Boeing 767-231
Service difficulty reports · 758
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 = '767231' 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 = '767231' 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 ABXA080054Bulb · malfunctioned708AX MADE A DIVERSION TO STA - PHX, NR 2 ENGINE SHUT DOWN DURING CRUISE DUE TO HIGH OIL TEMP, HIGHEST NOTED TEMP 173 DEGREES. ALL OTHER INDICATION APPEARED NORMAL. REPLACED RIGHT ENGINE OIL TEMP BULB IAW ABX B767 MM 79-34-00-4. TEMP SEPERATION REMAINED CONSTASDR ABXA080063Door Frame · corrodedAFT LOWER CARGO DOOR FRAME BELOW VENT DOORS CORRODED IN SEVERAL PLACES. REMOVED AND REPLACED CHORD DOOR BEAM IAW B767 SRM 51-40-02.SDR ABXA070299Bulkhead · damagedNR 2 PYLON AFT TORQUE BOX BULKHEAD SIDE BRACE ATTACH LUG HAD LOCK FASTENER HEAD SHEARED OFF LEFT SIDE. REPLACED BROKEN AND MISSING HI-LOKS IAW B767 MM 54-51-03, DC9 SRM 51-40-02, AND DWG 311T3180 AS PER RFTS 42887.SDR ABXA070277Battery · dischargedEMERGENCY EXIT LIGHTS FADED OUT DURING TEST. SWITCHED BATTERY WITH SPARE IAW B767 MM 33-51-07. THE SPARE EMERGENCY LIGHT BATTERY WAS DEFERRED 56859 FOR MAINTENANCE TRACKING IAW ABX GMM 01.07.04. CLEARED DI 56859, REMOVED AND REPLACED SPARE EMERGENCY LIGHT BSDR ABXA070238Bulb · inoperativeABORTED APPROACH AT MHR. NOSE GEAR FAILED TO ILLUMINATE ON GEAR SELECT DOWN, NO LIGHT IN GEAR INDICATION LIGHT TEST. DID ALT GEAR EXTEND PROCEDURE AND HAD TOWER CONFIRM NOSE GEAR DOWN. VERIFIED NOSE GEAR ANNUNCIATOR DID NOT ILLUMINATE ON LIGHTS TEST. REPLASDR ABXA070071Battery · dischargedON PRE-DEPARTURE CHECK, FOUND WHEN EMERGENCY LIGHT SWITCH SELECTED TO ON, LIGHTS ILLUMINATED MOMENTARILY, THEN EXTINGUISHED. SWAPPED SPARE AND ACTIVE EMERGENCY POWER SUPPLIES. OPS CHECKED GOOD IAW B767 MM 33-51-07-2.SDR ABXA070019Blade · damagedON TAKEOFF FROM ILN, DURING LANDING GEAR RETRACTION, GOT SUBSTANTIAL IMPACT SOUND FROM LEFT ENGINE AREA, AND BURNING SMELL AFTER SOUND. NO ENGINE ABNORMALITIES OR EXCEEDANCES. LANDED UNDER WEIGHT. C/W BIRD STRIKE INSPECTION BORESCOPE & BLADE REPLACEMENT ON SDR ABXA060262Battery · dischargedEMERGENCY LIGHTS WERE LEFT ON WITH SWITCH IN -ARMED- POSITION. SWAPPED MAIN POWER SUPPLY WITH ALTERNATE POWER SUPPLY IAW B767 AMM 33-51-02. OPS CHECKED GOOD.SDR ABXA060261Battery · dischargedSTANDBY EMERGENCY LIGHT BATTERY INOPERATIVE. REMOVED AND REPLACED STANDBY EMERGENCY LIGHT BATTERY IAW B767 MM 33-51-07. OPS CHECKED GOOD.SDR ABXA060238Rib · crackedAFT FORWARD RIB FOR FORWARD LOWER