Boeing 767-232
Service difficulty reports · 2,991
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 = '767232' 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 = '767232' 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 ABXA060174Sensor · misinstalledAFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. FOUND LT GEAR TILT SENSOR'S IMPROPERLY INSTALLED. REMOVED REINSTALLED IAW 767 M/M 32-09-02. ADJUSTED LT & RT MAIN TILT SENSORS IAW 767 M/M 32-09-02, COMPLIED WITH GEAR SWING IAW 767 M/M 32-32-00 GEAR RETRACTION SDR DL767060016Skin · crackedCRACK DAMAGE WAS FOUND ON THE NR 8 LEADING EDGE SLAT, END RIB AT OSS 531.611. REPAIRED ERA 452170-14.SDR DL767050678Line · failedON TOUCHDOWN LOST CTR HYD SYSTEM. FOUND DISCONNECT ON ADP PRESSURE LINE FAILED. REPLACED SAME.SDR DL767050670Shutoff Valve · leakingEICAS MESSAGE -L/E SLAT DISAGREE- ILLUMINATED WHEN THE FLAP LEVER WAS PLACED AT 1 DEGREE POSITION. FOLLOWED QRH PROC AND SLATS EXTENDED ELECTRICALLY AND FLAPS EXTENDED HYDRAULICALLY. L/E SLAT DISAGREE MSG WAS NOT ILLUMINATED DURING MTC CHECK. PERFORMED BITESDR DL767050669Fan · seizedFUMES REPORTED IN MID CABIN OVERHEAD AREA, DIVERSION RDU. FOUND GASPER FAN AT FAULT. REPLACED SAME.SDR DL767050551Wire · shortedNOTICED ELECTRICAL PLASTIC ODOR NEAR CAPTAINS GLARESHIELD LIGHT CONTROL PANEL, NEAR LOWER LEFT CORNER OF WINDSCREEN. FOUND L1 WINDOW SENSOR CONNECTION BAD AND SHORTED. REMOVED AND REPLACED L1 WINDOW ASSY PER AMM.SDR DL767050518Bulkhead · crackedDAMAGE FOUND ON FS 1582 BULKHEAD AT STIFFENER 14L LAPJOINT BETWEEN TEAR STRAPS 4 AND 5. REPAIRED USING DOUBLER/STRUCTURAL SHIMS ON AFT SIDE OF BULKHEAD. BOEING APPROVED WITH AMOC TO AD 2005-03-11.SDR DL767050481Power Supply · inoperativeEMERGENCY LIGHTS INOP THROUGHOUT CABIN. REPLACED M9008 POWER SUPPLY, CHECKS OK.SDR DL767050386Yaw Damper · malfunctionedUNCOMMANDED RUDDER INPUT AT ROTATION, THOROUGHLY CHECKED SYSTEM. UNABLE TO DUPLICATE OR FIND FAULT.SDR DL767050317Skin · corrodedREPAIR OF CORROSION WAS FOUND AT SEVERAL LOCATIONS ALONG STRINGER 38R AND 39R AF FS 434. THE DAMAGE TO THE BUTT SPLICE STRIP WAS BLENDED AND HFEC INSPECTED. SKIN DAMAGE WAS REPAIRED PER THE SRM 53-00-01 FIG 201. INFORMATION WAS PROVIDED TO BOEING AND BOEINGSDR DL767050267Shutoff Valve · sticksWHEN POWER INITIALLY REDUCED TO START INITIAL DESCENT A SMELL DEVELOPED IN THE AIRCRAFT. REPLACED NR 1 HPSOV.SDR DL767050144Skin · dentedTHE FUSELAGE SKIN WAS DAMAGED BY GROUND EQUIPMENT AT FS 643 NEAR STRINGER 28R. THE DAMAGE WAS REMOVED WITH A 4.5 X 3 INCH CUTOUT IN THE