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 DL767971666Power Supply · inoperativeFWD MOST 4 RT OVERHEAD EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY, SYSTEM OPS CHECK NORMAL.SDR DL767971665Power Supply · inoperativeAFT LT 3 OUTSIDE EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY, OPS CHECK NORMAL.SDR DL767971631Inverter · failedFL 390 EN ROUTE TO KSFO, FIRST HAD A STATUS MESSAGE STANDBY INVERTER, FOLLOWED BY A BURNING SMELL AND THEN HEAVY SMOKE, FOLLOWED SMOKE REMOVAL CHECKLIST AND DIVERTED INTO KLAS. FOUND STATIC INVERTER FAILED, REPLACED SAME. PERFORMED TEST PER MM. ALL OPS NORMSDR DL767971572Union · brokenAFTER T/O, RETRACTED GEAR, RAISED FLAPS TO 5 DEG, THEN 1 DEG AND LOST HYD FLUID IN CTR SYS. FLAPS REMAINED AT 5 DEG, RAISED WITH ALT SYS. MTC FOUND UNION (P/N S270T230- 20) ON OUTLET OF ADP PUMP BROKEN. REPLACED WITH AS1582C10.SDR DL767971526Skin · delaminatedTWO AREAS OF DELAMINATION WERE FOUND ON THE UPPER SKIN OF THE NR 11 SLAT T/E WEDGE. ONE AREA OF DELAMINATION WAS FOUND ON THE UPPER SKIN OF THE NR 12 SLAT T/E WEDGE. NO CORE DAMAGE OCCURRED ON ANY OF THE DAMAGE. THE DAMAGE WAS REPAIRED PER B767-200 SRM 57-4SDR DL767971506Skin · corrosionCORROSION DAMAGE TO THE WING CENTER SECTION UPPER SKIN WAS FOUND AT NUMEROUS LOCATIONS AT THE UPPER SKIN TO STRINGER ATTACH FASTENER HOLES ON STR 1 TO 8, 10 TO 12, 14 AND 15. ALSO, CORROSION WAS FOUND AROUND SEVERAL SKIN TO REAR SPAR ATTACH FASTENER HOLES. RSDR DL767971505Seat Track · crackedTHE FUSELAGE SEAT TRACKS LOCATED AT LBL 33, 55 AND RBL 54 WERE FOUND CRACKED IN THE VERTICAL WEB OF THE UPPER CHORD AT APPROX FS 786 AS DESCRIBED IN S/B 767-57-0029. IN ADDITION, PREVENTATIVE MODIFICATIONS TO THE LBL/RBL 33 AND LBL/RBL 54 FLOORBEAMS ARE BEINGSDR DL767971504Skin · corrosionCORROSION WAS FOUND JUST AFT OF STA 1307 UNDER THE UHF ANTENNA BOX. THE DAMAGE WAS CUTOUT AS SHOWN IN FIGURE 1. THE SKIN AT THIS LOCATION HAS A MAX THICKNESS OF .135 AND IS CHEM-MILLED FROM 2024-T3 CLAD SHEET. A PREVIOUS REPAIR IS LOCATED JUST FORWARD OF THSDR DL767971482Skin · corrosionCORROSION WAS DISCOVERED ON THE UPPER SURFACE OF THE WING CENTER SECTION UPPER SKIN PANELS AT BUTT SPLICE BETWEEN THE FORWARD AND AFT SKIN PANELS AT STRINGER 17, BETWEEN RBL 74.81 AND 97.42. THE SKIN WAS TRIMMED TO REMOVE THE CORROSION IN THE FORWARD AND AFT SDR DL767971379Power Supply · inoperativeAFT SECTION OVERHEAD AISLE EMERGENCY LIGHTS AND R-4 DOOR EXIT LIGHT INOP. REPLACED POWER SUPPLY. SYSTEM CHECKS NORMAL.SDR DL767971332Slat · delaminatedTHE NR 9 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE A 4 INCH INBOARD/OUTBOARD X 2 FWD/AFT SECTION OF THE UPPER SKIN DELAMINATED. THE DAMAGE IS LOCATED INBOARD OF THE END OF THE SLAT WEDGE. THIS AREA WAS REPAIRED