Boeing 767-332
Service difficulty reports · 11,959
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 = '767332' 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 = '767332' 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 DL76S952095Skin · dentedLT WING UPPER SURFACE OF I/B AILERON DENTED. REPAIRED AS PER SRM 57-60-01 REF 51-70-17. DAMAGE FROM HAIL.SDR DL76S952094Skin · dentedLT WING UPPER SURFACE OF NR 6 SPOILER DENTED. REMOVED AND INSTALLED ON RC7. REMOVED PANEL, REMOVED DAMAGE AND FABRICATED REPLACEMENT AS PER SRM 51070-17. REPAIRED PER 51-70-17. DAMAGE FROM HAIL.SDR DL76S952093Skin · dentedLT WING UPPER SURFACE OF NR 2 SPOILER DENTED. REPAIRED PER SRM 57-70-01. DAMAGE FROM HAIL.SDR DL76S952092Skin · dentedLT WING UPPER SURFACE NR 5 SPOILER DENTED. REMOVED AND REPAIRED PER SRM 51-70-17 REF FROM 57-70-01. DAMAGE FROM HAIL.SDR DL76S952091Skin · damagedRT ELEVATOR UPPER SURFACE DAMAGED. OUTBOARD ELEVATOR. SANDED AND POTTED AREAS OF DAMAGE AS PER SRM 55-70-01. REPAIRED PER SRM 55-70-01. REPAIRED PER ERA 270814-14. DAMAGE FROM HAIL.SDR DL76S952090Skin · damagedRT ELEVATOR UPPER SURFACE DAMAGED. OUTBOARD ELEVATOR. SANDED AND POTTED AREAS OF DAMAGE AS PER SRM 55-70-01. REPAIRED PER ERA 270814-14 AND SRM 55-70-01. DAMAGE FROM HAIL.SDR DL76S952089Skin · dentedLT WING UPPER SURFACE NR 6 SPOILER DENTED. REMOVED AND INSTALLED ON RC7. REMOVED PANEL. REMOVED DAMAGE AND FABRICATED REPLACEMENT CORE AS PER SRM 51-70-17. REPAIRED PER 51-70-17. DAMAGE FROM HAIL.SDR DL76S952088Skin · damagedRT ELEVATOR UPPER SURFACE DAMAGED, OUTBOARD ELEVATOR. SEALED AND POTTED AREAS OF DAMAGE AS PER SRM 59-70-00. REPAIRED PER ERA 270814-14. DAMAGE FROM HAIL.SDR DL76S951907Skin · dentedSLAT T/E WEDGE HAIL DAMAGED. REPAIRED PER CMM 57-43-61, FOR NR 3 L/E SLAT DURING SHOP VISIT.SDR DL76S951885Wedge · dentedDURING INSPECITON NR 1 SLAT WEDGE WAS FOUND DENTED FROM HAIL. REPLACED WEDGE PER SRM 57-43-61.SDR DL76S951884Te Wedge · dentedRT WING NR 7 SLAT TRAILING EDGE WEDGE UPPER SURFACE DENTED. REPLACED WEDGE PER CMM 57-43-61.SDR DL76S951882Te Wedge · damagedNR 5 SLAT TRAILING EDGE WEDGE UPPER SURFACE DENTED. REPLACED T/E WEDGE PER CMM 57-43-61.SDR DL76S951879Te Wedge · dentedNR 2 L/E SLAT FOUND TO HAVE DENTS APPARENTLY CAUSED BY HAIL. REPLACED TRAILING EDGE WEDGE AS PER CMM 57-43-61.SDR DL76S951872Te Wedge · dentedRT WING NR 8 SLAT TRAILING EDGE WEDGE UPPER SURFACE DENTED. REPLACED TRAILING EDGE WEDGE PER CMM 57-43-61.SDR DL76S951866Skin · dentedUPON