SKIN. THE SKIN WAS REPAIRED WITH AN ALUMINUM DOUBLER PER ER/A 097220-14, REV A.SDR DL767050118Pressure Blkhd · crackedMFEC INSPECTION OF THE AFT PRESSURE DOME WEB AT THE STIFFENER 16R LAP JOINT REVEALED 2 CRACKS IN THE AFT WEB PIECE. BHEC INSPECTION REVEALED 3 MORE CRACKED HOLES. THE DAMAGED SECTION OF WEB WAS REMOVED WITH A CUT OUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBSDR DL767050080Line · leakingRT HYD SYS FAILURE. RT HYD SYS QTY DROPPED QUICKLY SUGGESTING A LEAK. FOUND RT ENGINE PRESSURE LINE CHAFED THROUGH, REPLACED SAME.SDR DL767050067Engine · failedWHILE RUNNING APU ON GND WITH PACKS ON MTC NOTICED SMOKE IN THE CABIN AND SMOKE OUT OF APU EXHAUST. FOUND APU COMPRESSOR OUTLET DRIPPING OIL. REPLACED APU.SDR DL767050049Pseu · malfunctionedON FLAP RETRACTION GOT L/E FLAP DISAGREE. ON FINAL GOT L/E FLAP ASYM PLI WAS FLUCTUATING POS 5 DEG TO POS 12 DEG. T/S PER FIM 27-81-00. PSEU FAULTS CARD NR 10 AND SHOWS CODES 305 421 422 AND 301. REPLACED PSEU. FSEU SHOWS OUTBD SLAT RVDT MISSING AND 603 FLSDR DL767041140Cooling Fan · malfunctionedFWD EQUIPMENT COOLING FAN MESSAGE WITH SMELL. REPLACED SAME.SDR DL767041130Odor · detectedDURING CLIMBOUT, SMELL NOTICED IN COCKPIT, LIKE BURNING PLASTIC. RAN ENGINES AND PACKS, UNABLE TO DUPLICATE. SUSPECT RECENT FAN LUBE.SDR DL767041108Circuit Card · intermittentINTERMITTENT FWD CARGO FIRE LIGHT PLUS BELL CAME ON DURING TAXI IN. REPLACED FIRE CARD M10427 IN P-54 PANEL. SYSTEM CHECKS NORMAL PER M/M. PER CVG FIRE DEPT, NO EVIDENCE OF SMOKE, ODOR, OR FIRE FOUND.SDR DL767041075Bolt · misinstalledFOUND BY FAA INSPECTOR, RIGHT MLG WING DOOR LOWER AFT MOUNT BOLT INSTALLED INCORRECTLY. BOLT IS DAMAGED AND CENTER SHIMS ARE MISSING. INSTALLED NEW BOLT AND HARDWARE PER AMM 32-12-06 AND IPC32-12-01-05 RIGHT MLG WING DOOR LOWER AFT MOUNT INSTALLATIONS NOW COSDR DL767040957Odor · detectedRAN ENGINES AND PACKS. INSPECTED AIRCRAFT, UNABLE TO DUPLICATE.SDR DL767040816Pump · failedON LANDING ROLL WHILE EXITING THE RUNWAY 26R LOST ALL CTR HYD FLUID. REPLACED ADP.SDR DL767040807Fan · unserviceableELECTRICAL ODOR IN COCKPIT ON 3 SEPARATE OCASSIONS, IT WAS ALSO SMELLED THROUGHOUT CABIN LASTING ONLY A FEW MINUTES THEN DISSIPATING. INSTRUCTED F/A TO TURN OFF CHILLERS AT FIRST OCCURRENCE AND IT CLEARED THEN IT RETURNED 2 MORE TIMES. FOUND LT RECIRC FAN TOSDR DL767040792Pressure Switch · inoperativeRIGHT ENG FUEL FILTER EICAS MSG ON TAKEOFF, ATB. REPLACED NR 2 ENG FUEL FILTER/FUEL PRESS SW. NO DEBRIS FOUND. OK FOR SERVICE PER FIM 73-11-00 PG 106.SDR DL767040780Fan · inoperativeFORWARD EQ SUPPLY FAN 2 EICAS MSG WITH EQUIP COOLING SUPPLY FAN 2 CB POPPED STRONG ELECTRICAL FUMES IN COCKPIT, REPLACED FAN.SDR DL767040726Charger · inoperativeON SERVICE CHECK FOUND RT AFT EXT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND BATTERY CHARGER PER M/M. CHECKS GOOD.SDR DL767040725Battery · inoperativeON SERVICE CHECK FOUND RT AFT EXT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND BATTERY CHARGER PER M/M. CHECKS GOOD.SDR DL767040724Charger · inoperativeON SERVICE CHECK FOUND LT SIDE AFT EXT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY AND CHARGER PER M/M, CHECKS GOOD.SDR DL767040723Battery · inoperativeON SERVICE CHECK FOUND LT SIDE AFT EXT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY AND CHARGER PER M/M, CHECKS GOOD.SDR DL767040712Valve · failedAFTER TOUCHDOWN LOST CENTER HYDRAULIC SYSTEM C HYD QTY. FOUND CHECK VALVE ON RAT BROKEN. REPLACED SAME.SDR DL767040679Wedge · delaminatedIB AFT FLAP TE WEDGE WAS FOUND WITH DAMAGE TO THE LOWER SKIN AND CORE. REPAIRED IAW ERA 091685-14.SDR DL767040678Skin · crackedRT LOWER WING SKIN SIDE LINK FITTING ATTACH FASTENER FOUND CRACKED. REPAIRED IAW ERA 091372-14AD.SDR DL767040671Support Beam · corrodedLEFT AND RIGHT INBOARD FLAP INBOARD AND OUTBOARD SUPPORTS CORRODED. REPAIRED IAW ERA 091244-14.SDR DL767040663Fitting · damagedLEFT WING FRONT SPAR OUTBOARD PITCH LOAD FITTING HAS TWO DAMAGED HOLES DUE TO TOOLING WHILE ACCOMPLISHING EO 01-074906-03AD. REPAIR IAW ERA 091345-14AD.SDR DL767040637Valve · inoperativeACFT WOULD NOT PRESSURIZE AFTER TAKEOFF. REPLACED FWD EQUIPMENT COOLING OVERBOARD EXHAUST VALVE.SDR DL767040614Structure · corrodedWHILE ACCOMPLISHING THE I/B TRAILING EDGE MAIN FLAP ATTACH BOLT REPLACEMENT PER EA 01-085672-12AD, CORROSION WAS FOUND IN THE BORES OF THE FWD TWO AND AFT ATTACH FOUR HOLES OF THE 9-10 BEAM AND THE ASSOCIATED MATING HOLES ON THE FLAP AND THE FOUR HOLES COMMON SDR DL767040601Skin · corrodedCORROSION FOUND ON THE FUSELAGE SKIN AT APPROX FS 1323 BETWEEN S-39R AND 39L. DAMAGE REPAIRED WITH DOUBLER/TRIPLER ARRANGEMENT VIA ERA 091295-14 REV B.SDR DL767040603Sill · corrodedER/A 091340-14, C2 DOOR LOWER SILL WAS FOUND WITH CORROSION LOCATED ON THE INNER CHORD UPPER FLANGE AT FS 1270-1279. ADDITIONAL CORROSION WAS FOUND ON THE WEB AT FS 1279.SDR DL767040532Fitting · corrodedLEFT HORIZONTAL STAB CENTER SECTION PIVOT FITTING WAS FOUND WITH A ROTATED BUSHING RETAINER AND SUBSEQUENTLY CORROSION IN THE BORE. REPAIRED PER ERA 090340-14.SDR DL767040463Stiffener · crackedCRACKS WERE