Boeing 767-332
Service difficulty reports · 11,959
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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 = '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 DL76L972340Ballast · failedACRID ELECTRIC BURNING SMELL IN AFT AIRCRAFT 25 MINS AFTER TAKEOFF. CKED AFT GALLEY AND ALL CARGO COMPT FOR EVIDENCE OF SMELL. CKS OK, FOUND BALLAST IN AFT GALLEY HOT. REPLACED 2 AFT GALLEY BALLASTS AND DISCONNECTED REMAINING 2. FWD TO MCO AND PLCD PER MEL SDR DL76S972328Floorbeam · corrosionCORROSION WAS FOUND ON THE UPPER CAP AT FS 1480 AT LBL 30 AND ENTIRE RT SIDE. REPAIRED PER ERA330975-14.SDR DL76S972327Floorbeam · puncturedA NEW UPPER TEE CHORD WAS ADDED TO THE BEAM EXTRUSION PER SRM. DURING ACCOMPLISHMENT THE FLOORBEAM WEB WAS PUNCTURED. REPAIRED PER ERA 330971-14.SDR DL76S972326Seat Tracks · crackedSEAT TRACKS AT LBL AND RBL 54 WERE FOUND CRACKED IN THE VERTICAL WEB OF THE UPPER CHORD AT FS 786. REPAIRED PER ERA330946-14.SDR DL76S972325Keel Beam · corrodedLT KEEL BEAM HAD CORROSION AT STA 917. REPAIRED PER ERA 330983-14.SDR DL76S972324Floorbeam · crackedFS 246 FLOORBEAM WEB WAS FOUND WITH VERT CRACK APPROX 3 LONG AT RBL 20. THE OVERLYING STIFFENER WAS ALSO CRACKED. REPAIRED PER ERA 330992-14.SDR DL76S972280Skin · dentedFUSELAGE / SKIN / STA 1241 / STRG. 33L : REPAIR FOR SKIN DENT. THE SKIN JUST AFT OF THE STA 1241 FRAME WAS FOUND DENTED AT S-33L. NO UNDELYING STRUCTURE WAS FOUND DAMAGE. THE SKIN DENT WAS CUTOUT AND REPAIRED WITH A DOUBLER PER SRM. ER/A SDR DL76S972173Coffeemaker · failedELECTRICAL BURNING SMELL COMING FROM MID GALLEY AREA WHEN COFFEE MAKER IS USED. REPLACED COFFEEMAKER.SDR DL76S972265Frame · crackedFORWARD CARGO COMPARTMENT STA 544 FRAME UPPER CHORD HAD AN 8 INCH CRACK IN THE RADIUS OF THE HORIZONTAL FLANGE AT RBL 16. REPLACED FLANGE.SDR DL76S972140Skin · dentedA DENT WAS FOUND IN THE EXTERNAL SKIN AT STA 640 BETWEEN S31R AND S32R. THE DENT IS 2.5 BELOW AN EXISTING SRM SMALL SMALL HOLE REPAIR. REPAIRED PER ERA 330885-14.SDR DL76S972093Power Supply · inoperativeEMERGENCY FLOOR TRACK LIGHTS BETWEEN SEATS 10 AND 13 BOTH SIDES ARE OUT. REPLACED EMERGENCY FLOOR TRACK LIGHTS POWER SUPPLY ASSY M9008, OPS CK NORMAL.SDR DL76S972092Bulb · failedLT AFT OVERWING EMERGENCY LIGHT OUT. RELAMPED SAME, OPS CK NORMAL.SDR DL76S972089Hyd Hose · rupturedDURING TAXI IN LOST CENTER HYDRAULIC SYSTEM FLUID AND PRESS. FOUND ADP PRESSURE LINE LEAKING. REPLACED SAME.SDR DL76L972095Battery · dischargedON L/O, FOUND LT AFT DOOR SLIDE AND LT AFT GROUND AREA SLIDE LIGHT INOP. REPLACED BATTERY.SDR DL76S972060Chiller · failedDURING TURN TO FINAL, SMELLED FUMES IN COCKPIT. F/AS COULD NOT SMELL THE FUMES IN