Boeing 767-232
Service difficulty reports · 2,991
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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 = '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 DL767982603Switch · failedLEFT MAIN GEAR INDICATED UNSAFE WHEN LOWERED. POM WAS FOLLOWED, HOWEVER GEAR STILL INDICATED UNSAFE HYD. QUANTITY AND PRESSURES WERE NORMAL. REPLACED LANDING GEAR LEVER AND SWICTHES AS PROXIMITY BOX. FAULTED SWITCH 421 AND 422. ALSO, REPLACED LEFT GEAR. SDR DL767982344Wedge · delaminatedTHE UPPER SKIN OF THE TRAILING EDGE WEDGE ON THE NR 6 SLAT WAS FOUND WITH A 5 X 4 AREA OF DELAMINATION APPROXIMATELY 62 INCHES FROM THE O/B EDGE OF THE SLAT. THE DAMAGE WAS TRIMMED AWAY AND REPAIRED PER THE B767 SRM 51-70-10 AND DOCUMENTED PER ER/A 366072-14ASDR DL767982222Air Dist · smokeF/A REPORTED SMOKE IN AFT CABIN. UPON DISCONNECTING UTILITY BUSES ODOR/SMELL WENT AWAY. RESET UTILITY BUSES OPERATED ALL GALLEY EQUIPMENT, NO ODOR PRESENT. RAN PACK RECIRC FANS AND GASPER FANS, TURNED ON ALL LIGHTS AND VIDEO EQUIPMENT AND NO TROUBLE FOUND.SDR DL767982109Oven · contaminatedSHORTLY AFTER TAKEOFF, SMOKE OBSERVED FROM AFT GALLEY OVENS. COULD NOT DETERMINE SOURCE OF SMOKE, FOOD OR ELECTRICAL. FOUND BURNT SUBSTANCE IN CORNER OF LOWER LEFT OVEN IN AFT GALLEY. REPLACED OVEN ASSEMBLY AND NEW OVEN, OPS NORMAL.SDR DL767981889Battery Pack · dischargedMSU T/S EMERGENCY LIGHT PROBLEM. FOUND M735 BATTERY CHARGER BAD. REPLACED CHARGER AND BATTERY PACK. CKS NML.SDR DL767981885Skin · corrodedCORROSION DAMAGE WAS FOUND DURING ROUTINE INSPECTION OF THE CENTER WING UPPER SKIN OVERLYING THE REAR SPAR. CORROSION WAS LOCATED AT LBL 68 NEAR THE DRAIN AT LBL 75. REPAIRED PER ERA 332134-14.SDR DL767981886Floorbeam · corrodedCORROSION WAS FOUND ON THE UPPER CAP OF THE RBL 33 LONGITUDINAL OVERWING FLOORBEAM BETWEEN FS 835 AND 910. A SECTION OF UPPER CAP WILL BE REPLACED WITH A SPLICE REPAIR ON EACH END OF THE REPLACEMENT SECTION. REPAIRED PER ERA 332139-14.SDR DL767981800Rvdt · intermittantAFTER TAKEOFF, L/E CAUTION AND L/E SLAT ASSY EICAS MSG. RETURNED TO LAX. REPLACED M548 RVDT PER MM, ALL OPS NORMAL.SDR DL767981766Light · inoperativeAFT EMERGENCY LIGHT ON SEAT 25F INOP. REPLACED LIGHT ASSY, CKS GOOD.SDR DL767981757Light · damagedEMERGENCY TRACK LIGHTING DAMAGED BY 2L DOOR. INSPECTED ALL EMERGENCY TRACK LIGHTING, REPAIRED DAMAGE, CKS OK.SDR DL767981726Floorbeam · corrodedCORROSION DAMAGE WAS FOUND ON THE UPPER CAP OF THE OVERWING LONGITUDINAL FLOORBEAM AT RBL 54, FROM BS 850 TO THE AFT END OF THE UPPER CAP AT APPROX BS 1000. THE UPPER CAP WAS REPLACED, BUT THE ORIGINAL EXTRUSION COULD NOT BE