CARGO DOOR CRACKED ON LOWER FLANGE. RIB IS ON AIRCRAFT STRUCTURE. REPAIRED HORIZONTAL LEG OF FORWARD LOWER CARGO DOOR ACTUATOR SUPPORT IAW B767 SRM.SDR ABXA060239Angle · crackedNR 2 ENGINE STRUT CLOSEOUT ANGLE WAS CRACKED JUST AFT OF THE OUTBOARD MID SPAR FITTING (INBOARD FASTENER OF THE CLOSEOUT FITTING ON THE OUTBOARD SIDE). REMOVED AND REPLACED CLOSEOUT FITTING IAW BOEING DWG 311T3150 AND BOEING SRM 51-40-2.SDR ABXA060237Skin · damagedSTATIC DISCHARGE MARK ON FUSELAGE EXTERIOR AT FS 430 BETWEEN LONGERON 11 AND 12 RIGHT. REPAIRED IAW B767 SRM 53-00-01.SDR ABXA060158Engine · surgesRIGHT ENGINE SURGE AT CONSTANT THRUST. ENGINE WAS SHUTDOWN DUE TO UNRECOVERABLE SURGE. COMPLIED WITH/W NR 2 ENGINE INSPECTION IAW FIM 71-05-00. BOROSCOPED NR 2 ENGINE. NO DEFECTS FOUND. TURNED VSV SCHEDULE RATE SCREW ON TURN CLOCKWISE. OPS CHECK GOOD ON GROSDR ABXA050187Window · missing1ST CABIN WINDOW AFT OF OVERWING EMERGENCY EXIT LEFT SIDE WAS MISSING A PIECE OF THE OUTER PANE. REMOVED AND REPLACED BROKEN WINDOW AFT OF LEFT EMERGENCY EXIT DOOR IAW B767 AMM 56-21-01-4.SDR ABXA050123Slide · malfunctionedMAIN ENTRY DOOR SLIDE WOULD NOT ARM. CYCLED MAIN ENTRY DOOR SEVERAL CYCLES. SLIDE ARM MECHANISM ARMED AND DISARMED AS REQUIRED. ALL CHECKS GOOD IAW B767 AMM.SDR ABXA050120Girt Bar · contaminatedCREW REPORTED MAIN ENTRY DOOR SLIDE WOULD NOT ARM. CHECKED FOR DEBRIS IN GIRT BAR AREA. CLEARED AREA AND CYCLED DOOR. DOOR CHECKED GOOD. SLIDE ARMS AND DISARMS.SDR ABXA050086Pressure Switch · defectiveIN FLIGHT, RIGHT OIL FILTER LIGHT DID NOT GO OUT WITH TRUST REDUCTION. RT ENGINE WAS SHUT DOWN. WINDMILLED FOR 31 MINUTES, OIL PRESSURE UNKNOWN. FOUND THE RIGHT OIL FILTER DIFFERENTIAL PRESSURE SWITCH DEFECTIVE. REPLACED THE SWITCH. COMPLIED WITH NR 2 ENGSDR ABXA050029Girt Bar · failedLT FORWARD ENTRY DOOR GIRT BAR FAILED TO LOCK. PLACED MED EMERGENCY ESCAPE SLIDE ON DEFERRAL AND MAINTENANCE PROCEDURES COMPLIED WITH. CLEARED DEFERRAL. FOUND SEAL ON LOWER FORWARD BUSTLE BINDING. TRIMMED SEAL ON BUSTLE AND EMERGENCY SLIDE ARMS NORMAL IAW BSDR ABXA050024Fitting · crackedLEFT WING SPOILER TORQUE TUBE HINGE FITTING CRACKED AT RSS 714.10. REMOVED AND REPLACED HINGE FITTING.SDR ABXA040402A/C Pack · malfunctionedEMERGENCY DECLARED. AIR DIVERSION FROM ILN TO ORD, FLIGHT 1408. RIGHT PACK INOP AND PACK OFF LIGHT ILLUMINATED. EICAS MESSAGE'S RIGHT PACK OFF AND RIGHT PACK TEMP DISPLAYED. LIGHT DID NOT EXTINGUISH WHEN STANDBY SELECTED OR WHEN PACK SELECTED OFF. INSPECTSDR