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 DL76G011318Window · crackedF/O RT WINDOW CRACKED ON LANDING. REPLACED SAME.SDR DL76L011315Dau · failedSTATUS MSG IN-FLT, FLT DATA ACQ. PULLED C/B J7 AND J8. ELEC SMELL JUST PRIOR TO MESSAGE. REPLACED DFDAU AND FLT DATA REC PER MM. OPS NORMAL. MTC REPORTED DFDAU HAD STRONG ELEC SMELL.SDR DL76S020919Light · inoperativeFOUND ON L/O CHECK, DOOR R1 EXT EMERGENCY SLIDE LIGHT INOP. REPLACED LIGHT ASSY, CHECK GOOD.SDR DL76L011289Engine · leakingON T/O FROM BRU REPORTED SMOKE IN CABIN.CLEARED AFTER 15 MINUTES OF FLT.ATL MTC FOUND OIL LEAKING FROM SPINNER. REPLACED ENGINE.SDR DL76L011288Yoke · erraticON CLIMBOUT PASS 250 KTS THE YOKE STARTED TO OSCILLATE IN THE ELEVATOR WITH OR WITHOUT THE AUTOPILOT ON. IT DID SLIGHTLY DAMPER WITH THE LT AUTOPILOT BUT NOT THE CNTR OR RT AUTOPILOT. THOROUGHLY INSPECTED AIRCRAFT, UNABLE TO DUPLICATE.SDR DL76L011282Fan · failedEICAS ADVISORY L RECIR FAN AND INOP LIGHT ON OVERHEAD PANEL.PRIOR TO EICAS MESSAGE - STRONG ELECTRICAL SMELL OF SMOKE INALL CABINS. REPLACED FAN SDR DL76K011278Connector · separatedAISLE SIDE WHITE EMRGENCY LITE INOP AT 3EF. SECURED CONNECTION ON ASSEMBLY.SDR DL76K011266Rod · brokenLANDING GEAR DISAGREE WITH GEAR DOOR ADVISORY WHEN GEAR HANDLE PLACED UP AFTER T/O. NR 8 BRAKE ANTI-ROTATION ROD BROKE. REPLACED BRAKE AND LINE.SDR DL76G011262Odor · detectedATB FOR ELECTRICAL SMELL IN AFT GALLEY...CREW TURNED OFF OVENS AND RECIRC FANS AND UTILITY BUSSES AND SMELL DISSIPATED. MAD MTC INVESTIGATING.SDR DL76G011267Hydraulic Line · failedNR 7 SPOILER CONTROL ACTUATOR PRESSURE LINE AT ACTUATOR PULLED OUT OF B-NUT BREAKING LINE AND CAUSING COMPLETE LOSS OF RIGHT HYDRAULIC SYSTEM FLUID. REPLACED LINE.SDR DL76S011253Light · inoperativeLT AFT DOOR EXT EMERGENCY LIGHT INOP RELAMPED. CKS OK.SDR DL76G011252Line · crackedRT HYD SYSTEM FLUID LOSS.REPLACED NO.7 SPOILER ACTUATOR LINE WITH TEMP LINE.FWD TO MCO. SDR DL76P011251Chip Detector · crackedTHE MAIN ENGINE CHIP DETECTOR BOSS SLOTS (3 EA) HAD BEGUN TO FAIL (CRACK) AT THE WEAKEST AREA OF THE BOSS. REPLACED THE BOSS AND DETECTORSDR DL76P011245Skin · dentedFUSELAGE SKIN DENTED 4" FWD OF STA 1395, AT S-34R AND STA 1373 BETWEEN S-34R AND S-35R. BOTH DAMAGE LOCATIONS ARE TRIMMED OUT AND DOUBLER/TRIPLER INSTALLED. CORRECTIVE ACTION: ER/A 397815-14SDR DL76L011243Pump · leaking4 HOURS INTO FLIGHT, CTR HYD "RSVR" LIGHT AND "CTR HYD QTY" EICAS