CABIN AND COULD NOT DETERMINE THE SOURCE. WHILE TAXIING IN RECEIVED AN EICAS LT PACK TEMP MSG WITH INOP, LT IN LT PACK SW. ODD SMELL COMING FROM FORWARD CHILLER. PULLED AND CSDR DL76L972051Hsi · failedSMOKE IN CKPT APPEARS TO BE COMING FROM INSTRUMENT PANEL, AREA ON COPILOTS SIDE IN THE AREA OF ADI/HSI. DOWNPOWERED A/C REMOVED COPILOTS INSTRUMENTS AND INSPECTED LIGHTING PANEL. REPLACED F/O ADI/HSI DUE TO EVIDENCE OF SMOKE. APPLIED EXTERNAL AND APU PWR. SDR DL76S972111Skin · corrosionDURING ACCOMPLISHMENT OF EO 1-60000-3, CORROSION WAS FOUND DIRECTLY UNDER THE DRAIN SCREEN LOCATED AT APPROXIMATELY LBL 70. THE RESULTING BLENDS, WITH A MAXIMUM DEPTH OF .155, ARE SHOWN ON FIGURE 1. TO FACILITATE INSTALLATION OF A REPAIR DOUBLER UNDER THE LBSDR DL76S972022Fseu · failedRECEIVED LEADING EDGE SLAT ASSYM MSG AFTER SELECTING FLAPS FROM FLAPS ONE TO UP. REPLACED FSEU AND NR 10 SLAT INBOARD SENSOR, BITE CHECKS GOOD.SDR DL76S972039Floorbeam Web · crackedTHE FS 246 FLOORBEAM WEB WAS FOUND WITH A VERTICAL CRACK APPROX 3 LONG AT RBL 20. ADDITIONALLY, THE ATTACHING VERTICAL STIFFENER WAS FOUND CRACKED. REPAIRED PER ERA 330789-14.SDR DL76S972038Seat Track · crackedTHE FUSELAGE SEAT TRACKS LOCATED AT RBL 33, LBL 54 AND RBL 54 WERE FOUND CRACKED IN THE VERTICAL WEB OF THE UPPER CHORD AT APPROX FS 786. REPAIRED PER ERA 330781-14.SDR DL76S972029Skin · damagedUNIDENTIFIED SKIN REPAIR FOUND AT FS 640 JUST ABOVE S31R. FINAL CUTOUT IN SKIN IS 3.25 BY 2.75. REPAIRED PER PER ERA 361621-14.SDR DL76S972027Skin · dentedGROUND DAMAGE FOUND AT APPROX FS 510 BETWEEN STRINGERS 33L AND 35L. DAMAGE CUTOUT AND REPAIRED PER ERA 330797-14.SDR DL76L971908Egt Indication · highLT ENGINE EGT EXCEEDED MAX CONTINOUS EGT IN CLIMB. EGT REACHED 626 DEG, THRUST LEVER WAS PULLED BACK MANUALLY TO PREVENT EGT GOING HIGHER. EGT WAS 60 TO 80 DEG HIGHER THAN RT ENG FOR SAME EPR SETTING. NO SURGE OR STALL INDICATED ON ENGINE EXCEEDANCE PAGE. SDR DL76S971829Pseu · failedNOSE A/G DISAGREE AND HORN WITH CONFIG WARN. BITE ON PSEU SHOWS S266 BAD. REPLACED, NO HELP. REPLACED PSEU, CKS OK.SDR DL76S971834Engine · failedPASSING FL 23500 ABOUT 10 SEC AFTER SELECTING CLB PWR, LEFT ENG COMPRESSOR STALL (5 BANGS). PULLED TO IDLE MAX TEMP 928 FOR 4 SEC, INDICATED AIRSPD 310 KTS. BEGAN DESCENT, LEFT ENG COMPRESSOR STALLED AGAIN 3 TIMES AS PWR WAS REDUCED. SHUTDOWN ENG PASSING 8SDR DL76L971846Sam Module · failedEICAS/OVERHEAD RUDDER RATIO AND AILERON LOCK-OUT MESSAGE CAME ON AFTER LEVEL OFF AND A/P DISCONNECT. TRIED RESET, NO HELP. A/C SUSTAINED LIGHTNING STRIKE AFTER TAKEOFF. REPLACED LEFT AND RIGHT SAM MODULES PER MM. MCDP TEST NUMBER 40 ALL OK. PERFORMED LIGHSDR DL76S971922Floorbeam · crackedTHE FUSELAGE