED.SDR 2000UALA00402Battery Pack · dischargedEEL LT AISLE INTERMITTENTLY FLASHES ON AND OFF BY ITSELF. *S/D* REPLACED EEL BATTERY PACK AT ROW 16AB. LIGHTS TEST OK AND NO MOREFLASHING.SDR 2000UALA00378Coffeemaker · smokeSPARKS AND SMOKE SEEN FROM AFT GALLEY HOTPLATE H61. DIVERTED TO CLE. *S/D* FOUND HOT PLATE H62 AT FAULT, NOT H61. REPLACED H62 HOT PLATE, OPS CHECKED NORMAL.SDR 2000UALA00376Connector · corrodedPOSSIBLE FUEL LEAK OR BROKEN GAUGE. FLIGHT DIVERTED TO DEN. DISCREPANCY BETWEEN CALCULATED AND TOTALIZER FUEL READINGS, ALSO FUEL IMBALANCE. *S/D* THE FUEL DISCREPANCY RESULTED IN A D1 AND D4 FAULT ON THE FQIS PROCESSOR INDICATING LEFT MAIN TANK DENSITOMETSDR 2000UALA00366Drain Valve · leakingFOUND LT AND RT MANIFOLD DRAIN VALVES LEAKING HEAVILY. *S/D* THE FUELING MANIFOLD DRAIN VALVES WERE REPLACED. IT WAS ALSO FOUND THAT THE LT SURGE TANK DRAIN LINE WAS LEAKING. THE COUPLING O-RINGS WERE REPLACED IN THE DRAIN LINE. THREE LEAKS AT RIB 3 BETWESDR 2000UALA00346Battery · inoperativeLEFT OVERWING EMERGENCY LIGHT STAYS ILLUMINATED IN THE ARMED POSITION. REPLACED BATTERY PACK (P/N: 2013-1), OPS CHECK GOOD.SDR 2000UALA00345Throttle · malfunctionedDESCENDING FROM FL 390 TO FL 350, NR 1 ENGINE DID NOT ACCELERATE WHILE THROTTLE MOVED FORWARD NORMALLY. *S/D* NO CAUSE WAS FOUND FOR THIS DISCREPANCY. MAINTENANCE PERFORMED AN ACCELERATION TEST, AND IT PASSED TEST. AIRCRAFT FLEW SUBSEQUENT FLIGHTS WITH NO SDR 2000UALA00320Control Cable · icedAT CRUISE, FL390, WITH AUTO THROTTLE AND AUTO PILOT ENGAGED, AUTO PILOT DISCONNECT LIGHT SHOWN & AURAL WARNING SOUNDED. PITCH-YAW DISENGAGED. AILERON MOVEMENT RESTRICTED. A-P DISCONNECT BAR USED. NO HELP. USED 15LBS PRESSURE TO DISENGAGE AILERONS. RE-OCCURREDSDR 2000UALA00276Compensator · failedFUEL SYSTEM INDICATION PROBLEMS: TOTALIZER READS 3 THOUSAND POUNDS HIGHER THAN CALCULATED. AFTER TAKEOFF CENTER TANK WENT ZERO TO 0.6, LEFT WING 2 THOUSAND HIGHER THAN RIGHT IN CLIMBOUT. IN CRUISE LEFT AND RIGHT WING TANKS INDICATIONS EQUALIZED. DIVERTED TOSDR 2000UALA00280Bolt · crackedNR 1 PYLON O/B SIDE LOAD FITTING I/B BOLT HAD CRACK INDICATION. *S/D* BOLT MATERIAL IS H11 STEEL AND CRACK IS THE RESULT OF STRESS CORROSION, A CHARACTERISTIC OF H11 MATERIAL. INCONEL 718 BOLTS WERE INSTALLED PER PROCEDURES OUTLINED IN BOEING SERVICE BULLETSDR 2000UALA00279Bolt · crackedNR 2 PYLON O/B SIDELOAD FITTING I/B BOLT FOUND CRACK INDICAITON. *S/D* BOLT MATERIAL IS H11 STEEL AND CRACK IS THE RESULT OF STRESS CORROSION, A CHARACTERISTIC OF H11 MATERIAL. INCONEL 718 BOLTS WERE INSTALLED PER PROCEDURES OUTLINED IN BOEING SERVICE BULLESDR 2000UALA00278Tube · leakingOFF WING SLIDE LOWER TUBE FAILED AIR RETENTION TEST. FOUND A HOLE IN LOWER TUBE (P/N 106620-218) AND ASPIRATOR WAS SMASHED AND CRACKED. DAMAGE APPARENTLY OCCURRED AT LAST OVERHAUL. SLIDE (P/N 101630-306).
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