ABXA040338Light · inoperativeOVERHEAD PANEL EMERGENCY LIGHTS BACKGROUND LIGHTING DIM/INOP. REPLACED EMERGENCY LIGHT AND CREW OXYGEN LIGHT PLATE. OPS CHECKED GOOD IAW B767 AMM 33-13-07.SDR ABXA040317Lamp · inoperativeLT MAIN GEAR DOWN (GREEN) INDICATION LIGHT INOPERATIVE. LIGHT INOPERATIVE WITH TEST BUTTON PUSHED. CREW PERFORMED A GO AROUND AT EWR. RELAMPED LT MAIN GEAR DOWN GREEN INDICATOR LIGHT AND RT MAIN GEAR DOWN GREEN INDICATOR LIGHT. OPS CHECKED OK.SDR ABXA040297Seal · tornDURING R1 PREFLIGHT, DISCOVERED CAPTAINS NR 2 WINDOW CRANK BINDING TOWARDS CLOSE. FOUND L2 WINDOW SEAL TORN AND CATCHING ON WINDOW, REMOVED AND REPLACED L2 WINDOW SEAL IAW AMM 56-11-11-4.SDR ABXA040280Screw · defectiveDURING MAINTENANCE INSPECTION AT BFI, FOUND THE CAPTAIN'S SLIDING WINDOW WOULD NOT CLOSE. NR 2 L WINDOW. REPLACED NR 2 LT WINDOW BALL SCREW AND NUT ASSEMBLY IAW MM CHAP. 56-11-04-4.SDR ABXA040182Pressure Switch · defectiveLT ENGINE OIL FILTER MESSAGE DISPLAYED. MESSAGE REMAINED WHEN THRUST REDUCED & ENG SHUTDOWN. NR 1 ENG OIL PRESSURE LIGHT DID NOT COME ON. C/W FIM 79A-35-00-90, OIL FILTER EICAS MESSAGE WAS NOT DISPLAYED AT AIRCRAFT ARRIVAL THOUGH ENGINE WAS STILL WINDMILLINGSDR ABXA040177Stop · brokenCOCKPIT ENTRY DOOR CAME OPEN AND THEN JAMMED DURING TAXI AND COULD NOT BE OPENED. COCKPIT DOOR LATCH BROKEN. REPLACED BROKEN DOOR STOP IAW 767 SRM 51-40-2.SDR ABXA040170Spring · failedMAIN ENTRY DOOR ESCAPE SLIDE DEPLOYMENT BAR WOULD NOT STAY UP. REPLACED DEPLOYMENT BAR GAS SPRINGS. OPS CHECKED GOOD IAW B767 AMM 26-66-01.SDR ABXA040134A/C Pack · shutdownDURING APPROACH TO RUNWAY 22L AT MHR, WHEN LANDING GEAR WAS LOWERED, RIGHT PACK SHUT OFF AND LOC FAILED. MISSED APPROACH EXECUTED, GEAR CYCLED UP AND DOWN AND EVERYTHING SEEMED TO WORK AGAIN. MAINTENANCE AT MHR COMPLIED WITH MCDP GROUND TEST 30. NO CURRENT SDR ABXA040079Fitting · crackedMX INSPECTED O/B PITCH LOAD FITTING LOCATED ON NR 2 ENG PYLON MANDATED BY AD 2001-08-23 & S/B 767-57A0070. HFEC INSPECTION REVEALED A CRACK INDICATION IN FITTING. CRACK WAS LOCATED IN UPPER I/B RADIUS OF FITTING, APPROX 1.25 INCH LONG RUNNING FORWARD AND AFTSDR ABXA040086Fitting · crackedDURING INSPECTION OF NR 2 ENGINE PYLON OUTBOARD SIDE LOAD FITTING PER AD 2001-08-23 AND SB 767-547A0070, HFEC INSPECTION REVEALED CRACK IN UPPER INBOARD RADIUS. INTERIM REPAIR ON REA B657-49099MR.SDR ABXA040042Element · defectiveCREW DETECTED A BURNING ELECTRICAL ODOR IN THE COCKPIT AFTER TAKEOFF. THE PROBABLE SOURCE WAS LOCATED BY