GROUND INSPECTION AT DFW AFTER HAIL STORM FOUND A DENT IN NUMBER 10 SPOILER ON THE UPPER SURFACE. REPAIRED PER SRM 57-70-01 REFERENCE TO SRM 51-70-17.SDR DL76S951865Skin · damagedUPON GROUND INSPECTION DFW AFTER HAIL STORM, FOUND HOLES ON UPPER SURFACE OF NR 9 SPOILER. REPAIRED PER SRM 57-70-01 REF 51-17-17.SDR DL76S951863Skin · dentedUPON GROUND INSP, IN DFW AFTER HAIL STORM UPPER SURFACE WAS FOUND TO BE DENTED ON THE NR 7 SPOILER. REPAIRED PER SRM 51-70-17.SDR DL76S951854Skin · dentedDURING GROUND INSPECTION, DAMAGE FOUND TO UPPER SURFACE OF LT I/B ELEVATOR. REPAIRD PER SRM 55-20-01 REF 51-70-17.SDR DL76S951853Skin · dentedDAMAGE FOUND DURING GROUND INSPECTION AFTER HAIL STORM IN DFW. DAMAGE WAS FOUND ON UPPER SURFACE O/B RT AILIRON IN VARIOUS AREAS. REPAIR WAS PERFORMED BY SRM 51-70-03 REF SRM 57-60-02.SDR DL76S951852Skin · dentedDURING GROUND INSPECTION DAMAGE FOUND ON UPPER SURFACE OF RT I/B AILERON. REPAIRED PER SRM 57-60-01 REF 51-70-17.SDR DL76S951829Skin · dentedDURING SHOP INSPECTION, NR 2 SPOILER HAD A DENT FROM HAIL DAMAGE AND WAS REPAIRED PER 57-70-01.SDR DL76P951837Coffee Maker · failedDURING CRUISE, FORWARD GALLEY COFFEE MAKER STARTED TO POP AND EMIT SMOKE AND ELECTRICAL BURNING ODOR. SHUTOFF POWER, ODOR QUICKLY STOPPED. FOUND BURNED WIRES ON NR 2 COFFEE MAKER. REPLACED UNIT, OPERATION NORMAL.SDR DL76S951783Skin · lightning strikeFOUND DURING LETTER CHECK, LIGHTNING STRIKE ABOVE L/E OF LEFT WING. REPAIRED PER SRM 53-00-01, DYE CHECKED OK AND PAINTED.SDR DL76S951782Skin · lightning strikeFOUND DURING LETTER CHECK. SEVERAL LIGHTNING STRIKES ABOVE COCKPIT AREA. REPAIRED PER SRM 53-00-01.SDR DL76L951693Valve · faultyON CLIMBOUT, HAD LEFT BLEED OVERHEAT LIGHT WITH EICAS MSG, RETURNED ATL. AIR SUPPLY BITE FAULTS FAN, AIR VALVE AND FAN AIR TEMP SENSOR. REPLACED FAN AIR VALVE AND FAN AIR TEMP SENSOR. AIR SUPPLY BITE CHECKS GOOD OPERATION NORMAL.SDR DL76S951720Trunnion · fracturedAFTER ARRIVAL AT GATE WHILE AIRCRAFT WAS MOTIONLESS, THE LEFT MAIN LANDING GEAR TRUNNION OUTER CYLINDER FRACTURED AT THE AFT TRUNNION BORE. THE LOWER 180 OF THE AFT END SEPARATED REMOVING A 6 INCH LONG PIECE. INITIAL VISUAL EXAMINATION REVEALS SEVERE CORROSISDR DL76L951637Engine · damageNR 2 ENGINE FAILED BORESCOPE INSPECTION, FOUND FIRST STAGE GUIDE VANE DAMAGE BEYOND LIMITS. REPLACED ENGINE FOR RETURN TO SERVICE.SDR DL76S951575Te Wedge · delaminationDURING LTR CHECK, THE NR 1 L/E SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED. THE