OBTAINED. REPAIRED PER ERA 332058SDR DL767981707Floorbeam · corrodedCORROSION WAS FOUND ON THE UPPER SURFACE OF THE BS 287 FLOORBEAM UPPER CHORD. IN ADDITION, AN EXISTING REPAIR WAS ALSO LOCATED IN THE SAME AREA. REPAIRED PER ERA 332044-14.SDR DL767981666Battery Pack · dischargedL1 SLIDE LIGHT INOP, ALSO BOTH LT OVERWING SLIDE LIGHTS INOP. REPLACED BOTH BATTERIES.SDR DL767981617Power Supply · inoperativeRT OVERWING EGRESS LIGHTS INOP. REPLACED BATTERY POWER SUPPLY, CKS GOOD.SDR DL767981469Wedge · delaminatedDELAMINATION WAS FOUND ON THE NR 1 SLAT T/E WEDGE. DELAM AREA IS APPROX 4 IN DIAMETER. REPAIRED PER ERA 365245-14AD.SDR DL767981422Check Valve · failedRIGHT GEN DRIVE LIGHT ILLUMINATED AFTER TAKEOFF. REPLACED PRESSURE SERVICE CHECK VALVE, LEAK CHECK GOOD.SDR DL767981374Engine · failedAS POWER CAME UP FROM IDLE A BANG WAS HEARD AND LT ENG REMAINED AT IDLE PWR. NO CONTROL OF LEFT ENG FROM COCKPIT. NO ENG EXCEEDANCE NOTED AND NO INDICATIONS IN COCKPIT OF ENG FAILURE. ENG WAS NOT SHUTDOWN FOR EMERG LANDING AT JFK. FOUND METAL IN TAILPIPESDR DL767981281Skin · delaminatedDELAMINATION WAS FOUND ON SEVERAL T/E WEDGES OF THE L/E SLATS (NR 1, 2, 4 AND 5). REPAIRED PER ERA 365004-14AD.SDR DL767981211Skin · dentedFUSELAGE SKIN WAS FOUND WITH A GOUGE LOCATED AT BS 632 BETWEEN STRINGERS 30R AND 31R. REPAIRED PER ERA 331774-14 REV B.SDR DL767981213Bulkhead · damagedBULKHEAD AT NAC STA 163.5 ON THE RT OF PYLON HAD TOOLING DAMAGE THAT NECESSITATED PART REPLACEMENT. NO REPLACEMENT PART AVAILABLE, A NEW PART WAS FABRICATED. PART FABRICATED PER ERA 331773-14.SDR DL767981212Skin · corrodedCORROSION WAS FOUND AROUND SEVERAL FASTENER HOLES WHERE THE FWD AND AFT CTR WING UPR SKIN ATTACHES TO STGR U-17 BETWEEN LBL 74 AND LBL 90. A SECTION AFT OF THE AFT UPPER WING SKIN WAS REMOVED. REPAIRED PER ERA 331767-14.SDR DL767981132Skin · crackedNACELLES, NR 2 PYLON, TORQUE BOX, INBD STRUT SKIN, ACCESS CUTOUT: REPAIR FOR CRACK. THE NR 2 PYLON TORQUE BOX SKIN WAS FOUND WITH A CRACK IN THE UPPER AFT CORNER OF THE ACCESS CUTOUT AT NAC STA 231. THE CRACK WAS STOP DRILLED ON A TIME-LIMITED BASIS WITH A SDR DL767981097Wedge · delaminatedNR 5 LEADING EDGE SLAT T/E WEDGE WAS FOUND WITH DELAMINATION ON THE UPPER SURFACE MEASURING 3 X 5. REPAIR PER ERA 364831-14AD.SDR DL767981067Engine · failedIN DESCENT, NR 2 ENG SHOWED NO OIL QTY AND 10 PSI PRESS. SHUT DOWN ENGINE PER POM. MAINTENANCE IN PROGRESS. FOUND METAL ON CHIP DETECTOR, REPLACED ENGINE.SDR DL767980799Structure · corrodedFUSELAGE STRINGERS 36L TO 33R WERE FOUND CORRODED BETWEEN FS 412 AND 456. NEW SECTIONS OF STRINGER WERE SPLICED IN PER SRM OR LONGER BLUEPRINT STRINGER