OBSERVING A DISCOLORED/CHARRED AREA OF THE RT FORWARD WINDOW. LOWER RIGHT CORNER WHERE THE ELECTRICAL WIRING CONNECTS TO THE WINDOW HEAT ELEMENT. RIGHT SDR ABXA040041Odor · detectedUNUSUAL ODOR IN COCKPIT. STRONGEST IN FOOT WELLS. NO NOTICABLE ODOR AFT OF COCKPIT DOOR. RAN APU AND PACKS, STILL NO ODOR. INSPECTED COCKPIT AND FOUND NOTHING OUT OF ORDINARY.SDR ABXA030491Window · stuckFIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED FIRST OFFICER'S WINDOW IAW B767 MM.SDR ABXA030461Acm · contaminatedAIR CONDITIONING SYSTEM HAD A STRONG GLUE TYPE ODOR, ESPECIALLY DURING DESCENT. ODOR WAS THERE WITH APU OR ENGINES SUPPLYING AIR. FOUND ODOR TO BE AN OIL TYPE ODOR FROM ACM'S. PERFORMED STEPS TO REMOVE OIL CONTAMINATION FROM AIR CONDITIONING SYSTEM IAW B767SDR ABXA030451Acoustic Liner · missingNR 2 ENGINE REVERSER OUTBOARD SIDE INNER AREA HAD DAMAGE DUE TO LIBERATION OF A P/N 803723 ENGINE FAN EXIT CASE OUTBOARD ACOUSTIC LINER SEGMENT ASSEMBLY, WHICH RAN FROM THE 3 O'CLOCK TO THE 5 O'CLOCK POSITION, AFT FACING FORWARD. REPLACED NR 2 ENGINE OUTBOARD SDR ABXA040023Bolt · brokenRIGHT MAIN LANDING GEAR ACTUATOR ATTACH FITTING AT REAR SPAR AREA HAD BROKEN BOLT HEADS, 2 EACH, AT AFT AND FRONT OUTBOARD SIDE OF ACTUATOR. REMOVED AND REPLACED FASTENERS AT REAR SPAR IAW BOEING SRM 51-00-00.SDR ABXA030139Actuator · defectiveSPOILERS LIGHT ILLUMINATED EICAS MESSAGE SPOILERS DISPLAYED WITH SPOILERS SELECTED DOWN. THIS HAPPENED IMMEDIATELY AFTER TAKEOFF. AT FL 350, CONTROL WHEEL DISPLAYED AN UNCOMMANDED 45 DEGREES WITH AUTOPILOT ENGAGED. AUTOPILOT WAS DISCONNECTED AND THE UNCOMMASDR ABXA030085Door Frame · contaminatedEMERGENCY SLIDE WOULD NOT ARM. FOUND DEBRIS IN MAIN ENTRY DOOR JAMB, REMOVED DEBRIS. DOOR CLOSED AND EMERGENCY SLIDE ARMED AS REQUIRED IAW B767 MM.SDR ABXA030059Shroud · damagedREVERSER ISOLATION VALVE EICAS MESSAGE AND REVERSER ISOLATION LIGHT ILLUMINATED AFTER LANDING WITH REVERSER LEVERS STOWED. RT ENGINE FAN EXIT DUCT, OUTER SHROUD, FAN STARTORS DAMAGED AND OUTER FAN SHROUD PANELS WERE MISSING. ENGINE AND TRHUST REVERSER CHANGED SDR ABXA030027Pressure Switch · defectiveLT ENGINE OIL FILTER MESSAGE DISPLAYED. MESSAGE REMAINED WHEN THRUST REDUCED. AFTER ENGINE SHUTDOWN, MESSAGE DISAPPEARED. NOTE: LT ENGINE SHUTDOWN, (0) OIL PRESSURE LAST 5 MINUTES OF FLT. REMOVED AND REPLACED THE NR 1 ENGINE MAIN OIL FILTER AND THE OIL FILTERSDR ABXA020226Channel · corroded"T" CHANNEL CORRODED, C2 BAG BIN DOOR, BELOW DOOR VENT CUTOUTS. REPLACED "T" CHANNEL IAW BOEING SRM.SDR ABAX020004Mechanism · out of adjustTHE FORCE TO MOVE THE MAIN ENTRY DOOR TO THE CLOSED POSITION WAS EXCESSIVE. COMPLIED WITH ENTRY DOOR COUNTERBALANCE ADJUSTMENT IAW 767 AMM 52-11-16. OPS CHECKED GOOD.SDR ABXA010914Slat · malfunctionedFLT 407- THE CREW DECLARED AN EMERGENCY AND PERFORMED A GO-AROUND INBOUND TO ILN. EICAS MSG LE SLAT ASYM DISPLAYED. LEADING EDGE LIGHT ILLUMINATED WITH FLAP LEVER IN 1. BOTH FLAP POINTERS WERE CORRECT. COMPLETED FIM PROCEDURES IAW B767 FIM 27A-81-00. LIGHTSDR ABXA010912Bearing · seizedCAPTAIN'S AND FIRST OFFICER'S AILERON CONTROL WHEEL BINDING. COMPLIED WITH FIM 27A-11-00, FIG 106, BLOCK 1,2. FOUND BEARING ON LEFT WHEEL WELL QUADRANT CENTERING FORCE SEIZED. REPLACED BEARING IAW BOEING STANDARD OVERHAUL PRACTICES MANUAL 20-50-03. AILERONSDR ABXA010871Battery · dischargedDURING MAINTENANCE INSPECTION, FOUND FLIGHT DECK REMOVABLE EMERGENCY EXIT SIGN BATTERIES LOW. REPLACED BATTERIES IAW B767 MM 33-51-01.SDR ABXA010819Module · malfunctionedEICAS MESSAGE GEAR DISAGREE DISPLAYED AND GEAR AMBER LIGHT ILLUMINATED WITH GREEN DOWN LIGHTS ILLUMINATING. ACCOMPLISHED ABNORMAL PROCEDURE. ON FINAL, GPWS GAVE TOO LOUD GEAR WARNING. ACCOMPLISHED GO AROUND. WHEN GEAR EXTENDED AGAIN, INDICATIONS WERE NORMASDR ABXA010696Switch · defectiveLEFT ENGINE OIL FILTER MESSAGE DISPLAYED. MESSAGE REMAINED WHEN THRUST REDUCED. #1 ENGINE SHUTDOWN, EMERGENCY DECLARED, DIVERTED TO SLC. AFTER ENGINE SHUTDOWN, MESSAGE DISAPPEARED. REPLACED THE OIL PRESSURE SWITCH ON THE LEFT ENGINE. SYSTEM OPS CHECKED GOOD IASDR ABXA010663Fcu · malfunctionedDURING CLIMB, THE NR 1 ENGINE STARTED TO ACCELERATE UNCOMMANDED. PULLED THE THROTTLE TO IDLE, ENGINE DID NOT RESPOND. THE NR 1 ENGINE WAS SHUTDOWN. THE AIRCRAFT RETURNED TO ILN WHERE IT LANDED UNEVENTFULLY. REPLACED THE LEFT TT2 SENSOR AND THE LEFT FUEL COSDR ABXA010658Module · faultyEICAS MESSAGE GEAR DISAGREE DISPLAYED AND GEAR AMBER LIGHT ILLUMINATED WITH GEAR. GREEN DOWN LIGHT ILLUMINATED. ALSO EICAS MESSAGE LANDING MONITOR DISPLAYED WITH LANDING GEAR UP AND LOCKED. DID GEAR RECYCLE AND OVERFLEW STATION. REPLACED LANDING GEAR CONTRSDR ABXA010530Connector · dirtyFRM CODE FOR LEFT ENGINE VIBRATION HIGH INDICATED. OTHER ENGINE INDICATIONS WERE NORMAL. VIBRATION INDICATION CHANGED WITH THRUST LEVER MOVEMENT. HIGHEST INDICATION WAS 1.5 IPS. FAN /LPT0.6 IPS N2. MAINTENANCE COMPLETED ABX767 FIM 71A 05.00 PROCEDURES. C
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