DELAMINATED AREA IS APPROXIMATELY 5 INCHES IN DIAMETER AND IS LOCATED 75 INCHES FROM THE INBOARD END AND 2 INCHES FROM THE TRAILING EDGE. REPAIRED PER DSDR DL76S951429Skin · punctureFOUND DURING LETTER CHECK INSP, DENT AND PUNCTURE ON UNDERSIDE OF OUTBOARD AFT FLAP BEHIND NR 11 SPOILER R5T WING. REPAIRED PER SRM 57-53-01, PAINTED AREA.SDR DL76S951428Skin · dentedFOUND DURING LETTER CHECK INSP, DENT ON UNDERSIDE OF OUTBOARD FLAP OUTBOARD END RT WING. REMOVED DAMAGED AREA AND STARTED REPAIR PER SRM 57-53-01, OK TO PAINT FINISHED REPAIR PER SRM 57-53-01 AND PAINTED AREA.SDR DL76L951272Skin · crackedRT OUTBD ELEVATOR LOWER SKIN WAS CRACKED AND DENTED AT ELEVATOR, STA 246 AND 25 INCH AFT OF LEADING EDGE. DAMAGE WAS REPAIRED PER SRM 51-70-17.SDR DL76S951280Wheel · failedON TAXI OUT FELT AND HEARD LOUD BANG AT NOSE AREA. RETURNED TO GATE, FOUND RT NOSE WHEEL RIM BROKEN AND LEFT WHEEL DAMAGED FROM THE EXPLOSION. INITIAL INSPECTION, INDICATES FAILURE OF WHEEL AT BEAD AREA.SDR DL76S951144Smoke Alarm · activatedDURING CRUISE, HAD FOUR LAVATORY SMOKE ALARMS SOUND. WITH NO VISIBLE SMOKE ONLY SLIGHT ELECTRICAL SMELL. SMELL DISSIPATED QUICKLY. AFTER LANDING, REACTIVATIED SMOKE, ALARMS, RAN PACKS, RECIC. FAN AND ALL GALLEY EQUIPMENT, NO TROUBLE FOUND RETURNED TO SERVISDR DL76L951143Qty Transmitter · malfunctionedDURING CRUISE FL 290, CENTER HYDRAULIC QUANTITY LIGHT CAME ON WITH DROP IN BRAKE PRESSURE. ALSO, HAD RESERVE BRAKES AND STEERING LIGHT COME ON AND OFF. THEN QTY INDICATION FLUCTUATIONS. DIVERTED JFK, LANDED WITHOUT INCIDENT. VERIFIED HYDRAULIC QTY FULL, RESDR DL76S950828Longeron · wornDURING SHOP INSPECTION, NR 1 ENGINE CORE COWL LOWER LONGERON WAS FOUND WORN AT THE AFT HINGE FITTING. REPAIRED PER SRM 54-41-02 FIG 207.SDR DL76S951187Cowling · wornDURING SHOP INSP THE AFT LOWER LONGERON OF THE LEFT ENGINE SIDE COWL WAS FOUND TO BE WORN AT THE HINGE FITTING AND THE HINGE FITTING WAS WORN AND BENT. A NEW SECTION WAS SPLICED IN PER SRM 54-41-02, AND THE HINGE FITTING WAS BLENDED TO ALLOWABLE LIMITS OF SRMSDR DL76L950774Skin · damagedDURING LETTER CHECK INSP. FOUND AREA OF DAMAGE ON LOWER SURFACE OF T/E FORE FLAP MARKED IN LINE WITH NR 8 TIRE, RT WING. INSTALLED PERMANENT REPAIR PER SRM 57-53-01 FIG 201.SDR DL76S950698Skin · lightning strikeDURING LETTER CHECK, FOUND SEVERAL LIGHTNING STIKES TO FUSELAGE SKIN. RT SIDE REPAIRED PER SRM 53-00-01 ITEM 3.SDR DL76S950657Fan · shortedDURING CRUISE, FLIGHT ATTENDANT REPORTED BURNING SMELL FROM