SEAT TRACKS LOCATED AT RBL 33, LBL 54, AND RBL 54 WERE FOUND CRACKED IN THE VERTICAL WEB OF THE UPPER CHORD AT APPROXIMATELY FS 786 AS DESCRIBED IN BOEING SB 767-57-0029. THE VERTICAL WEB IS M/F FROM .063 THK 2024-T3 AL MATERIAL. IN ADDITION, TOSDR DL76S971745Floorbeam · crackedTHE FS 246 FLOORBEAM WEB WAS FOUND WITH A 3.25 CRACK AT RBL 20. REPAIRED PER DAL ER/A.SDR DL76S971625Light · inoperativePIREP - EMERGENCY OVERWING RIGHT EMERGENCY TRACK LIGHTING FLOOR LIGHT DAMAGED. REINSTALLED LIGHT IN FLOOR TRACK.SDR DL76S971610Threshold · corrodedTHE BULK CARGO COMPARTMENT DOOR THRESHOLD COVER PLATE WAS REPLACED DUE TO CORROSION.SDR DL76S971563Power Supply · inoperativeLEFT WING SLIDE EMERGENCY ILLUMINATION LIGHTS AT STATION 1197, 1230 AND LEFT AFT DOOR EMERGENCY ILLUMINATION LIGHT INOP. REPLACED M738 POWER SUPPLY AND BATTERY PACK. OPS CHECK GOOD PER MM.SDR DL76S971560Skin · delaminatedTHE NR 6 SLAT TRAILING EDGE WEDGE UPPER SURFACE WAS FOUND DELAMINATED. THE DELAMINATION IS LOCATED 10 FROM THE AFT EDGE EDGE, 82 FROM THE INBOARD END AND IS APPROX 3 IN DIAMETER. THE DELAMINATED AREA WAS REPAIRED PER B767 SRM, CHAPT 51-70-10, FIGURE 9.SDR DL76L971500Skin · dentedTHE FUSELAGE SKIN AND UNDERLYING STRUCTURE WAS DAMAGED BETWEEN STA 588 AND 634 BETWEEN STR 35 TO 38R. THE TO DAMAGE RESULTED IN MULTIPLE DENTS IN THE FUSELAGE SKIN ABOVE AND BELOW STR 36R SKIN LAP JUST AFT OF STA 588 FRAME. STR 35, 36, 37R WERE DEFORMED IN TSDR DL76P971476Skin · corrosionCORROSION WAS FOUND ON THE FUSELAGE SKIN UNDER THE LT FORWRD AIRFONE ANTENNA AT STA 686 FROM STR 35L TO 36L. THE DAMAGE RESULTED IN A CUTOUT MEASURING 6.75 BY 2.75. A DOUBLER WAS INSTALLED AND APPROVED PER FAA/DER FORM 8110-3, DER DESIGNATION SO-775, DTD 7-2SDR DL76L971436Coffeemaker · odorCOFFEEMAKER IN MID GALLEY GAVE OFF SMOKEY-ELECTRICAL SMELL 6 HRS INTO FLIGHT. REPLACED MID AFT AND RIGHT AFT COFFEEMAKERS, SYSTEM OPS CHECKS NORMAL.SDR DL76L971430Spin Brake · brokenFOUND RT NOSE WHEEL SPIN DOWN BRAKE ARM BROKEN AND MISSING. REPLACED SPIN BRAKE ASSY.SDR DL76P971414Retract Mech · lack of lubeLE SLAT ASSY EICAS MESSAGE AND LEADING EDGE LIGHT DID BITE CK ON PROX BOX CHECKED FSEC CHECKED AIR GAP ON NR 12 SLAT ALL OK. FOUND NR 12 SLAT CHETTERING LUBED SLAT GRD OPS NML NO FAULTS LOGGED NOTE: CHECKED SENSORS GAP FULL UP ALL OK AT 20 DEGREES FLAP SENSORSDR DL76S971372Bulb · failedR-3 DOOR EMER EXIT LIGHT INOP. RELAMPED RT OVERWING MOST AFT EMER LIGHT.SDR DL76L971316Bpcu · failedLEVEL AT FL310 ON CENTER AUTOPILOT, A/C EXPERIENCED A SHARP PITCH BUMP OR SPIKE. AUTOTHOTTLES, ALL GALLEY POWER DROPPED OFF MOMENTARLIY, GALLEY POWER RECOVERED AUTOMATICALLY. RECONNECTED AUTOTHOTTLES, NO PROBLEMS REMAINEDER OF