SPLICES WERE INSTALLED. A SMALL SECTION OF SKIN WAS CORRODED AND CUTOUT. THE SKIN WAS REPAIRED PER THSDR DL767980581Wedge · dentedTHE RT WING NR 7 SLAT WAS FOUND WITH A 5 X 2.5 X .025 DENT ON THE LOWER SURFACE THE TRAILING EDGE WEDGE. THE DENT WAS REPAIRED PER THE B767 SRM 57-43-02 AND DOCUMENTED PER ER/A364235-14AD.SDR DL767980499Wedge · delaminatedTHE LT WING NR 4 SLAT WAS FOUND WITH A 3 INCH DIAMETER AREA OF SKIN DELAMINATION. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364149-14AD.SDR DL767980419Wedge · delaminationTHE UPPER SKIN OF THE LT WING NR 4 SLAT TRAILING EDGE WEDGE WAS FOUND WITH 2 AREAS 2 INCH DIAMETER DELAMINATIONS. THE THE DAMAGE WAS REPAIRED PER THE B767 SRM AND DOCUMENTED PER ER/A 364074-14AD.SDR DL767980413Light · inoperativeON L/O, FOUND ONE LT AND ONE RT EMERGENCY LIGHTS INOP AFT OF CARGO DOORS ON FUSELAGE.SDR DL767980421Wedge · delaminatedTHE UPPER SKIN OF THE RT WING NR 8 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 4 X 2.5 AREA OF DELAMINATION. THE DAMAGE WAS REPAIRED PER THE B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364048-14AD.SDR DL767980420Wedge · delaminationTHE UPPER SKIN OF THE LT WING NR 5 SLAT WAS FOUND WITH A 1 INCH DIAMETER AREA OF DELAMINATION. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364049-14AD.SDR DL767980380Skin · dentedTHE FUSELAGE SKIN WAS BADLY DENTED AT FS 1351 NEAR STRINGER 31R (JUST AFT OF THE C2 DOOR CUTOUT). THE UNDERLYING FRAME WAS ALSO DENTED. THE DAMAGED FRAME WAS REPAIRED PER THE B767 SRM 71-70-11. THE DENTED SKIN WAS CUTOUT AND REPAIRED WITH AN ALUMINUM DOUBLESDR DL767980328Power Supply · inoperativeSECTIONS OF SEAT MOUNTED EMERGENCY LIGHTING INOP. FOUND ON PREFLIGHT. REPLACED POWER SUPPLY, SYSTEM CKS GOOD.SDR DL767980207Pressure Deck · crackedTHE WHEEL WELL PRESSURE DECK WAS FOUND WITH A CRACK AT 977 ON THE LEFT HAND SIDE AT LBL 35, THE CRACK IS 12 INCHES LONG. THE CRACK WAS REPAIRED PER 767-200 SRM 53-50-51 FIG 202 AND ERA 363828-14. AN EIGHT INCH CRACK WAS ALSO FOUND ON THE RIGHT HAND SIDE ATSDR DL767980813Battery · dischargedJUMPSEAT TWO CENTER FLASHLIGHT RED LIGHT NOT FLASHING. REPLACED BATTERY AND BULB ASSY.SDR DL767972696Skin · puncturedTHE FUSELAGE SKIN AT FS 422 BETWEEN STRINGERS 21L AND 22L WAS PUNCTURED BY GROUND EQUIPMENT. THE FINAL SKIN CUTOUT WAS 6.5 BY 5. THE DAMAGE WAS REPAIRED WITH A SKIN DOUBLER. INSTALLED PER THE PROCEDURES OF THE B767 SRM AND DOCUMENTED PER ER/A 300885-14, REVSDR DL767972679Bracket · brokenDURING MTC, AFTER OPERATING THE RT ENG TO IDLE FOR HIGH OIL CONSUMPTION CHECKOUT, FOUND FUEL RUNNING FROM RT ENG STRUT DRAINLINE. INSPECTED AREA, FOUND ENG FUEL FEED LINE