PER B767 SRM 57-43-02, FIGURE 201SDR DL767971331Skin · corrosionTHE SECTION 46 FUSELAGE SKIN BETWEEN STR 35L AND 36L HAS 3 DISTINCT AREAS OF SEVERE CORROSION THROUGH THE SKIN RESULTING IN .5 DIA HOLES. DAMAGE LOCATIONS ARE 1338, 1363, 1380 AN EXISTING REPAIR ST FS 1389 BETWEEN SUBJECT STR WILL BE REMOVED AND THE DAMAGE INSDR DL767971325Skin · corrosionDURING ACCOMPLISHMENT OF EO 1-60000-3, CORROSION WAS FOUND ON THE UPPER SURFACE OF THE CENTER SECTION UPPER WING SKIN AT APPROXIMATELY FS 950 TO 955 AND RBL 65 TO 80. THE DEEPEST CORROSION WAS FOUND DIRECTLY UNDER THE DRAIN SCREEN LOCATED AT APPROX RBL 70. TSDR DL767971260Light · inoperativeAFT RT OVERWING SLIDE LGT INOP. REPAIRED SHORTED LGT ASSY AND REPLACED FUSE ON PWR SUPPLY.SDR DL767971326Skin · corrosionCORROSION WAS DISCOVERED ON THE WING CENTER SECTION UPPER SKIN, TOP SURFACE, BETWEEN STR U-15 TO THE AFT SPAR AND RBL 75 TO 95. THE CORROSION CONCENTRATED AROUND THE STRINGER TO SKIN FASTENER HOLES ABOVE THE AFT SPAR AND STR 3 TO 8, 11, 12 AND 15. THE FASTENSDR DL767971445Te Wedge · delaminatedTHE NR 5 SLAT TRAILING EDGE WEDGE UPPER SURFACE WAS FOUND DELAMINATED ON THE AFT INBOARD CORNER. THE DELAMINATION IS APPROX 3 BY 3.5. THIS AREA WAS REPAIRED PER B767-200 SRM 51-70-10, FIGURE 9.SDR DL767971198Bulb · failed1R DOOR ARMING LIGHT ON 1L F/A PANEL INOP. RELAMPED, SYSTEM CHECKS GOOD.SDR DL767971116Light · missingIRREG: 3RD WHITE EEPLS LGT MISSING F/C LT SIDE. REPLACED LGT MODULE, CKS GOOD.SDR DL767971117Te Wedge · delaminationTHE NR 8 SLAT WAS FOUND TO HAVE THE TRAILING EDGE WEDGE UPPER SKIN DELAMINATED. THE DELAMINATION IS A 1 DIA CIRCLE, APPROX. 4 FROM THE AFT EDGE OF THE TRAILING EDGE WEDGE AND 3 O/B OF THE I/B END. THE TRAILING EDGE WEDGE IS MANUFACTURED WITH 0.016 5052-H38 FSDR DL767971118Skin · dentedTHE RT SIDE FUSELAGE SKIN WAS DAMAGED BY GROUND EQUIPMENT BELOW THE C3 CARGO DOOR, RESULTING IN A DEEP DENT AT FS 1435 ABOVE STRINGER 35L. THE DAMAGE REQUIRES REMOVAL, REQUIRING A CUTOUT SIZED APPROX 2.0 (RWD/AFT) BY 6.0 (UP/DOWN). STR 35L IS ALSO DEEPLY DENSDR DL767971010Power Supply · inoperativeRT CEILING EMERGENCY LIGHTS OUT. REPLACED POWER SUPPLY M730.SDR DL767970889Tilt Fuse · failedAFTER TAKEOFF, RT MLG WOULD NOT RETRACT. REPLACED TRUCK TILT FUSE, OPS CHECK GOOD.SDR DL767970881Check Valve · failedAFTER TAKEOFF, RT MLG WOULD NOT RETRACT. REPLACED TILT FUSE CHECK VALVE, OPS CHECK GOOD.SDR DL767970788Idg · failedON TAKEOFF, LOST 'L' GEN FOLLOWED BY AC L BUS OFF. STARTED APU DID NOT GET L BUS BACK. FOLLOWED BY 'L' GEN DRIVE LIGHT. APU WAS RUNNING OK. NO ISOLATION LIGHT. REPLACED NR 1 IDG AND GARLOCK SEAL. OPS CHECK GOOD. BPCU FAULTED LT GCU, REPLACED GCU. CHECKSDR DL767970728Skin · corrodedDURING HMV, EXTENSIVE CORROSION WAS FOUND IN THE