MESSAGE CAME ON. CTR HYD QUANTITY INDICATED 0.47RF. SWITCHED OFF ELEC PUMPS AND QTY CONTINUED TO DECREASE. SWITCHED ELEC PUMPS BACK ON AND ADP OFF AND QUANTITY CONTINUED TO DECREASE. SWITCHED SDR DL76L011239Coffeemaker · dirtyFLT DIVERTED TO BOS WITH BURNING SMELL IN AFT GALLEY. REMOVED ALL AFT COFFEEMAKERS AND CLEANED AREA OF COFFEE RESIDUE. INSPECTED AFT GALLEY FOR OTHER SOURCE OF SMELL. NONE FOUND. REPLACED NR 1 AND NR 3 COFFEEMAKERS PRECAUTIONARY.SDR DL76L011240Engine · malfunctionedHEARD A THUMP ON RIGHT SIDE DURING APPROACH. PASSENGER ON RIGHT SIDE SAW A FLASH OF LIGHT AT THE SAME TIME. NO ABNORMAL ENGINE INDICATIONS, BUT SUSPECT SMALL COMPRESSOR STALL. REMOVED AND REPLACED RIGHT ENGINE PER ROUTINE CARD DECK 1-27.SDR DL76S011205Engine · overtempRT ENG OVERTEMP ON T/O. EGT943 T/O DISCONTINUED AT 90K. CHECKED INLET AND EXH, RAN ENG PER PFHB MAX PWR ASSURANCE TEST. CLEARED EICAS COMPUTER, MSG 943 FOR 3 SEC OVERTEMP AREA A-MCC ADVISED.SDR DL76G011172Fan · faultyDIVERTED TO YQX DUE TO SMOKE IN CABIN. FOUND RT RECIRC FAN AT FAULT. FWD TO MCO PER MEL 21-25-01A.SDR DL76K011167Fairing · separatedDURING FLT BALL CAP FAIRING DEPARTED A/C CAUSING DAMAGE TO THE NR 7/8 SLATS AND STRUCTURE UNDERNEATH FAIRING. INSPECTED AREA REPLACED UPPER RT FWD PYLON FAIRING AND REPAIRED DAMAGE ON NR CARDS 1-11. REPLACED 8 SLAT ON N/R CARD 10 A ROUTINE JIC OPN 7008AD ON SDR DL76K011158Battery Pack · dischargedAFT LEFT EXTERIOR EMER LIGHTS INOP. REPLACED BATTERY PACK.SDR DL76S011153Engine · malfunctionedRT ENG EGT EXCEEDED 979 DURING T/O. N2 VIBS 5.0 AND RT HP BLEED LIGHT ON. AIRCRAFT RETURNED TO ATL AND ON APPROACH INTO ATL RT ENG WAS SHUTDOWN BY CREW DUE EGT CONTINUING TO RISE. REMOVED AND REPLACED NR 2 ENG.SDR DL76G011126Hydraulic Line · separatedRT HYDRAULIC SYSTEM QUANTITY AND PRESSURE WENT TO ZERO DURING DESCENT AND APPROACH. ACCOMPANIED BY A SPOILERS EICAS MESSAGE. NO ABNORMAL CONTROL INPUTS WERE FELT. ACCOMPLISHED PROCEDURES PER POM. FOUND HYD PRESSURE LINE TO NR 7 SPOILER PCA SEPARATED FROM PSDR DL76G011125Fmc · malfunctionedDUAL FMC FAIL. LEG PAGES BLANK ON BOTH CALLS. UNABLE TO ENTER ANY FIX LEGS ON BOTH CDU'S. RESET C/BS. BITE HISTORY ON BOTH CDU'S SHOW NO FAULTS. NO FMC FAILURES / LIGHTS. AS PRECAUTION REMOVED BOTH CDU, CLEAN FILTERS INSPECT CONNECTORS AND REINSTALL. CDUSDR DL76G011116Valve · failedT/O DISCONTINUED. RT WING ANTI-ICE VALVE ILLUMINATED, APPROX 100 