NOTED IN THE RADIUS OF THE RBL AND LBL 10 VERTICAL STIFFENERS OF THE CENTER SECTION FRONT SPAR. CRACKS WERE LOCATED APPROXIMATELY 5 INCHES FROM TOP OF STIFFENER. DAMAGE WAS REMOVED AND SPLICE INSTRUCTIONS PROVIDED VIA ERA 090218-14.SDR DL767040384Structure · corrodedRIGHT I/B FLAP ATTACH BOLTS HOLES CORRODED. REPAIRED PER ERA 089397-14MA REF NRC402 404 400 403 399 401.SDR DL767040293Battery · dischargedEMERGENCY EXIT SIGNS INOP AT RT AND LT OVERWING EXIT DOORS. REPLACED EMERGENCY PWR SUPPLY BATTERIES AT M737, M732 PER M/M, NOW OPS NORMAL.SDR DL767040222Wire · brokenMCO LEFT WING ILLUMINATION LIGHT INOP. FOUND LIGHT ASSY TERMINAL BOARD BROKEN AND WIRES DAMAGED WITH EVIDENCE OF ARCING. NDS NEW ASSY TO INCLUDE TERMINAL BLOCK NOT SHOWN IN IPC. NDS MFG P/N 30-1543-1. NASI DAL, PULLED AND COLLARED C/B N-35 WING ILLUM ON P1SDR DL767040507Wire · corrodedDURING HMV IN GSO FOUND NR 2 PYLON AND ENGINE WIRING CORRODED AT CANNON PLUGS. REPLACED WIRES AND PLUGS.SDR DL767040506Wire · corrodedDURING HMV IN GSO FOUND NR 1 PYLON AND ENGINE WIRING CORRODED AT CANNON PLUGS. REPLACED WIRING AND PLUGS.SDR DL767040158Fuse · blownON MAINTENANCE PREFLIGHT INSPECTION FOUND FIRST CLASS EMERGENCY LIGHTS INOP IN THE SEAT PANELS. TROUBLESHOOTING FOUND BLOWN FUSE IN POWER SUPPLY M9008. REPLACED FUSE, LIGHTS NOW OPERATIONAL CHECK OK.SDR DL767040154Fitting · corrodedTHE INBOARD SUPPORT BEAM FOR THE INBOARD FLAP ON THE LT WING WAS FOUND WITH CORROSION IN THE FLAP ATTACH HOLES. THE CORROSION WAS REMOVED BY OVERSIZING THE HOLES. ALUMINUM REPAIR BUSHINGS WERE FABRICATED AND INSTALLED IN THE HOLE BORES. THE REPAIR WAS ACCOMSDR DL767040123Fan · failedIN FLIGHT THE CREW REPORTED, GOT A RT RECIRC FAN INOP LIGHT ACCOMPANIED BY A STRONG PUNGENT ODOR. THE ODOR WENT AWAY WHEN BOTH RECIRC FANS WERE TURNED OFF. ALSO PULLED THE CIRCUIT BREAKER FOR THE RT RECIRC FAN. THE LT RECIRC FAN OPERATED NORMALLY ON THE GROSDR DL767040128Fitting · corrodedWHILE ACCOMPLISHING BOLT REPLACEMENTS FOR THE INBOARD FLAP SUPPORT FITTINGS ON THE LT & RT WINGS PER AD 2002-22-07, SEVERAL FITTING HOLE BORES WERE FOUND WITH CORROSION. THE HOLE BORES WERE OVERSIZED TO REMOVE ALL CORROSION, HFEC INSPECTED, AND BUSHED. NEW BSDR DL767040009Beam · corrodedCORROSION WAS FOUND IN THE HOLE BORES OF THE '9-10' BEAM WHICH PROVIDES THE OUTBOARD SUPPORT FOR THE INBOARD FLAP ON THE LT WING. THE CORRODED HOLES WERE OVERSIZED TO REMOVE CORROSION AND BUSHED TO ALLOW INSTALLATION OF PROPER SIZE BOLTS. THE REPAIR WAS ACCO
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