BELLY SKIN AND STRINGERS BETWEEN STA 1220 TO 1362 AND BETWEEN STRINGERS S-36L AND S-36R. THE FWD SKIN WAS TRIMMED AT STATION 1230 AND REMOVED FROM THE LAP SPLICES ON EITHER SIDE AT S-36L AND S-36R TO THE EOP ATSDR DL767970727Stringer · corrodedMTC DETERMINED THAT ALL STRINGERS FROM 34L TO 32R, EXCEPT 35R, ARE CORRODED BEYOND ALLOWABLE LIMITS. INSTRUCTIONS GIVEN TO SPLICE IN NEW STRINGER SECTIONS.SDR DL767970729Skin · gougedTHE FUSELAGE SKIN WAS FOUND TO BE DAMAGED IN SEVERAL LOCATIONS AFT OF THE LOWER PORTION OF THE L2 DOOR CUTOUT. THE DAMAGE CONSISTED OF SEVERAL GOUGES, A DENT AND AN EXISTING DOUBLER REPAIR ALL WITHIN CLOSE PROXIMITY.SDR DL767970710Skin · dentedA FUSELAGE DENT RUNNING FROM S-39L TO S-34L AND BETWEEN FS 500 AND FS 552 WAS FOUND TO BE OUTSIDE OF ALLOWABLE DAMAGE LIMITS. THE DAMAGE REQUIRES A CUTOUT OF THE DAMAGED SKIN COVERING A FACTORY SKIN JOINT. THE LOWER SKIN IS MACHINED TO 0.056 AND MADE FROM SDR DL767970539Battery Pack · dischargedEMERGENCY TRACK LIGHTING DIM IN COACH CABIN WITH SWITCH IN THE ARMED POSITION. REPLACED THE 9009 AND 9010 BATTERY PACKS, OPERATIONAL CHECK NORMAL.SDR DL767970467Skin · corrodedTHE FUSELAGE SKIN AND STRINGERS WERE FOUND CORRODED BETWEEN STA 1540 AND STA 1562, LOCATED BETWEEN STR 39R AND STR 39L. THE FUSELAGE SKIN IS CORRODED NEAR AN EXISTING DRAIN HOLE. STRINGER SECTIONS WERE SPLICED IN TO REPAIR THE DAMAGED STRINGERS. THE SKIN WASDR DL767970373Skin · corrosionDURING HMV, BULGING WAS DISCOVERED ON THE UPPER SURFACE OF THE CENTER WING, UPPER SKIN PANEL AT THE BUTT-SPLICE, BETWEEN THE FORWARD AND AFT SKIN PANELS AT STRINGER 17 AND BETWEEN RBL 74.81 AND 97.42. THE SKIN WAS TRIMMED TO REMOVE THE CORROSION IN THE FORWARSDR DL767970336Slat · damagedA/C DIVERTED INTO MCO WITH FLAP/SLATS LOCKOUT. ON ARRIVAL, FOUND NR 8 SLAT DAMAGED. REPLACED NR 8 SLAT, OPS CHECK NORMAL.SDR DL767970320Controler · failedAIR RETURN, UNABLE TO PRESSURIZE CABIN. TROUBLE SHOOTING IN PROGRESS. REPLACED EQUIPMENT COOLING SYSTEM CONTROLLER. SYSTEM CHECKS NORMAL.SDR DL767970305Skin · corrosionDURING AN INSPECTION OF THE FAR AFT BELLY SKIN, FURTHER CORROSION WAS FOUND AROUND A CUTOUT REPAIRED PREVIOUSLY BY DAL MTC PER SRM GUIDELINES. THE CUTOUT, APPROX 6.125 BY 7 IN SIZE, IS LOCATED BETWEEN FS 1788 AND FS 1809 AND ON EITHER SIDE OF BL 0 (BETWEEN STSDR DL767970299Skin · crackedDURING A LAYOVER VISIT, SKIN WAS FOUND CRACKED AND CORRODED AT STRINGER 32R AND 34R BETWEEN FS 1461 AND FS 1480. BOTH WERE REPAIRED PER SRM.SDR DL767970089Battery Pack · dischargedRT OVERWING SLIDE AND LEFT SPOILER SQUIBS FAILED TEST ON THE MAINTENANCE PANEL. REPLACED THE BATTERY PACK.SDR DL767970066Light · inoperativeEMERGENCY LIGHT AFT OF C2 CARGO DOOR INOP. RELAMPED, OPS CHECKS NORMAL.SDR DL767970060Panel · missingLT WING TO FUSELAGE PANEL 195CL MISSING MOST SCREWS STILL IN NUTPLATES. PANEL MUST HAVE LEFT INFLIGHT. FOUND DURING LTTR CK. MFG PANEL TREATED AND PAINTED AND INSTALLED PER ERA NR 360958-14.SDR DL767970117Skin · corrosionSKIN AND STRINGERS WERE FOUND CORRODED AT FS 1540 BETWEEN STR 34L AND 39L. A 3.75 BY 2.25 CUTOUT WAS MADE. STRS 34L TO 39L REQUIRED NEW SECTIONS TO BE SPLICED IN. ADDITIONAL DAMAGE WAS FOUND AFTER INITIAL RELEASE OF ER/A. A SECOND 2 BY 3 CUTOUT WAS MADE BESDR DL767962733Hyd Filter · crackedON TAXI OUT, LOSS OF CENTER HYDR QTY WENT TO ZERO AND SYS PRESS LIGHT CAME ON. FOUND C-SYS HYD MODULE AFT BLEW ELEMENT CASE CAUSING HYD FAILURE OF C-SYS. REPLACED EDP FILTERS AND MODULE.SDR DL767962732Skin · corrodedNR 95 CORROSION THROUGH FUSELAGE SKIN AT STA 1542 STR 35. NR 177 THROUGH 182 WRITTEN FOR STRINGER DAMAGE STR 34L THROUGH 39L WILL REPAIR PER ERA 360836-14 AS OF 12/19/96 ERA PENDING FAA APPROVAL.SDR DL767962628Inverter · failedHAD STATIC INVERTER MSG ON EICAS FOLLOWED BY SMELL OF SMOKE. A/C DIVERTED INTO BIS. STATIC INVERTER WAS REPLACED AND FLT CONTINUED ON TO PDX.SDR DL767962482Bolt · looseNR 2 ENGINE FWD MOUNT BOLTS LOOSE. RT FWD, 50 INCH/POUNDS. RT AFT, 500 INCH/POUNDS. LT FWD, 500 INCH/POUNDS. LT AFT, 2,000 INC/POUNDS. WHICH IS THE NORMAL TORQUE. NO GAP EXISTS BETWEEN THE MATING SURFACE OF THE FWD ENGINE MOUNTS. BOLTS REPLACED AND TOSDR DL767962476Doubler · corrodedTHE FUSELAGE LT SIDE BULK CARGO DOOR INTERNAL BEARSTRAP SURROUND DOUBLER WAS FOUND WITH CORROSION BETWEEN FS 1445 AND 1448, JUST OUTBOARD AND ABOVE THE LOWER SILL OUTER CHORD ATTACHMENT. THE DOUBLER WAS BLENDED AND REINFORCED WITH A SHEET METAL DOUBLER. SDR DL767962475Skin · corrodedTHE FUSELAGE SKIN AT F.S.1370 AND STR 39R WAS FOUND CORRODED. THE SKIN WAS CUT OUT AND REPAIRED WITH A DOUBLER. REV. A TO ER/A PROVIDES FAA APPROVAL.SDR DL767962477Skin · corrodedTHE FUSEALGE SKIN WAS FOUND CORRODED AT F.S. 676 BETWEEN STR'S 39L AND 39R. THE DAMAGE WAS CUT OUT AND REINFORCED WITH A DOUBLER. REV A TO ERA PROVIDES FAA APPROVAL.SDR DL767962229Lens · missingFROM CDL RED TRACK LIGHT EXIT LENS MISSING FROM RT OVERWING EXIT. REPLACED LENS AND BULB, OPN NORMAL.SDR DL767962148Fan · shortedSTRONG ELECTRICAL ODOR IN AIRCRAFT ON TAXI-OUT. FWD EXHAUST EQUIPMENT COOLING FAN POPPED C/B. FWD TO MCO AND PLAC PER MEL 21-58-04A, NEEDS FAN DAL 211002542.SDR DL767962113Tr Unit · failedRADAR FAILED IN FLIGHT. R/T FAULT DISPLAYED. REPLACED TRANSCVR. OPS. CHECK NORMAL.SDR DL767962074Switch · malfunctionedALL EXTERIOR EMERGENCY LIGHTS REPORTED ON. RETURNED TO GATE. ASSOCIATED WITH RT AFT ENT DOOR LIGHT CYCLING ON AND OFF. REPLACED PROX SWITCH AT RT AFT DOOR, SYSTEM OPS CHECK GOOD.
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