OVERHEAD GASPER FAN VENTS. DEACTIVATED FAN, ODOR STOPPED. REPLACED GASPER FAN OPERATION NORMAL.SDR DL76L951703Nose Cowl · crackedDURING SHOP VISIT, A 2 INCH BY 6 INCH HOLE AT THE 6 O'CLOCK POSITION WAS REPAIRED PER SRM 54-13-01, FOR NR 1 ENGINE NOSE COWL.SDR DL76L950658Transmitter · malfunctionDURING CLIMBOUT, HAD NO OIL PRESSURE INDICATION ON NR 2 ENGINE, SHUT ENGINE DOWN, RETURNED JFK. FOUND FAULTY OIL PRESSURE TRANSMITTER, REPLACED SAME, OPERATION NORMAL. SUPPLEMENT 1: SHOP EVALUATION OF TRANSMITTER DID NOT FIND ANY FAULT. DUE TO LOW OIL PRESSUSDR DL76L950627Engine · high oil consumpAFTER REVIEWING OIL CONSUMPTION HISTORY, IT WAS DETERMINED CONSUMPTION RATE WAS BEYOND LIMITS, ENGINE WAS REMOVED AND ROUTED TO SHOP.SDR DL76L950597Floor Panel · dentedC-1 CARGO COMPARTMENT FLOOR PANEL 4R IS DENTED IN CENTER OF PANEL. FOUND AND REPAIRED PER HMV, PER SRM 53-00-50.SDR DL76S950548Skin · lightning strikeDURING LETTER CHECK INSP, FOUND 10 LIGHTNING STRIKES ON A/C BELLY (STARTING JUST AFT OF NOSE GEAR TO SECOND BODY DRAIN AFT OF E AND E COMPT AT 6 O'CLOCK POS) FUSELAGE SKIN BLENDED DAMAGE PER SRM 53-00-01, DYE CHECK OK. TREATED AREAS W/ALODINE.SDR DL76S950547Skin · lightning strikeFOUND DURING LETTER CHECK INSP, LIGHTNING STRIKE FOREWARD OF RIGHT LOWER PITOT TUBE ON FUSE SKIN BLENDED DAMAGE PER SRM 53-00-01 DYE CHK OK, TREATED AREA AND REPAINTED.SDR DL76S950546Aileron · lightning strikeDURING LETTER CHECK INSP, FOUND L/WING ODBD AILERON EVIDENCE OF LIGHTNING STRIKE INSTALLED PERMANENT REPAIR AS PER SRM 57-60-02 FIG 201, BALANCE NOT CHANGED REF 51-60-01, PAINTED REPAIR ON LEFT AILERON.SDR DL76L950553Wedge · delaminatedDURING HMV, FOUND RIGHT WING OUTBOARD FLAP TRAILING EDGE WEDGE WITH DELAMINATION AT 2 FEET OUTBOARD OF THE INB FLAP TRACK. REPAIRED PER SRM 57-53-01.SDR DL76L950518Flap · wornAT HMV, RT WING OUTBOARD FLAP WAS FOUND WITH WEAR DAMAGE AT INBOARD FORWARD EDGE AND AT THE INBOARD ATTACH FITTING. REPAIRED PER SRM 57-53-01 PG 205 WITH REFERENCE TO SRM 51-70-17.SDR DL76L950444Sensor · failedDURING CLIMB-OUT, HAD SLAT ASSYMETRY LIGHT VISUAL CHECK OK SLATS APPEARED UP. ACCOMPLISHED ABNORMAL PROCEDURES, RETURNED JFK. THE SLAT LIGHT CAME ON AT FLAPS 1 DEGREE TO FULL UP. INTERROGATED PSEU, HAD FAULT CODE 280, LEFT OUTER SLAT NR 5 SENSOR. REPLACED SDR DL76S952035Te Wedge · delaminationFOUND T/E DAMAGE DURING INSPECTION, REPLACE T/E WEDGE PER CMM 57-43-45, FOR NR 2 L/E SLAT PANEL.
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