KNOTS. REMOVED AND REPLACED WING TAI VALVE. OPS CKS OK. PERFORMED ENG RUN VALVE LIGHT REMAINED OFF. CK OK PER M/M.SDR DL76G011109Detector · dirtyGOT FWD EQP OVERHEAT LT ON TAXI-OUT. WENT TO STANDBY PER MANUALS FOR 5 MINS NO LIGHT. TOOK OFF GOT LITE AGAIN AFTER T/O WENT TO OVRD PER POM AND RETURNED TO AIRPORT C/A - ECS PG SHOWS FLT DK SUP FLOW MAINT MSG. PER F.I.M. CLEANED TS163 SENSORSDR DL76L011101Engine · failedACFT ATB DUE TO NBR 1 ENGINE FLUX. REPLACED FMU. SDR DL76S011076Harness · defectiveSEAT 37A EMERGENCY LIGHT INOP ON TEST. REPLACED LIGHT HARNESS.SDR DL76S011074Harness · burnedWORKING MCO APU ELEC INOP. FOUND GENERATOR FEEDER CABLE BURNT. CABLE SENT TO SHOP WITH OLD GENERATOR. REPLACED CABLE.SDR DL76L011045Shutoff Valve · failedON TAKEOFF DUCT PRESS FLUCTUATED PLUS MINUS 15 PSI. REPLACED PRSOV PER MM. CKS OK.SDR DL76S011040Frame · crackedBOLT HOLE HFEC INSPECTION OF THE LT FWD OUTER CHORD OF THE FS 1809.5 BULKHEAD REVEALED A SMALL CRACK IN A FASTENER HOLE. THE FASTENER LOCATION IS COMMON TO THE INSPECTION AREA OF BAC S/B 767-53-0078 AND AD 2001-09-13. THE CRACKED SECTION OF CAP WAS CUT AND RSDR DL76S011039Frame · crackedBOLT HOLE HFEC INSPECTION OF FASTENERS COMMON TO THE RT FWD OUTER CHORD OF THE FS 1809.5 BULKHEAD INDICATED SMALL CRACKS IN 3 FASTENER HOLES. THE HOLES ARE COMMON TO THE INSPECTION AREA OF BAC S/B 767-53-0078 AND AD 2001-09-13. THE CRACKED SECTION OF CHORD WSDR DL76L011032Idg · failedDIVERTED TO JFK DUE TO LT IDG FAILED AND GEN BREAKER TRIPPED. REPLACED LT IDG.SDR DL76S011012Pin · backed outPAX SEAT 31A EMERGENCY LIGHTS WON`T TEST. FOUND PULLED/BACKED OUT PIN IN SEAT HARNESS. REPAIRED SAME.SDR DL76S011011Light · inoperativeR-1 DOOR EXTERIOR EMERGENCY LIGHT INOP. REPLACED BULB, OP CK GOOD.SDR DL76S011008Mec · malfunctionedDURING FLIGHT NR 2 ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. ENGINE SHUT DOWN, LANDED SINGLE ENGINE. CHECKED THROTTLE CABLES, ALL SECURE. REMOVED AND REPLACED MECPRE M/M. LEAK AND RUN CHECK GOOD.SDR DL76S010981Fseu · shortedAT LEVEL OFF GOT FLAP/SLAT ELEC MESSAGE C/B P11G16 POPPED SMOKE IN COCKPIT. FOUND FLAP/SLAT ELECTRONICS UNIT HAD A TRANSFORMER THAT HAD OVERHEATED. REPLACED THE FLAP / SLAT ELECTRONICS UNIT AND TESTED PER MAINT MANUAL. OPERATED FLAPS IN ALTERNATE AND NORMAL MOSDR DL76G010978Skin · dentedFUSELAGE / SKIN ASSY / FS 1373 / STRG. 27R : GROUND DAMAGE REPAIR THE FUSELAGE SKIN WAS BADLY DENTED BY