COUPLING AT THE TOP OF THE STRUT JUST FWD OF THE WING LE CHAFFED THRU DUE TO A BROKEN HYSDR DL767972547Stringer · corrodedCORROSION DAMAGE BEYOND LIMITS FOUND ON STR 34R FROM STA 550 TO STA 654. REPAIRED PER ERA 331055-14.SDR DL767972546Stringer · corrodedSTR 30R CORRODED BEYOND LIMITS BETWEEN STA 1439 AND 1461. ALSO, STR 32R CORRODED BEYOND LIMITS BETWEEN STA 1417 AND 1439. REPAIRED PER ERA 331054-14.SDR DL767972545Floorbeam · corrodedCORROSION FOUND ON STA 287 FLOORBEAM UPPER CHORD FROM LBL 10 TO THE RT EOP. REPAIRED PER ERA 331029-14.SDR DL767972544Floorbeam · crackedFS 246 FLOORBEAM UPPER WEB FOUND WITH TYP CRACK AT RBL 20 UNDERNEATH THE RBL 20 STIFFENER. ALSO, STIFFENER CRACKED. ADDITIONALLY, CORROSION FOUND ON WEB AND MID CHORD AT APPROX RBL 30 AND RBL 40. REPAIRED ERA 331015-14.SDR DL767972543Skin · corrodedADDITIONAL CORROSION DAMAGE FOUND NEAR EXISTING REPAIRED CORROSION DAMAGE (REF ERA208585-14). REPAIR IS REMOVED AND A LARGER REPAIR INSTALLED. REPAIR PER ERA 208585-14, REV B.SDR DL767972513Skin · corrodedTHE FUSELAGE SKIN AT BS 1202, STR 39R WAS FOUND CORRODED. THE CUTOUT IS APPROX 5.5 X 1.75 IN THE SKIN. REPAIRED PER ERA 331052-14.SDR DL767972491Bulb · missingEMERGENCY TRACK LIGHT BULB AND LENS MISSING AT ROW 34B. INSTALLED BULB, LENS, AND O-RING AT EMERGENCY LIGHT 34B.SDR DL767971914Hose · chaffedAPPROX 30 MIN AFTER ENGINE START-R HYD SYS QTY EICAS MSG. SELECTED STATUS PAGE AND RT HYD QTY SHOWED .05. S/O RT PRIMARY AND DEMAND PUMP OFF. FOUND ENG HYD PUMP PRESS HOSE WORN THROUGH. HOSE WAS RUBBING BRACKET BOLT HEAD JUST BELOW TOP GANG CLAMP. REPLACEDSDR DL767971849Hyd Line · leakingLT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. AN APPROVED INTERIM LINE HAD BEEN INSTALLED AT MIA BECAUSE OF A HYDRAULIC LEAK. REPLACED LINE WITH PERMANENT REPAIR. BLED AND PURGED SYS PER MM TRUCK POSITIONING ACTUATOR REPLACEMENT PROCEDURES. SUSPECTSDR DL767971804Power Supply · inoperativeTWO SECTIONS OF EMERGENCY FLOOR TRACK LIGHTS IN REAR SECTION OF AIRCRAFT INOP. REPLACED BATTERY PACKS AND RACKS M9009 AMD M9010. EMERGENCY FLOOR TRACK LIGHTS OPS NORMAL.SDR DL767971718Ram Air Turbine · failedLOSS OF CENTER HYDRAULIC PRESSURE AND QUANTITY ON TAKEOFF. FOUND FAILURE OF THE RAM AIR TURBINE GROUND CHECKOUT MODULE IN THE RIGHT WHEEL WELL. REPLACED SAME, SYSTEM CHKS OK.SDR DL767971668Power Supply · inoperativeLEFT CENTER BY MID GALLEY OVERHEAD EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY, OPS CHECKS NORMAL.SDR DL767971667Power Supply · inoperativeRT SIDE OUTSIDE EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY, CHECKS NORMAL.
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