FLIGHT. BITE MCDP AND BPCU. BSDR DL76L971314Engine · failedNR 1 ENG STALLED WHEN ADVANCED FOR TAKEOFF. REPLACED NR 1 ENGINE PER CARD DECK. TEST FLIGHT PERFORMED, ALL NORMAL.SDR DL76S971347Skin · delaminatedTHE NR 9 LE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE A 3.5 DIAMETER SECTION OF THE UPPER SKIN DELAMINATED. THE DAMAGE IS LOCATED IN THE CENTER OF THE SLAT WEDGE FWD/ AFT AND INB'D/OUTB'D. THE DAMAGED SECTION WAS REPAIRED PER B767 SRM 57-43-02, FIGURE 201.SDR DL76S971264Bulb · shortedDURING CRUISE 37000 FT 1 HR INTO FLT, SMELLED ELECTRICAL SMELL. SHUT OFF UTILITY BUSSES PULLED C/BS U6 U33. F/A REPORTED, WORSE IN LT HAND F/C TURNED OFF LT PACK WHEN PAX IN 14A. REPORTED PUFF OF SMOKE FROM LT FLOOR BOARD GRAY IN COLOR. RECEIVED PRIORITY HSDR DL76L971254Sensor · malfunctionedEICAS MESS RT ENG BLEED OFF AND RT BLEED OVERHEAT OFF. LANDED JFK FOR MTC. FOUND FAN AIR VALVE TEMP SENSOR AT FAULT. LOCKED FAN AIR VLV INTO INTERMEDIATE POSTION AND FWD TO MCO PER MEL 36-12-02A. REPLACED FAN AIR SENSOR AND OPS CHECKED IN VIE. SYSTEM CHECKSDR DL76S971211Hyd Line · leakingCTR HYD SYS FAILED WHEN LOWERING MLG. FOUND PRESS LINE FROM ADP TO BULKHEAD LEAKING. REPLACED LINE, SERVICED HYD SYS AND HAD 1.8 GAL REMAINING. LEAK CKD OK.SDR DL76G971210Engine · failedWHILE PERFORMING NR 1 SERVICE CHECK, FOUND METAL ON MASTER AND TRANSFER GEARBOX CHIP, A SUMP CHIP DETECTORS. REPLACING NR 2 ENGINE.SDR DL76L971175Sensor · dirtyAFT LAV INOP LIGHT ILLUMINATED ON LAV PANEL IN AFT GALLEY. ASSOCIATED LAVS, NO FLUSH. TRIED RESET PER PRM WITH NO SUCCESS. AIRCRAFT RETURNED TO JFK. CLEANED TANK SENSOR, OPS CHECK GOOD.SDR DL76G971174Fan Blades · lack of lubeFAN VIBRATION ON LEFT ENGINE WENT TO 5.0 ON INITIAL CLIMB-OUT 4.2-4.5 IN CRUISE AT FL 310/330/350. COULD FEEL VIBS ONLY AT IDLE OR LOW PWR SETTINGS. REMOVED AND LUBED FAN BLADES PER MM. LUBED PER OPN 4021. PERFORMED ENG VIB SURVEY WITH PBS 4000 IN ACCORD WISDR DL76S971196Intercostal · crackedDRIVE MOTOR SUPPORT/BAG BIN FLOOR SUPPORT CRACKED AT FS 560 P/N 451T2503-2. REPLACED INTERCOSTAL PER SRM 51-70-13-0-1.SDR DL76S971108Valve · inoperativeNOSE GEAR DID NOT RETRACT ON T/O, DURING GEAR RETRACTION A/C SHUDDERED, CENTER HYD SYS EICAS MSG CAME ON, CENTER HYD PUMP LOW PRESS LTS CAME ON. DEMAND PUMP LOW PRESS LTS CAME ON WHEN GEAR HANDLE WAS PLACED IN DOWN POSITION. CENTER HYD SYS RETURNED TO NORMALSDR DL76L971114Control Module · leakingC HYDRAULIC SYSTEM LEAKING IN CRUISE. QTY DROPPED TO 0.32. DURING GEAR/FLAP EXTENSION QTY DROPPED TO 0.08. CREW DECLARED EMERGENCY. MX FOUND RT STAB TRIM CONTROL MODULE LEAKING. REPLACED RIGHT STAB TRIM CONTROL MODULE. OPS CHECK GOOD.
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