GROUND EQUIPMENT AT FS 1373 NEAR STRINGER 27R. AN UNDERLYING FRAME SHEAR CLIP AND INTERCOSTAL WERESDR DL76L010958Oxygen System · missingDURING INSPECTION OF OXYGEN MASK EO PER AD FOUND NO OXYGEN EQUIPMENT IN PSU ABOVE SEATS 20 A AND B. NO OXYGEN GENERATOR OR MASKS OR ANYTHING. EO 1-85011-12AD REPLACED PSU AND OXYGEN GEN. ON, OFF A 351001259, B 353201010.SDR DL76G010955Windshield · crackedCAPTS WINDSHIELD OUTER LAYER SHATTERED. REPLACED LT FWD WINDSHIELD AND WINDOW HEAT CONTROLLER PER M/M TORQUED PER ERA 388709-14. ALL CHECKS GOOD.SDR DL76S010953Unknown · odorAT FL 410 TERRAIN SYSTEM STARTED WARNING OF TERRAIN, NOTICED ODOR OF MELTING PLASTIC. CK UNDER O-CARE SHIELD WIRING OR ODOR FOUND FIBERGLASS ON F/O ALT. REPOSITION, OK. DROPPED O/H PNL, ALL NORMAL. DROPPED C/B BOS NORMAL. CK E/E BUNDLES P51 PNL AREA NORMASDR DL76S010934Gasket · leakingLT ENG FIRE INDICATIONS SHORTLY AFTER TAKEOFF THROTTLE. RETARDED TO IDLE AND FIRE INDICATION WENT OUT. FOUND ALL THERMOCOUPLE GASKETS LEAKING. REPLACED GASKETS, CK OK ON RUN.SDR DL76L010968Bearing · failedFOUND METAL ON MCD. REINSPECTION SHOWED MORE FINES. ANALYSIS REVEALED BEARING MATERIAL. REPLACED ENGINE.SDR DL76L010913Fan · faultySMOKE IN COCKPIT. ALSO GOT FWD EQ EXH FAN STATUS MSG WITH POPPED CB. WENT TO OVRD ON EQUIP COOLING AND SMOKE DISSIPATED. ON LANDING GOT NO COOLING LIGHT AND WENT TO STBYSUSPECT FWD EQ EXH FAN BURNED OUT. FWD TO MCO. OPERATE PER MEL 21-58-04B. SDR DL76K010890Harness · damagedSEAT 2 EF EMERGENCY LIGHTS INOP. REPAIRED DAMAGED SEAT HARNESS.SDR DL76L010889Charger · failedCREW REPORTED BATTERY CHARGER MSG WITH VOLTAGE AT 24 VOLTS. REPLACED BATTERY CHARGER.SDR DL76S010873Line · leakingLT ENG GEN DRIVE LIGHT CAME ON DURING T/O ROLL. DISCONTINUED T/O AT APPROX 90 KNOTS GROSS WGT 295000. FOUND OIL LINE FROM IDG FILTER TO OIL COOLER LEAKING. REPLACED SAME. MOTORED ENG LEAK CKS OK. RAN ENG IDG. OPERATION AND INDICATION NORMAL.SDR DL76L010859Lavatory · inoperativeDIVERTED TO CCS DUE TO LAV SYSTEMS INOP. SERVICED LAVS.SDR DL76L010848Fmu · failedFLUCTUATING PARAMETERS ON NR 2 ENGINE AT CRUISE. REPLACED FMU.SDR DL76S010854Stiffener · crackedCRACKS DISCOVERED IN THE RBL AND LBL 10 VERTICAL STIFFENERS OF THE WING CENTER SECTION FRONT SPAR. THE DAMAGE IS IN THE WEB OF EACH OF THE STIFFENERS AT THE OVERWING LONGITUDINAL FLOORBEAM TO STIFFENER JOINT. ER/A 397596-14.
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